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Interface - Science topic

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What do we mean by sharp and diffused interface model in the context of multiphase flows?
Kindly clarify the difference with the help of famous methods, i.e., in which category do they fall: phase field method, LBM, LS, VOF, CLSVOF, etc.?
Which one should be preferred and why?
It is kindly requested, if you can, to help with the references to support your answer.
Best regards.
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In the context of multiphase flows, the terms sharp interface model and diffused interface model refer to how the interface between two immiscible phases (e.g., liquid and gas) is represented.
Sharp Interface Model
  • In this model, the interface is treated as a discontinuity with negligible or no thickness.
  • The fluid properties (e.g., density, viscosity) change abruptly across the interface, and the interfacial dynamics (e.g., surface tension) are explicitly computed at the interface.
Famous Methods in this Category:
  1. Level-Set (LS) Method: Represents the interface as the zero level of a signed distance function. The interface is tracked sharply but requires reinitialization to maintain a proper distance function.
  2. Volume of Fluid (VOF) Method: Tracks the volume fraction of a fluid in each computational cell. The interface is reconstructed (e.g., PLIC) and remains sharp, although reconstruction errors may introduce some diffusion.
  3. Coupled Level-Set and VOF (CLSVOF):Combines the accuracy of LS for smooth interface representation with VOF's mass conservation. Maintains a sharp interface with better mass conservation.
Diffused Interface Model
  • Here, the interface is represented as a continuous transition region where fluid properties vary smoothly over a finite thickness.
  • The interface dynamics are modeled by additional equations, often involving a phase field variable.
Famous Methods in this Category:
  1. Phase-Field Method: Introduces an order parameter (e.g., concentration or phase variable) that varies smoothly between the phases. Solves a Cahn-Hilliard or Allen-Cahn equation for the phase variable. Naturally captures topological changes (e.g., coalescence, breakup) but requires fine resolution to resolve the interface width.
  2. Lattice Boltzmann Method (LBM): Can implement both sharp and diffuse interface approaches, but it is commonly used with phase-field-like approaches for diffuse interfaces. Handles complex interfacial dynamics, especially for flows involving micro/nano scales.
Which Should Be Preferred and Why?
The choice depends on application requirements:
  1. Sharp Interface Methods: Preferable when high accuracy in interface shape and dynamics is critical (e.g., droplet collisions, wave breaking). Suitable for macroscale flows with well-defined interfaces. Methods: VOF and CLSVOF are common for mass conservation; LS is chosen for smoother interfaces.
  2. Diffuse Interface Methods: Ideal for flows where topology changes (e.g., coalescence, breakup) occur frequently and need automatic handling. Suitable for microscale flows, flows with thermal or solutal effects, or phase-change problems. Methods: Phase-Field and LBM for interfacial transport processes.
Practical Preference:
  • For industrial applications requiring mass conservation and sharp interfaces (e.g., multiphase simulations in aerospace or automotive sectors), CLSVOF is often preferred.
  • For flows involving interfacial instabilities or complex phenomena like emulsification, Phase-Field or LBM may be more efficient.
Choosing the best model also depends on the available computational resources and the physics of the problem being simulated.
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Can somebody explain the difference in two terms : Interface tracking methods, and interface capturing methods in the context of multiphase flow modelling?
There are multiple methods, like, phase field model, level set, which categories do they fall in and why? if someone can help clarify this. please.
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In the context of multiphase flow modeling, interface tracking and interface capturing methods are two distinct approaches to handling the evolution of interfaces between different phases (e.g., liquid-liquid, liquid-gas). Here's an explanation of each and where methods like the phase-field model and level-set method fit in:
Interface Tracking Methods
  • Definition: Interface tracking methods explicitly track the location of the interface by using computational elements (grids, markers, or particles) that follow the interface as it evolves.
  • Key Features: The interface is a sharp boundary. The computational mesh or marker adapts to follow the interface. Examples: Lagrangian Methods: The interface is explicitly represented by marker points or meshes that move with the fluid flow. Front Tracking Methods: A separate mesh or set of points tracks the interface, which is then projected onto the computational grid.
  • Advantages: Precise interface representation. Accurate modeling of sharp discontinuities in properties like density or viscosity.
  • Disadvantages: Challenging for complex interface topologies (e.g., merging or splitting of interfaces). Computationally intensive due to the need for mesh adaptation or marker handling.
Interface Capturing Methods
  • Definition: Interface capturing methods implicitly represent the interface on a fixed computational grid without explicitly tracking its location. Instead, the interface is reconstructed or identified using a continuous field.
  • Key Features: The interface is not a sharp boundary but is represented by a transition zone. The governing equations for the field are solved across the entire domain, including the interface. Examples: Volume-of-Fluid (VOF): Tracks the volume fraction of a phase in each grid cell. Level-Set Method: Uses a signed distance function to represent the interface location. Phase-Field Method: Represents the interface as a diffuse region where an order parameter (like a concentration or phase field) transitions smoothly between phases.
  • Advantages: Handles complex topologies (e.g., break-up or coalescence) naturally. Suitable for large deformations of the interface.
  • Disadvantages: Less precise representation of the interface. Diffusive nature can blur sharp interfaces if not well-resolved.
Classification of Specific Methods
  1. Level-Set Method Category: Interface capturing. Why: The interface is represented by a signed distance function (zero level-set = interface), and the function is evolved using advection equations. The interface is reconstructed implicitly on a fixed grid.
  2. Phase-Field Model Category: Interface capturing. Why: The interface is represented by a smooth transition of an order parameter (e.g., concentration or phase indicator) governed by coupled partial differential equations (e.g., Cahn-Hilliard or Allen-Cahn equations). The interface is diffuse, and the width is controlled by model parameters.
  3. VOF (Volume of Fluid) Category: Interface capturing. Why: Tracks the volume fraction of the fluid in each computational cell and reconstructs the interface implicitly based on these fractions.
  4. Front Tracking Category: Interface tracking. Why: Uses marker points or meshes that explicitly follow the motion of the interface.
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On the optimization of the interface between biomaterials and semiconductors.
How can biomaterials be effectively combined with semiconductor materials to develop biosensors or implantable medical devices? How do the physicochemical properties between the interfaces affect device performance?
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As semiconductors come between conductors and insulators so they conduct electricity partially. Semiconductors made up of atoms which form covalent bonds with the other atoms around them.
In case of biomaterials, if we use semiconductors then they will form covalent bond via joining functional groups available on biomaterial and the semiconductors which will definitely form the efficient interface. Apart from this, conductivity can be enhanced to some extent which would give good results and ultimately leads to efficient biosensors that can sense analyte to the minimal extent.
In case of biomedical implants, using biomaterial enhances mechanical, chemical and physical properties in combination with the semiconductor can be improved due to mobile electron charge carriers which is essential for overall strength of the whole implants used in biomedical field.
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Hey , i am a college student , i try to simulate a microbond test between a fiber carbon/epoxy resin on Ansys workbench , and i need to set a cohesive elements , i can insert a fracture and i have the choice between interface delamination or contact debonding , i know the difference between both ( the definition of the material law and the elements that are used Inter20X and CONTA..) , at first i tried to do it using a contact debonding but the results are not satisfying so i thought that the interface delamination would be a better choice since it used interface elements that are better to simulate an adhesive ... but i don't see how to set correctly the control match on mesh , i mean which faces i should select ?
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Yanjie Bai , Bhavanasi Subbaratnam thanks a lot for your answers it helps !
I tried to insert a contact debonding , i initially have a bonded contact between the carbon fiber and epoxy , i've defined a material (fracture energies bases debonding ) since i can't define it with a traction separation law ( it is reserved for the delamination interface ) , however it debond at first , then i have a sliding between the epoxy and carbon ...actually my question is : should i try again to modify the mesh, material properties to have better results or should i give up on contact debonding and try to insert interface delamination ?
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Muñoz, Lucio, 2005. " Private and Public Sector Interfaces: Prerequisites for Sustainable Development", In: Sustainable Development Policy & Administration, Chapter 26, Taylor & Francis Group, Boca Raton, Fl, USA.
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David, thank you for taking the time to write.
The reason I wrote the article using true sustainability thinking linked to human rights, governments, and businesses in 2005 was to share a framework that later can be looked up to see progress or failure and follow the why....If you read the article you will see that it gives AN ACADEMIC rationale why all the wrong you list went that way and also be able to look at what should have been,
You will find that we write in same areas from different angles
I do appreciate your comments
Respectfully yours;
Lucio
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I've used the cut and extrude options in the Parts module and the cut operation in the Assembly module. However, when I assemble the soil and pile, there are small gaps or overlaps at the interface. Are there any other techniques or best practices to ensure a perfect fit between the two geometries?
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To avoid gaps or overlaps between the soil and pile in Abaqus during assembly, ensure proper interaction definitions and mesh alignment. Here are some key strategies:
1. Define Contact Interactions: Use appropriate contact pairs between the pile and soil, such as surface-to-surface or node-to-surface contact. Apply a suitable friction coefficient to model realistic soil-pile interaction.
2. Use Tie Constraints: For rigid connections, apply tie constraints to connect the pile and soil surfaces without relative motion.
3. Mesh Compatibility: Ensure that the mesh near the interface of the pile and soil is fine enough to capture contact behavior accurately and that nodes align as closely as possible.
4. Adjust Contact Pressure Parameters: Use a small initial clearance value or adjust the contact stabilization settings to prevent initial gaps.
5. Activate Interaction from Start: Ensure contact definitions are active at the beginning of the analysis to avoid sudden overlaps during simulation.
These methods will help achieve a realistic simulation of soil-pile behavior without issues at the interface.
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Hello everyone,
I am currently simulating a NiO/Ga2O3 p-n junction diode, but I am facing an issue where the diode is not showing any current, even at 5 V. Both materials (NiO and Ga2O3) work fine individually in separate simulations. However, when simulating the NiO/Ga2O3 heterojunction diode, no current flows, and I do not observe any variation in self-heating.
I have defined the material properties for both NiO and Ga2O3 correctly, and when I simulate Ga2O3 with other p-type materials like SiC or GaN, the diode works as expected. Could anyone help me understand why current is not flowing in the NiO/Ga2O3 heterojunction device? Is there a special model or specific interface properties that I need to define for this system?
Any insights or suggestions would be greatly appreciated!
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I'm in the same situation.
Diode is not showing any current. Did you solve the problem? If you solved it, please let me know :)
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When designing hydrogel filler-organic resin coating materials, how can we achieve good distribution of the organic filler within the matrix and form a tight interface?
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Dear Lei Zhang, it depends on the polymer and the filler in question. Generally, two ways of preparing such compounds. Either by melt mixing or by solution mixing. The first way use internal mixers (such as Brabender), two roll-mill, extruders (single and twin screw), and orhers. Solution mixing use Solvent to solubilize first the polymer and after that the filler is added under mixing, once good didpersion is reached, the solvent is gradually evaporated.
Generally, good contact is achieved by the use of coupling agents, where silanes are the most widely used and studied. My Regards
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Reservoir Engineering: Multi-Phase Fluid Flow
1.  Whether the generalization of Darcy’s law to the simultaneous flow of two immiscible fluids by Wyckoff and Botset (eight years following 1856’s Darcy’s law) remains sufficient enough to bring in capillary effects, although, each immiscible fluid obeys Darcy’s law within the diminished pore-space (where, each immiscible fluid occupies an available space in which it can flow, which consists of the pore space minus the space the other immiscible fluid occupies)?
2.  Even though, mass conservation equation considers an explicit flow rate for each fluid phase (water, oil & gas), how does “the combined flow” react to a given pressure drop @ field-scale?
In such cases, whether, the entire reservoir’s flow regime will uniformly obey the linear relation between flow rate and pressure drop?
What is the guarantee that both the immiscible fluids will tend to percolate @ low flow rates (where, the capillary forces remain to be too strong for the viscous forces to move the fluid interfaces), so that linear Darcy’s law would still prevail?
Won’t the enhanced flow rates lead to a non-linearity between flow rate and pressure drop, resulting from the gradual increase in mobilized interfaces?
If not, then, the two different (say, oil and water) (Newtonian) immiscible fluids flowing @ pore-scale - do no more behave as a (single) Newtonian fluid @ continuum-scale (if the effective viscosities of oil and water remain to depend on shear rate)?
In essence, how do we have a control over the following four different scenarios in an oil reservoir @ field-scale?
(a)          Low flow rates (where, the capillary forces remain to be too strong for the viscous forces to move the fluid interfaces, and thereby, still obeying linear Darcy’s law)
(b)         Moderately higher flow rates (appearance of strong pressure fluctuations, but, still obeying linear Darcy’s law)
(c)          Significantly higher flow rates (where, non-linearity set in, and a power law relation between flow rate and pressure drop gets developed)
(d)         Very high flow rates (where, capillary forces become negligible compared to viscous forces, and, eventually, comfortably following linear Darcy’s law)
3.   Feasible to capture the main mechanism responsible for the non-linearity in the flow-pressure relationship @ laboratory-scale?
If so, then, how could we deduce the threshold pressure (the pressure drop at which the interfaces start getting mobilized), associated with the correlation between time-averaged flow rate and excess pressure drop?
And also, would it remain feasible to capture the movement of the interfaces, which consumes energy, and which, eventually, leads to the reduction in the effective permeability @ lab-scale?
Suresh Kumar Govindarajan
Professor (HAG)
IIT Madras
22-Sep-2024
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Maybe you are getting too hung-up on D'Arcy's law: it is a simplification of flow through porous media that was obviously advanced thinking in the 19th century. The main problem with porous media is that the pore size is not easily measured or even calculated, so is approximated in terms of voidage fraction and a mean particle size. It is clear that flow through large rocks are very different from fine sands, and turbulence occurs as the pores (particles) get larger. You are then adding issues like multiphase flows to what is a difficult problem with a single phase. There are many publications on the topic of multiphase flow through porous media.
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Dear Fulden: I am starting to use the Simbiology interface of MAtlab and I found out online that you are a specialist in its use. I wish to ask you a question.
I have already learned to create kinetic models in Simbiology and do simulations by providing values for the parameters. However, I cannot see how to simulate in the interfase the time course of a reaction such as, for example, A + B <-> C, starting simultaneously with different initial concentrations of A, keeping the initial concentration of B constant.
Thanks a lot
Sergio B. Kaufman
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Hello everyone. Let's say I have flagged a variable with limits on the Simbiology diagram: boundary conditions = true. Where and how can I write the numerical values ​​of the limits in the diagram?
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To induce polarization and study of drain current.
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Hello Lakhmikanta Mishra
You can add interface charge density at the junction of two region.Must define x and y region. you can use following syntax in SILVACO TCAD
interface qf=1e13 x.min=3 x.max=4 y.min=0.057 y.max=0.057
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Hello everyone,
I am working on a deep learning power control project using NetSim. So far, I have successfully implemented a tabular Q-learning algorithm and obtained positive results. Now, I am looking to implement advanced reinforcement learning algorithms such as actor-critic and proximal policy optimization (PPO) using Gymnasium.
Could anyone provide guidance on how to interface NetSim with Gymnasium (https://github.com/Farama-Foundation/Gymnasium) for applying these RL algorithms? Any examples or resources would be greatly appreciated.
Thank you!
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Look at the 5G power control example in the page https://tetcos.com/machine-learning-netsim.html
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Chemical EOR: Microgels
1. Could microgels (soft gel particles with 3-D network structure in the size of microns, whose physical status wavers between colloid particles and polymers in a solvent) effectively stabilize emulsions (Mickering Emulsions as against conventional Pickering Emulsions stabilized by solid particles) in an oil-water system?
Whether microgelation would significantly elevate the interfacial pressure and modulus @ oil-water interface (in EOR application)?
In case, if it ends up with a mitigated dilatational modulus, then,
would it maintain a stable anti-deformation ability (during amplitude sweep) in an oil-water system?
2. Can we efficiently utilize the viscoelastic nature of microgels that permits them to stretch and deform; and which in turn leads to an enhanced adsorption section area @ oil-water interface that would make us better understand the interfacial behavior of microgels and its associated fundamental mechanism associated with the stability of the interface and emulsion?
Whether the traditional linear rheology will be able reflect the complete details on the interfacial viscoelasticity,
especially @ higher frequencies and @ large amplitudes
(as against the traditional small amplitude oscillation,
where non-linear responses @ high deformation and high deformation rate remain ignored)?
Will it end up with a relatively low degree of non-linearity under significant ionic strength (with acidic and basic dominant scenarios),
while, enhancing emulsifying capacity and improving the interfacial viscoelasticity in an oil-water system?
3. With an enhanced specific surface area and with an elevated exposure of hydrophobic groups on the surface, to what extent, would it remain feasible to capture the details on
(a) microgel diffusion in the bulk phase;
(b) adsorption;
(c) distortion of microgels @ interface; &
(d) reorganization of microgel aggregates within the surface?
Suresh Kumar Govindarajan
Professor (HAG)
31-Aug-2024
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Micro-gelation significantly impacts the interfacial pressure and modulus at the oil-water interface, especially in Enhanced Oil Recovery (EOR) applications. Key points include:
Interfacial Pressure and Modulus: Microgels form a viscoelastic layer, increasing interfacial pressure and modulus, making the interface more rigid and stable.
Reduction of Interfacial Tension: Microgels, combined with surfactants, reduce interfacial tension, aiding oil recovery by detaching oil droplets from rock surfaces.
Enhanced Stability: Microgels enhance the stability of the oil-water interface, preventing coalescence of oil droplets and maintaining uniform dispersion.
Rheological Properties: Microgels form an elastic interfacial film, withstanding higher stresses and strains, improving EOR efficiency.
In summary, micro-gelation enhances EOR efficiency by improving stability and reducing interfacial tension.
Furthermore, in practicality, Oil & Gas service companies have developped numerous chemical technologies to change the relative permeabilities to water (reduce Kr Water) and increase Ko oil) to control water and produce more oil, or to improve water injectivity.
Hope this shelps
D
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How can I interface different python (or any other language) based AI/ML models with NetSim? Any examples would be very helpful.
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Here is a new 5G power control example: https://tetcos.com/machine-learning-netsim.html. It explains how you can link a RL based scheduling algorithm to NetSim.
  1. The project uses reinforcement learning (RL) for downlink power control in 5G networks to mitigate interference, boost SINR, and maximize sum throughput.
  2. The environment is a 5G cellular network with stationary nodes and fading channels. The agent controls power in each gNB, with the state being a vector of received SINRs at the UEs.
  3. Two RL approaches are implemented: Tabular Q-Learning and more advanced algorithms (PPO, A2C) using OpenAI Gymnasium.
  4. The system is tested on three scenarios: 3 gNBs with 6 UEs, 4 gNBs with 11 UEs, and 7 gNBs with 20 UEs.
  5. Results show RL yields 1.5x to 2.5x performance improvement in sum throughput compared to scenarios without RL.
  6. The document provides detailed instructions on how to run the RL simulation using NetSim and Python, including system requirements and execution guidelines.
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i am a beginner to ansys fluent and working on the analysis of a naca008 aerofoil but after the meshing in fluent section its showing a error "WARNING: Unassigned interface zone detected for interface aerofoil-contact_region-trg" and i am unable to initialize the flow so someone help me to rectify this error
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Hello Gokul .s ,
This means that some interfaces are being generated in your model because you have partitioned the compute domain. If you do not want to use interfaces, you should use Share Topology in SpaceClaim or the Form New Part option if you are working with Design Modeler. The other solution is to connect interfaces in the Make Interfaces section in Fluent, which I do not recommend since you are a beginner.
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Chemical EOR
1. What is the average thickness of the brine film (1 nm??) that exists between reservoir rock mineral surfaces and crude-oil droplets – associated with a carbonate reservoir?
In such cases, whether the oil requires to be removed from solid rock surfaces, or, from relatively smoother brine surfaces?
With nanoparticle dispersion, what is the expected fraction of oil that remains directly in contact with the rock surface? With NPD, What is the expected fraction of oil that remains adhering to the solid rock surfaces through electrostatic forces? What will be the required threshold energy level towards separating oil from the surfaces given the imbalances between Brownian motion and electrostatic repulsion between nanoparticles (for a given nanoparticle size distribution)? Upon using Darcian approach, how would the details on the evolution of molecular structures of rock-brine interface and brine-oil interfaces approaching molecular thickness (from its original brine film thickness) would remain to be helpful?
If we have a slip @ brine-oil interface, how will we be able to quantify the effective viscosity of brine films?
2. Whether the degree of disjoining pressure associated with such brine films would significantly influence the resulting contact angle of oil droplets on rock surfaces?
Whether the alterations in ionic distributions in the Electric Double Layer of the brine film - as a function of brine film thickness and bulk ion concentration – would have an impact on the resulting contact angle?
3. With the thickness of the brine-film bounded between ‘rigid solid rock surface’ and relatively a ‘smooth diffusive oil surface’, would it remain feasible to upscale the details associated with Debye length of brine; the hydration diameter of ions in brine; the characteristic length of the density oscillation of brine molecules near solid rock surfaces; and the width of diffuse brine-oil interfaces – to a relatively larger pore-scale (leaving aside Darcy’s continuum-scale) – towards formulating a new EOR concept or facilitating the improvement of existing EOR technique?
Suresh Kumar Govindarajan
Professor (HAG)
12-Aug-2024
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Hi Suresh - Not sure I know the precise answer because there are many carbonate surfaces in the pore system of a carbonate rock. Different types of surfaces as well as the effect of capillary pressure between the wetting and non-wetting phase in combination with the geometry of the surfaces will undoubtly affect the local thickness of the wetting film. But if you look at capillary pressure curves for carbonates (both oil-brine, air-brine and especially air-Hg capillary pressure curves) and take into account that many oil-brine and air-brine capillary pressure curves are not truly equilibrium curves (it takes too long time to reduce the water saturation due to the low relative permeability to water), then you can extract the irreducible water volume equal to the pore surface water. And if you combine the pore surface volume with the pore surface area (from tomography or BET), then you can estimate that the average thickness of the wetting phase at irreducible water saturation is around 5 nm in carbonates. This is of cause an average value and will be larger in the corners of the pore system and smaller on the flat pore walls away from the corners.
As the recorded Amott water and oil wettability clearly is a function of the maximum hydrocarbon saturation in the pore system I expect that when you reach this minimum average wetting film thickness the film will break/penetrated by the hydrocarbon phase that then may locally change the pore wall wettability and park the irreducible water in the corners.
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As I understood, Vbi is the difference between the conduction band energy level between the Absorber and ETL interface to the Absorber and HTL interface (EC_Abs/ETL - EC_Abs/HTL) divided by the elementary charge (q).
but I am confused about identifying the table's built-in potential (Vbi) value.
Please anyone suggest to me, in full detail.
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The built-in potential (Vbi) is an important parameter in semiconductor devices, particularly in solar cells and other photovoltaic devices. It represents the potential difference that exists across the junction of two materials, typically the absorber layer and the electron transport layer (ETL) or the hole transport layer (HTL).
To identify the built-in potential value, you need to consider the energy band diagram of the device structure. The built-in potential can be calculated as the difference between the conduction band energy levels at the interface between the absorber and the ETL, and the interface between the absorber and the HTL, divided by the elementary charge (q).
Mathematically, the built-in potential can be expressed as:
```
Vbi = (EC_Abs/ETL - EC_Abs/HTL) / q
```
Where:
- `EC_Abs/ETL` is the conduction band energy level at the interface between the absorber and the ETL.
- `EC_Abs/HTL` is the conduction band energy level at the interface between the absorber and the HTL.
- `q` is the elementary charge (1.602 × 10^-19 C).
The key steps to identify the built-in potential value are as follows:
1. Understand the device structure: Identify the absorber layer, the ETL, and the HTL in the device.
2. Determine the energy band diagram: Construct the energy band diagram of the device, which shows the relative positions of the conduction band, valence band, and Fermi level for each layer.
3. Identify the conduction band energy levels: From the energy band diagram, locate the conduction band energy levels at the interface between the absorber and the ETL (`EC_Abs/ETL`), and the interface between the absorber and the HTL (`EC_Abs/HTL`).
4. Calculate the built-in potential: Use the formula `Vbi = (EC_Abs/ETL - EC_Abs/HTL) / q` to calculate the built-in potential value.
It's important to note that the built-in potential can be influenced by various factors, such as the materials used, doping concentrations, and interface properties. Therefore, the specific value of the built-in potential may vary depending on the device structure and the parameters of the individual layers.
good luck; partial credit ai
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I have newly installed GaussView 6.0 on Linux Ubuntu 22, but when I open it, it does not display any operation functions, no text or icons. However, when I open other graphical interface programs such as VMD, there are no problems. What is causing this
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Here are a few potential reasons why GaussView 6.0 might not be displaying any operation functions, text, or icons when you open it on your system:
1. Compatibility issues:
- GaussView 6.0 may not be fully compatible with the latest version of Ubuntu 22. Some older software can have compatibility issues with newer Linux distributions.
- Check the system requirements and supported Linux distributions for GaussView 6.0 to ensure it's officially supported on Ubuntu 22.
2. Graphics driver issues:
- The graphical user interface of GaussView 6.0 may be experiencing rendering problems due to incompatibilities with your system's graphics drivers.
- Try updating your graphics drivers to the latest version and see if that resolves the issue.
3. Missing dependencies:
- GaussView 6.0 may be missing certain libraries or dependencies required for its proper functioning on your Ubuntu 22 system.
- Check the software's documentation or installation instructions to ensure you have installed all the necessary dependencies.
4. Permissions and environment variables:
- Ensure that you have the correct permissions to run GaussView 6.0 on your system.
- Check if any environment variables required by GaussView 6.0 are set correctly.
5. Conflicting software:
- It's possible that other software installed on your system is interfering with the proper functioning of GaussView 6.0.
- Try running GaussView 6.0 in a new user account or a clean environment to see if the issue persists.
To troubleshoot this issue, you can try the following steps:
1. Check the GaussView 6.0 documentation or contact the software vendor for any known issues or compatibility information with Ubuntu 22.
2. Update your graphics drivers to the latest version and see if that resolves the problem.
3. Verify that you have installed all the necessary dependencies for GaussView 6.0 on your Ubuntu 22 system.
4. Check the permissions and environment variables related to GaussView 6.0.
5. Try running GaussView 6.0 in a new user account or a clean environment to see if the issue is specific to your current setup.
Good luck; partial credt ai
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I am trying to test the coincidence lattice method for the interface between wurtzite (0001) GaN and cubic diamond (111). How do I rotate the two lattices with respect to one another using VESTA?? I am fairly familiar with the VESTA interface and have used it extensively, just not for something like this. For reference, I am wanting to do something like in figure 4 of this paper ( ), where the hexagonal lattice is matched to the cubic lattice (experimental results have told us that the angle is somewhere between 20-25 degrees). The ultimate goal is to create an interface to study thermal transport across the interface using MD simulations in VASP. Thank you in advance for any help/advice.
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Eric Welch hey Eric , may you share, how you have managed to get particular coincidence angle between two surface ( as you mentioned in your query above) by using VESTA. I also want to study dynamics at boundaries of crystals structure.
Thank you
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I submitted my journal and got some comments, I have answered and corrected all the comments from the reviewer but I don't understand how to answer this question.
any expert researcher help me to explain what I have to do and how?
What can the authors say about the interface problem between the concrete core and the CFRP shells? What is the adhesion type like? How can core-shell bonding affect performance?
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What type of adhesive you are using?
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Hi,
I need to find out the effect of muddy bottoms in ship resistance in shallow water canals. For that I need to simulate two interfaces, ie) air water interface and mud water interface (I have to specify the thickness of the mud layer). How this done in STARCCM+?
Thanks, and regards.
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NUMERICAL MODELLING OF THE MUDDY LAYER EFFECT 1 ON SHIP’S RE2
SISTANCE AND SQUAT
3
4 Sami Kaidi, CEREMA-DtecEMF, Margny les Compiègne, France ;
5 Emmanuel Lefrançois, Université de technologie de Compiègne Sorbonne universités, laboratoire Roberval FRE 2012
6 CNRS, France ;
7 Hassan Smaoui, CEREMA-DtecEMF, Margny les Compiègne, France ;
8
9 ABSTRACT
10 The increasing use of maritime transport has led to an increase in ship size. However, the dimensions of channels and
11 harbours cannot follow the expansion rate of ships. Large ships will experience shallow water effects such as the bottom
12 effect more severely, which plays an important role in the manoeuvrability and the stability of ships. To reduce naviga13
tional restriction in estuary environment and close to ports (see Figure 1), the World Association for Waterborne
14 Transport Infrastructure (PIANC) established the concept of the nautical bottom. Using this concept, ships can navigate
15 with both small and negative under keel clearance (UKC) relative to the water-mud interface. Hence, the aim of this
16 work, is to conduct a numerical investigation in order to study the influence of the muddy seabed on the ship’s manoeu17
vrability especially on the ship’s resistance and squat. Accordingly, a 3D Computational Fluid Dynamics (CFD) model
18 based on the Volume of Fluid (VoF) method was used to simulate the multiphase flow for various setups. Four parame19
ters were tested: the mud properties, the ship's speed, the mud thickness and the UKC value relative to the water-mud
20 interface. The numerical results of this investigation were in reasonable agreement with experimental data. Through this
21 investigation it was also shown the performances of the CFD method to simulate setups difficult to achieve in tow
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I want to quantify some roughness parameters using AFM data. I tried to quantify some of them by Gwyddion software but its HHCF doesn’t have a fitting function contemplating all parameters I need.
Fit function that I found in my Gwyddion version:
y = 2sigma^2 * ( 1 - exp ( - ( r/E )^2 ))
, where, sigma is the interface width and E is the lateral correlation lenght.
Fit funtion that I was looking for:
y = 2sigma^2 * ( 1 - exp ( - ( r/E )^(2a) ))
, where a is the Hurst exponent.
I also tried to export data to origin and tried to set a new fitting function, but I got stuck on how to build it. Something went wrong since my limit bounds aren't being followed.
If anyone could help me with some insights I will be really grateful.
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The log - log plot of the HHCF data usually has a linear region followed by a plateau. Since for small lateral lengths, the value of HHCF grows as r^(2*alpha), by performing a linear fit of the log - log plot you can calculate the Hurst exponent. Interface width can be calculated from the plateau region. For the plateau region, HHCF grows as 2*sigma ^ (2*alpha). Use this to find sigma.
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Hi, I am using VASP to simulate interface of 2 block material slabs. After bringing them together I can get the stress tensor for the whole simulation box from OUTCAR. However, is there any way to calculate local stress tensors for these 2 sides of the interface separately?
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In VASP, it's not straightforward to calculate the local stress tensor for individual sides of an interface directly from the output files like OUTCAR. However, there are some approaches you can consider to estimate the stress tensor locally at the interface:
  1. Strain Mapping:Calculate the strain tensor for the entire simulation box using VASP output files or post-processing tools. Use the calculated strain tensor to estimate the stress tensor locally at the interface using continuum mechanics principles, assuming linear elasticity. This approach may require additional assumptions, such as uniform elastic properties across the interface region.
  2. Finite Element Method (FEM):Use finite element analysis software or libraries to perform local stress calculations based on the atomic positions and forces obtained from VASP simulations. Convert the atomic positions and forces into a mesh representation and solve the finite element equations to obtain the local stress tensor at the interface. This approach allows for more accurate and localized stress calculations but requires additional software and expertise in finite element analysis.
  3. Density Functional Theory (DFT) Calculations:Perform DFT calculations with a focus on the interface region to directly obtain the local stress tensor. This approach involves setting up a supercell containing the interface region and performing DFT calculations to compute the stress tensor within this region. While computationally expensive, this method provides accurate and detailed information about the local stress distribution at the interface.
  4. Machine Learning Models:Train machine learning models using data from VASP simulations to predict the local stress tensor at the interface based on features such as atomic positions, forces, and strain. This approach may require a large dataset of VASP simulation results for training the models and may not provide the same level of accuracy as DFT calculations but can be computationally efficient.
  5. Post-Processing Tools:Utilize post-processing tools specifically designed for analyzing interfaces and local properties in materials simulations. These tools may offer functionalities for calculating local stress tensors based on atomic positions and forces obtained from VASP simulations.
It's essential to consider the trade-offs between accuracy and computational cost when choosing an approach for calculating local stress tensors at the interface. Depending on your specific research goals and computational resources, you may need to experiment with different methods or combine multiple approaches to obtain meaningful insights into the interface properties.
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What type of interface layer is appropriate for evaporation within the temperature range of 100-200°C when creating a two-layered structure using multilayer formation? Specifically, discuss the characteristics and suitability of various interface layers such as Nafion, polypyrrole, polyaniline, and PEDOT/PSS in this process.
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Well, when we're talking about evaporating interface layers within the temperature range of 100-200°C to form a two-layered structure through multilayer formation, you Md.Saiful Islam need to consider the materials' characteristics and suitability for this process.
Firstly, Nafion is a fluoropolymer known for its excellent thermal stability and chemical resistance. However, it typically requires higher temperatures for evaporation, so it might not be the most suitable choice for this temperature range.
Next, polypyrrole and polyaniline are conductive polymers that offer good film-forming properties. They can be evaporated at lower temperatures and are suitable for creating thin films in the desired temperature range. Their versatility makes them potential candidates for interface layers in multilayer formation.
Lastly, PEDOT/PSS (poly(3,4-ethylenedioxythiophene)/poly(styrene sulfonate)) is another conductive polymer blend commonly used in organic electronic devices. It has excellent film-forming properties and can be evaporated at temperatures within the specified range. Its high conductivity and compatibility with various substrates make it a promising choice for interface layers in multilayer structures.
Considering the temperature range and the requirements for the formation of a two-layered structure through multilayer formation, polypyrrole, polyaniline, and PEDOT/PSS seem to be more appropriate choices compared to Nafion. Each of these materials has its advantages and limitations, but their compatibility with the specified temperature range and film-forming properties make them worth considering for the intended application.
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What is a phenomenon called "false vacuum collapse"?
as you know :
Mean field energy and bubble formation. The cloud is initially prepared in FV with all atoms in |↑⟩ (A). Although the single spin mode |↓⟩ is lower in energy in the center of the cloud (E↓E↑), the opposite is true in the low-density tails. The interface (domain wall) between ferromagnetic regions with opposite magnetism has positive (kinetic) energy, which is added to the minimum double energy resulting from ferromagnetic interaction. Macroscopic tunneling can occur resonantly in the bubble mode (B), which has a |↓⟩ bubble in the center. The increase in core energy compensates for the cost of domain-wall energy. Crossing the barrier can be caused by quantum fluctuations at zero temperature (full arrow) or by thermal fluctuations at finite temperature (empty arrow). After the tunneling process, the bubble size increases in the presence of dissipation to reach the true vacuum (TV) state (C), without returning to (A). Credit: Nature Physics (2024). DOI: 10.1038/s41567-023-02345-4
An experiment carried out in Italy with theoretical support from the University of Newcastle provided the first experimental evidence of vacuum decay.
In quantum field theory, when a not-so-stable state becomes a true stable state, it is called a "pseudovacuum collapse." This happens through the creation of small local bubbles. While existing theoretical work can predict how often this bubble formation occurs, there is not much empirical evidence.
The Pitaevskii Center for Supercold Atoms Laboratory for the Bose-Einstein Condensation in Trento reports for the first time observations of phenomena related to the stability of our universe. The results are the result of a collaboration between the University of Newcastle, the National Institute of Optics CNR, the Department of Physics at the University of Trento and TIFFA-INFEN and are published in Nature Physics.
The results are supported by theoretical simulations and numerical models, confirming the origin of the decay quantum field and its thermal activation, and opening the way to simulate out-of-equilibrium quantum field phenomena in atomic systems.
This experiment uses a supercooled gas at a temperature less than one microkelvin from absolute zero. At this temperature, the bubbles appear as the vacuum collapses, and Newcastle University's Professor Ian Moss and Dr Tom Billam were able to conclusively show that the bubbles are the result of heat-activated vacuum collapse.
Ian Moss, Professor of Theoretical Cosmology at Newcastle University's School of Mathematics, Statistics and Physics, said: "Vacuum collapse is thought to play a central role in the creation of space, time and matter in the Big Bang, but so far it has not. In particle physics, the decay of the Higgs boson vacuum changes the laws of physics and creates what has been described as the 'ultimate ecological catastrophe'."
Dr Tom Bilam, Senior Lecturer in Applied/Quantum Mathematics, added: "Using the power of ultracold atom experiments to simulate analogues of quantum physics in other systems – in this case the early universe itself – is a very exciting area of research. the moment."
This research opens new avenues in understanding the early universe as well as ferromagnetic quantum phase transitions.
This groundbreaking experiment is only the first step in the discovery of vacuum decay. The ultimate goal is to find vacuum decay at absolute zero temperature, where the process is driven solely by quantum vacuum fluctuations. An experiment in Cambridge, supported by Newcastle as part of the national QSimFP collaboration, is doing just that.
Stam Nicolis added a reply:
Just what the name says: There are many physical systems, whose potential energy, in the absence of fluctuations, possesses more than one minima. If these minima are not degenerate, it can occur that one is the absolute minimum, however, due to the choice of initial conditions, the system is found in another minimum. In the absence of fluctuations, it will stay in the potential well of that minimum.
In the presence of fluctuations, it can occur that the relative minimum is no longer a minimum: In that case the system won't stay there forever and it is possible to compute the rate at which it will evolve to another state.
While the presence of fluctuations is a necessary condition, it isn't sufficient for transitions to be possible.
Sergey Shevchenko added a reply:
What is a phenomenon called "false vacuum collapse"?”
- the answer to this question is: the question really is absurdity, since really there cannot be fundamentally any “false vacuum”, i.e. that really is an fundamental absurdity, and so its “collapse” is absurdity as well.
Though yeah, in mainstream physics really rather numerous fantastic/mystic “true/false vacuums” really exist, and corresponding publications, where corresponding fantastic/mystic properties and effects of/in the vacuums are “discovered”, are well popular and numerous.
That exists in the mainstream completely logically inevitably from the fact that in the mainstream all really fundamental phenomena/notions, first of all on this case “Matter”– and so everything in Matter, i.e. “particles”, “fundamental Nature forces” – and so “fields”, etc., including “vacuum”, “Consciousness”, “Space”, “Time”, “Energy”, “Information”, are fundamentally completely transcendent/uncertain/irrational,
- and so in every case when the mainstream addresses to something that is really fundamental, the results completely inevitably are only some the fantasies.
More see recent SS post in https://www.researchgate.net/post/What_is_a_super_vacuum_Is_the_earth_in_a_vacuum_And_what_is_dark_energy , and links in the post; reDzennn comment, 9/8 [because of too active moderator] passages, to a Nature Physics (2024) paper in
Zoltan Vilagosh added a reply:
Not that complicated really. False vacuum example = because you cannot see over the hill, you think are at the lowest level possible. This makes you think you have no potential energy left. But a surprise awaits if you make it to the top of the hill...you tumble lower onto the vast endless plain on the other side.
__/\O/\
\
\__O
Sergey Shevchenko added a reply:
“…Not that complicated really. False vacuum example = because you cannot see over the hill, you think are at the lowest level possible. This makes you think you have no potential energy left. But a surprise awaits if you make it to the top of the hill...you tumble lower onto the vast endless plain on the other side. …..”
- that above looks as tooo not complicated passage really, though, again, on such level the authors of the paper in a top physical Nature Physics (2024) journal also thought,
- which “discovered” “false vacuum bubbles decays” in some Bose-Einstein Cond sate of Na-23 atoms, more see reDzennn comment, 8 passages, in https://phys.org/news/2024-01-phenomenon-false-vacuum-decay.html, the strangely removed by moderator passage is in the end of whole comments series.
Though yeah, the really full stop “false vacuum” theories are rather popular in mainstream physics, including rather popular is the theory that Matter was created soon 14 billion years ago at some “bubble in spacetime decay”. Thank heavens till now no any even small bubbles didn’t decay near Earth, and nowhere in Space at all, in last 10 billion of years Milky Way existence.
However, again, this full stop – and so quite easily composed - fantasies are so rather popular, and in this case so some people don’t like the comment, correspondingly it is heavily “down voted”.
Juan Weisz added a reply
Perhaps vacuum does not collapse,
but you know the saying, nature abhors vacuum.
Harri Shore added a reply
False vacuum collapse is a theoretical concept in particle physics and cosmology. It suggests that our universe might currently exist in a metastable vacuum state, also known as a false vacuum. If this false vacuum were to collapse to a lower energy state, it could trigger catastrophic consequences, such as the destruction of all matter and the laws of physics as we know them. This hypothetical scenario is based on certain models in quantum field theory and the structure of the universe. However, there is currently no empirical evidence to support the occurrence of false vacuum collapse.
Harri Shore added a reply:
The "false vacuum collapse" refers to a hypothetical cosmic event that could have catastrophic implications for the universe as we know it. In theoretical physics, a vacuum state is considered to be the lowest possible energy state in which a quantum field can exist. A "true vacuum" is the absolute lowest energy state, while a "false vacuum" is a local minimum that is not the absolute lowest. The concept of a false vacuum collapse is based on the idea that if our universe currently exists in a false vacuum state, it is not truly stable but only metastable. This means there's a possibility, however minute, that a transition could occur, causing the universe to "fall" into the true vacuum state. Such a transition would propagate through space at the speed of light and fundamentally alter the laws of physics, potentially obliterating all structures in the universe as it goes.This transition could be triggered spontaneously due to quantum fluctuations or by a high-energy event. Once started, it would create a bubble of true vacuum that expands in all directions, converting the false vacuum into the true vacuum.Despite its dramatic implications, it's important to note that this is a highly speculative hypothesis and currently there is no experimental evidence to suggest that our universe is in a false vacuum state. Additionally, even if it were true, the odds of such an event happening within our lifetimes—or within the lifespan of the universe as it has existed so far—are exceedingly low.
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Answer
My dear Sergey Shevchenko
Emeritus doctor at the Institute of Physics of the National Academy of Sciences of Ukraine
Ukraine
Hello and thank you very much for your courtesy and respect. Abbas
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What is a phenomenon called "false vacuum collapse"?
as you know :
Mean field energy and bubble formation. The cloud is initially prepared in FV with all atoms in |↑⟩ (A). Although the single spin mode |↓⟩ is lower in energy in the center of the cloud (E↓E↑), the opposite is true in the low-density tails. The interface (domain wall) between ferromagnetic regions with opposite magnetism has positive (kinetic) energy, which is added to the minimum double energy resulting from ferromagnetic interaction. Macroscopic tunneling can occur resonantly in the bubble mode (B), which has a |↓⟩ bubble in the center. The increase in core energy compensates for the cost of domain-wall energy. Crossing the barrier can be caused by quantum fluctuations at zero temperature (full arrow) or by thermal fluctuations at finite temperature (empty arrow). After the tunneling process, the bubble size increases in the presence of dissipation to reach the true vacuum (TV) state (C), without returning to (A). Credit: Nature Physics (2024). DOI: 10.1038/s41567-023-02345-4
An experiment carried out in Italy with theoretical support from the University of Newcastle provided the first experimental evidence of vacuum decay.
In quantum field theory, when a not-so-stable state becomes a true stable state, it is called a "pseudovacuum collapse." This happens through the creation of small local bubbles. While existing theoretical work can predict how often this bubble formation occurs, there is not much empirical evidence.
The Pitaevskii Center for Supercold Atoms Laboratory for the Bose-Einstein Condensation in Trento reports for the first time observations of phenomena related to the stability of our universe. The results are the result of a collaboration between the University of Newcastle, the National Institute of Optics CNR, the Department of Physics at the University of Trento and TIFFA-INFEN and are published in Nature Physics.
The results are supported by theoretical simulations and numerical models, confirming the origin of the decay quantum field and its thermal activation, and opening the way to simulate out-of-equilibrium quantum field phenomena in atomic systems.
This experiment uses a supercooled gas at a temperature less than one microkelvin from absolute zero. At this temperature, the bubbles appear as the vacuum collapses, and Newcastle University's Professor Ian Moss and Dr Tom Billam were able to conclusively show that the bubbles are the result of heat-activated vacuum collapse.
Ian Moss, Professor of Theoretical Cosmology at Newcastle University's School of Mathematics, Statistics and Physics, said: "Vacuum collapse is thought to play a central role in the creation of space, time and matter in the Big Bang, but so far it has not. In particle physics, the decay of the Higgs boson vacuum changes the laws of physics and creates what has been described as the 'ultimate ecological catastrophe'."
Dr Tom Bilam, Senior Lecturer in Applied/Quantum Mathematics, added: "Using the power of ultracold atom experiments to simulate analogues of quantum physics in other systems – in this case the early universe itself – is a very exciting area of research. the moment."
This research opens new avenues in understanding the early universe as well as ferromagnetic quantum phase transitions.
This groundbreaking experiment is only the first step in the discovery of vacuum decay. The ultimate goal is to find vacuum decay at absolute zero temperature, where the process is driven solely by quantum vacuum fluctuations. An experiment in Cambridge, supported by Newcastle as part of the national QSimFP collaboration, is doing just that.
Stam Nicolis added a reply:
Just what the name says: There are many physical systems, whose potential energy, in the absence of fluctuations, possesses more than one minima. If these minima are not degenerate, it can occur that one is the absolute minimum, however, due to the choice of initial conditions, the system is found in another minimum. In the absence of fluctuations, it will stay in the potential well of that minimum.
In the presence of fluctuations, it can occur that the relative minimum is no longer a minimum: In that case the system won't stay there forever and it is possible to compute the rate at which it will evolve to another state.
While the presence of fluctuations is a necessary condition, it isn't sufficient for transitions to be possible.
Sergey Shevchenko added a reply:
What is a phenomenon called "false vacuum collapse"?”
- the answer to this question is: the question really is absurdity, since really there cannot be fundamentally any “false vacuum”, i.e. that really is an fundamental absurdity, and so its “collapse” is absurdity as well.
Though yeah, in mainstream physics really rather numerous fantastic/mystic “true/false vacuums” really exist, and corresponding publications, where corresponding fantastic/mystic properties and effects of/in the vacuums are “discovered”, are well popular and numerous.
That exists in the mainstream completely logically inevitably from the fact that in the mainstream all really fundamental phenomena/notions, first of all on this case “Matter”– and so everything in Matter, i.e. “particles”, “fundamental Nature forces” – and so “fields”, etc., including “vacuum”, “Consciousness”, “Space”, “Time”, “Energy”, “Information”, are fundamentally completely transcendent/uncertain/irrational,
- and so in every case when the mainstream addresses to something that is really fundamental, the results completely inevitably are only some the fantasies.
More see recent SS post in https://www.researchgate.net/post/What_is_a_super_vacuum_Is_the_earth_in_a_vacuum_And_what_is_dark_energy , and links in the post; reDzennn comment, 9/8 [because of too active moderator] passages, to a Nature Physics (2024) paper in
Zoltan Vilagosh added a reply:
Not that complicated really. False vacuum example = because you cannot see over the hill, you think are at the lowest level possible. This makes you think you have no potential energy left. But a surprise awaits if you make it to the top of the hill...you tumble lower onto the vast endless plain on the other side.
__/\O/\
\
\__O
Sergey Shevchenko added a reply:
“…Not that complicated really. False vacuum example = because you cannot see over the hill, you think are at the lowest level possible. This makes you think you have no potential energy left. But a surprise awaits if you make it to the top of the hill...you tumble lower onto the vast endless plain on the other side. …..”
- that above looks as tooo not complicated passage really, though, again, on such level the authors of the paper in a top physical Nature Physics (2024) journal also thought,
- which “discovered” “false vacuum bubbles decays” in some Bose-Einstein Cond sate of Na-23 atoms, more see reDzennn comment, 8 passages, in https://phys.org/news/2024-01-phenomenon-false-vacuum-decay.html, the strangely removed by moderator passage is in the end of whole comments series.
Though yeah, the really full stop “false vacuum” theories are rather popular in mainstream physics, including rather popular is the theory that Matter was created soon 14 billion years ago at some “bubble in spacetime decay”. Thank heavens till now no any even small bubbles didn’t decay near Earth, and nowhere in Space at all, in last 10 billion of years Milky Way existence.
However, again, this full stop – and so quite easily composed - fantasies are so rather popular, and in this case so some people don’t like the comment, correspondingly it is heavily “down voted”.
Relevant answer
Answer
My dear Sergey Shevchenko
Emeritus doctor at the Institute of Physics of the National Academy of Sciences of Ukraine
Ukraine
Hello and thank you very much for your courtesy and respect. Abbas
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How can we improve computer-brain interfaces for broader and safer use in medicine, research, and daily life?
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Improving computer-brain interfaces (CBIs) for broader and safer use in medicine, research, and daily life requires advancements in several key areas. Here are some strategies to enhance CBIs:
  1. Biocompatibility and Safety: Develop CBIs with materials and components that are biocompatible and pose minimal risk of tissue damage or immune response. This involves research into novel materials, coatings, and fabrication techniques to ensure safe and long-term integration with the brain.
  2. Minimally Invasive Techniques: Explore minimally invasive approaches for implanting CBIs, such as flexible electrodes, micro-scale devices, or non-invasive methods like transcranial magnetic stimulation (TMS) or electroencephalography (EEG). Minimizing tissue damage and surgical trauma can improve patient outcomes and acceptance of CBIs.
  3. High Spatial and Temporal Resolution: Enhance the spatial and temporal resolution of CBIs to enable precise and real-time monitoring and modulation of brain activity. This involves advancements in electrode design, signal processing algorithms, and imaging technologies to capture neural activity with high fidelity.
  4. Closed-Loop Systems: Develop closed-loop CBIs that can dynamically adapt stimulation parameters or therapeutic interventions based on real-time feedback from neural signals. Closed-loop systems can optimize treatment efficacy, minimize side effects, and improve patient outcomes in conditions such as epilepsy, Parkinson's disease, and chronic pain.
  5. Wireless and Wearable Interfaces: Design wireless and wearable CBIs that offer convenience, portability, and ease of use for patients and researchers. Wireless interfaces eliminate the need for cumbersome cables and connectors, enabling greater mobility and flexibility in clinical and research settings.
  6. User-Friendly Interfaces: Create user-friendly interfaces and software tools that simplify interaction with CBIs for both clinicians and end-users. Intuitive control interfaces, visualization tools, and personalized settings can enhance usability and acceptance of CBIs in daily life.
  7. Ethical and Regulatory Frameworks: Establish robust ethical and regulatory frameworks to govern the development, deployment, and use of CBIs, addressing privacy, consent, data security, and potential risks associated with brain-computer communication and manipulation.
  8. Interdisciplinary Collaboration: Foster collaboration between neuroscientists, engineers, clinicians, ethicists, and end-users to address the multifaceted challenges of CBIs. Interdisciplinary research and innovation can drive breakthroughs in technology, neuroscience, and healthcare delivery, accelerating the translation of CBIs into clinical practice and everyday life.
By addressing these considerations, we can advance the development and adoption of CBIs for a wide range of applications, including medical diagnostics, therapeutic interventions, assistive technologies, and cognitive enhancement.
Please follow me if it's helpful. All the very best. Regards, Safiul
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How to switch to the Ukrainian language of the interface of this site?
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How to switch to the Ukrainian language of the interface of this site?
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Abstract
This research proposal outlines an experimental framework designed to explore the gravitational redshift within the microtubules of neurons. Building on principles derived from atomic physics and quantum mechanics, we aim to bridge the gap between quantum phenomena and biological systems, offering insights into the fundamental nature of gravity's influence on biological structures at the quantum level.
The gravitational redshift is observed in samples as small as one millimeter.1 Gravitational redshift is a phenomenon predicted by the theory of General Relativity. It occurs when light or other electromagnetic radiation emitted from an object in a strong gravitational field is increased in wavelength, or redshifted, as it climbs out of the gravitational well. This effect is observed because, according to General Relativity, the presence of mass curves spacetime, and the path of light follows this curvature. The energy of the light decreases (which corresponds to an increase in wavelength) as it moves away from the source of gravity. This is because, in a gravitational field, time runs more slowly closer to the source of the field. As light moves away from such a source, its frequency appears to decrease to an observer located at a higher gravitational potential. This decrease in frequency translates to a shift toward the red end of the electromagnetic spectrum, hence the term "gravitational redshift."
The magnitude of the gravitational redshift depends on the strength of the gravitational field through which the light is traveling. The stronger the gravitational field (i.e., the closer to a massive body like a planet, star, or black hole), the more significant the redshift. Gravitational redshift has been observed in various astrophysical contexts, including the light coming from the surface of white dwarfs and neutron stars, and it serves as a crucial test for the theories of gravity.
Researching gravitational redshift in neuron microtubules would involve exploring whether gravitational effects within the brain, particularly within microtubules, could influence quantum states in a way that contributes to consciousness or cognitive processes.
Roger Penrose, a mathematical physicist, suggested that quantum gravity could play a role in the collapse of the quantum wave function. In traditional quantum mechanics, the wave function describes a superposition of all possible states of a system. This wave function collapses to a single outcome when observed. Penrose hypothesized that this collapse is not merely a result of observation (as traditionally thought) but can occur spontaneously due to gravitational effects. According to Penrose, when a quantum system reaches a certain level of mass-energy difference between its possible states, the gravitational difference becomes significant enough to cause the system to "choose" a state in a process called "objective reduction" (OR), without the need for an external observer.
This would require linking the microscopic quantum gravitational effects predicted by Penrose23 with the biological structures and functions identified by Hameroff4, an ambitious and highly theoretical endeavor that would bridge physics, neuroscience, and the study of consciousness.
The Orch OR theory is highly speculative and has been met with skepticism by many in the scientific community. One of the main criticisms is the lack of empirical evidence supporting coherent quantum states within the warm, wet environment of the brain, which many argue would lead to rapid decoherence of quantum states.
But that all seemed to change with the results of a recent study where, Polyatomic time crystals of the brain neuron extracted microtubule are projected like a hologram meters away.5
The role of gravitational effects in brain function, particularly in wave function collapse, remains a controversial proposition.
Research Proposal:
Investigating Gravitational Redshift in Neuronal Microtubules
Recent advancements in quantum physics have enabled the precise measurement of gravitational effects on atomic scales, as demonstrated by experiments measuring the gravitational redshift across millimeter-scale atomic samples. Extending these principles to biological systems, particularly neuronal microtubules, presents a novel approach to understanding the intersection of gravity, quantum mechanics, and biology.
Objectives
  • To develop an experimental setup capable of isolating and stabilizing neuronal microtubules in a controlled environment.
  • To measure the gravitational redshift within these microtubules by detecting shifts in their vibrational frequencies.
  • To analyze the implications of gravitational effects on quantum biological processes.
Methodology
1. Sample Preparation: Neurons will be prepared to isolate microtubules, maintaining their structural integrity.
2. Isolation Mechanism: Utilize magnetic or optical tweezers to stabilize microtubules in a controlled quantum state.
3. Frequency Measurement: Employ advanced spectroscopic techniques to detect minute changes in the vibrational frequencies of microtubules, indicative of gravitational redshift.
4. Data Analysis: Use computational models to analyze frequency shift data, comparing observed effects with theoretical predictions.
Equipment and Tools
  • Magnetic/optical tweezers for microtubule stabilization
  • High-precision spectroscopy equipment for frequency measurement
  • Computational resources for data analysis and modeling
Expected Outcomes
The successful execution of this proposal is expected to provide the first measurements of gravitational effects within biological structures at the quantum level, potentially unveiling new insights into the role of gravity in biological processes and quantum biology.
Budget and Timeline
A detailed budget and timeline will be developed, encompassing equipment acquisition, experimental setup, data collection, and analysis phases, projected to span over three years.
Initial Lab Hardware
For your research proposal aiming to measure gravitational redshifts within neuronal microtubules, you would need to integrate advanced optical and magnetic tweezers technologies. These tools are crucial for manipulating and measuring the quantum mechanical properties of microtubules with the precision required to detect such subtle phenomena.
Optical Tweezers
C-Trap® Optical Tweezers: Offered by LUMICKS, these are dynamic single-molecule microscopes that allow for simultaneous manipulation and visualization of single-molecule interactions in real-time. They combine high-resolution optical tweezers with fluorescence and label-free microscopy, integrating an advanced microfluidics system for a comprehensive solution to study molecular dynamics.
Modular Optical Tweezers from Thorlabs: This system provides a tool for trapping and manipulating microscopic-sized objects with a laser-based trap. It includes a high-precision 100X oil immersion objective lens and a 10X air condenser, making it suitable for a range of biological experiments. The system features adjustable force and spot size settings, ensuring precise control over the manipulation of microtubules.
Magnetic Tweezers
Magnetic Tweezers Technology: According to information from Frontiers in Physics, magnetic tweezers are capable of applying forces up to about 20 pN at distances of about 1 mm, using NdFeB magnets and standard beads. This force is sufficient for many single-molecule applications. Magnetic tweezers technology also includes electromagnetic tweezers, which offer efficient feedback loops for stable force clamps and the ability to modulate the strength and direction of the magnetic field with electric current.
Bead Tracking and Force Calibration: Critical for magnetic tweezers, bead tracking in 3D space and force calibration are essential techniques for precise measurements. The technology employs computer programs to track the bead in real-time and uses DNA attachment methods for single-molecule studies, ensuring accurate and reliable data collection.
Acquisition Sources
  • LUMICKS: For purchasing C-Trap® Optical Tweezers, you can directly contact LUMICKS, as they provide detailed product specifications and support for their integrated systems.
  • Thorlabs: The Modular Optical Tweezers system can be acquired from Thorlabs, which offers detailed product descriptions and technical specifications online, allowing for customization based on specific research needs.
These tools, combined with your innovative experimental design, aim to unlock new insights into the quantum biological processes within neurons, potentially revolutionizing our understanding of the interplay between gravitational forces and biological structures at the quantum level.
This research has the potential to fundamentally alter our understanding of the interface between gravity, quantum mechanics, and biology, opening new avenues for interdisciplinary research and technological innovation.
If I may add, footnotes for this question: 1
Bothwell, T., Kennedy, C.J., Aeppli, A., et al. (2022). Resolving the gravitational redshift across a millimetre-scale atomic sample. *Nature*, 602, 420–424. https://doi.org/10.1038/s41586-021-04349-7
2
Penrose, Roger. The Emperor's New Mind: Concerning Computers, Minds, and The Laws of Physics. Oxford University Press, 1989. This book presents Penrose's early thoughts on the connection between quantum mechanics, consciousness, and the role of gravity in the wave function collapse, introducing the idea that physical processes could influence consciousness.
3
Penrose, Roger. Shadows of the Mind: A Search for the Missing Science of Consciousness. Oxford University Press, 1994. In this follow-up, Penrose delves deeper into the theory that quantum mechanics plays a role in human consciousness, further developing his hypothesis on objective reduction (OR) and its gravitational basis.
4
Hameroff, Stuart, and Penrose, Roger. "After 20 years of skeptical criticism, the evidence now clearly supports Orch OR." *ScienceDaily*, 2014. https://www.sciencedaily.com/releases/2014/01/140116085105.htm
5
Saxena, Komal, Singh, Pushpendra, Sarkar, Jhimli, Sahoo, Pathik, Ghosh, Subrata, Krishnananda, Soami Daya, and Bandyopadhyay, Anirban. "Polyatomic time crystals of the brain neuron extracted microtubule are projected like a hologram meters away." *Journal of Applied Physics*, vol. 132, no. 19, 194401, Nov. 2022. [https://doi.org/10.1063/5.0130618]
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yes, they observed the gravitational effect inside the proton
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i am trying to make a GUI interface for my modelings but a syntax error are emerged.
how can i solve this error?
GUI codes are attached...
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have you found the solution of it
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How can one model explosion in a nuclear power plant using comsol multiphysics software? which physics interface are appropriate? which study can be used?
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The explosion usually occurs mainly due to hydrogen build-up if the excess heat is not removed via the cooling water. You need to model the process of dissociation of H20 into H2+02 and then estimate the pressure developed inside the dome of the plant. Suppose this pressure exceeds the yield limit of the material. You may assume it has failed. i.e. (exploded, cracked). This is a fundamental approach that you can build on by adding complexities at later stages.
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In a well-built apartment building, each apartment has its own walls, and there is an air gap between the walls of adjacent apartments, which provides excellent sound isolation. Could a similar concept provide high-performance thermal insulation?
In general, the thermal resistance of a material interface seems to be viewed as a problem to overcome, rather than an opportunity to create a better insulator (see, eg., https://en.wikipedia.org/wiki/Interfacial_thermal_resistance ). So perhaps it is possible to construct a laminar material that uses inter-laminae thermal impedance to create an extremely high resistance to heat conduction.
As the simplest example of this idea, consider a sheet of material that is composed of a large number of alternating layers of materials A and B. Each of these materials consists of atoms of a single element, and at least one of them is not electrically conductive. Material A has relatively heavy atoms and relatively weak (soft) interatomic bonds; material B has relatively light atoms and relatively strong (stiff) interatomic bonds. The natural modes of vibration in material A have much longer periods than those in B. Thermal vibrations in B layers should essentially reflect off the B/A interface. And, provided that the B layers are not too thin, thermal vibrations in A layers that pass across an A/B interface should largely dissipate into B-style vibrations before reaching the next A layer.
Is it possible to design and fabricate sheets of insulating material, based on this concept, that have exceptionally low thermal conductivity?
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Space shuttles are much easier to insulate thermally than buildings, since they are in the vacuum, where radiation is the only process available to transfer heat. therefore, a low emisivity (or high reflectivity) material at wavelenght corresponding to the surface temperature is very efficient. If not enough, because the outdoor temperature can be about 3 K , a layer of insulating material can be added. Since that material is under vacuum, it is about ten times more efficient than at atmospheric pressure.
So called vacuum insulation materials are available on the market, but, in my opinion, they cannot be used in the building industry, since much care is necessary when handling these materials. They cannot be cut, pierced, nailed.
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what we are working on is studying the friction between two concrete blocks
the bottom one is fixed and the top one is moving back and forth
in the experiments the concrete is deteriorating and the friction is decreasing
how I can model that in software
I tried in Ansys but the material is not deteriorating
I also tried to model it using Movable Cellular automata but I don't know how I will apply rules between the cells
Any Suggestions??
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To model friction between two concrete surfaces, we can use the Coulomb friction model. This model assumes that the friction force is proportional to the normal force between the surfaces, with a coefficient of friction μ. The friction force (F_friction) can be calculated using the formula
(F)friction = μ*( F)normal
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Dear CFD Community,
I'm stuck with a meshing challenge in ICEM CFD and hoping someone can point me in the right direction. My model involves two fluid zones:
  • Preheat Zone: Where the fluid enters the system.
  • Reactor Zone: Where the fluid is heated to a specific temperature.
These zones are connected, and the fluid needs to flow seamlessly from one to the other. However, I'm having trouble creating the interface between them in ICEM CFD.
I've made many attempts by trying to merge the interface of the two zones, but I keep encountering problems in achieving the successful merging of the two zones.
I'd be incredibly grateful if anyone could offer insights or solutions to help me overcome this hurdle. Any advice on:
  • Recommended workflow for connecting fluid zones in ICEM CFD.
  • Specific settings or options for interface creation relevant to my scenario.
  • Troubleshooting tips for common errors encountered with fluid zone interfaces.
I've attached a brief visualization of the geometry, to provide further context.
Thank you in advance for your time and expertise!
Sincerely,
Sudeep N S
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Actually, it depends on the kind of mesh you want to create: unstructured or structured. Because of the simplicity of the geometry I recommend the structured type. At the beginning, suppose that there are just one zone and create an O-Grid type for the whole geometry and do all the association processes. In the end, just split the block in the separation point and then associate the faces of blocks to the surfaces of the geometry. Note that you have just one surface between the two zones you can name it interior. Because of all mesh elements are coincident you can give it the interior boundary condition and so the precision of your simulation will be higher than the interface boundary type. You can see some useful tutorial videos in my youtube channel "infinitycfd" with this link:
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Hi, our team is currently exploring research opportunities regarding visualization tools for computational materials design of inorganic crystal structures. I am writing to ask what features people would like to have for such an interface?
I image such an interface to be something like we start with a chemical composition and we will see the stable phases and corresponding crystal structures. It would also be good if we can know the predicted properties of interest as well as how the structures can be related to the properties. Any thoughts/comments are welcome and appreciated. Thank you.
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Cheng Zeng I can share my thoughts and experiences to help you and your team in this journey. To make it accessible and engaging, let's break down the key aspects of your proposed interface and discuss them one by one.
  1. Chemical Composition Entry: Imagine this as the starting point. It's like entering the ingredients for a recipe. Users should be able to input the elements they want to work with, just like writing down the recipe for a dish.
  2. Stable Phases Visualization: Once the composition is entered, the interface should display the possible stable phases. Think of this as different recipes that can be created with the same ingredients. Users can visualize the various forms that these materials can take.
  3. Crystal Structures Exploration: Here, users should be able to delve deeper into each stable phase. It's like exploring the details of a dish in a recipe book. Users can rotate, zoom in, and inspect the crystal structures to understand their geometry.
  4. Predicted Properties: Just as a recipe book may provide nutritional information, your interface should offer predicted properties. Users should be able to see the characteristics and behavior of these materials. This is like knowing how a dish tastes and its nutritional value.
  5. Relationship Between Structure and Properties: This is the magic part. Users should be able to link the crystal structures to the properties. Think of it as understanding why certain ingredients and cooking methods result in a particular taste. In your case, why a specific crystal structure exhibits certain properties.
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The current RANS turbulence model requires a Reciprocal Wall Distance variable.
Make sure that all the study steps solving for the flow variables in this physics interface get their initial values of variables not solved for from a study step that has already computed the corresponding Reciprocal Wall Distance variable.
- Node: Turbulent Flow, SST (spf)
thanks in advance
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If you encounter the mentioned error in COMSOL Multiphysics with a RANS turbulence model, ensure proper initialization of the Reciprocal Wall Distance variable in study steps. Confirm correct settings for turbulence model and wall treatment, validate boundary conditions, and check solver settings. Consult COMSOL documentation for model-specific guidance. If issues persist, contact COMSOL support for assistance. Review and ensure proper definition and initialization of all required variables in accordance with RANS turbulence model requirements.
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Im having issue interfacing ad4111 with esp32 microcontroller however i tried sending spi commands directly to the ad4111 but. there is something im missing. if anyone have already worked with it or have any idea would help alot.
Command Sequence will be more helpful.
#embedded_systems #ADC #electronics #SPI
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See electronics.foxping. com -> 5.12 Electronic SPI Serial Communication (YouTube video clip) for details about SPI communication.
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Dear All,
I trying to model heterointerface between two oxides, at first I modeled each surface oxide alone and then I tried to attached OH, O, OOH molecule to find Gibbs free energy. My problem occur when I tried to model the heterointerface. I built my structure using vesta by importing the first unit cell of oxide and enlarge the cell in X and Y direction to fit with the other unit cell of the oxide. I found this procedure is done in some paper to match both lattice parameter. When optimized the oxide alone, the relaxation was not that hard, but when I had an interface between two oxides, the relaxation distort the structure.
I am seeking help in making better structure and relaxation.
This calculation was very costly and I do not want to lose core-hour in the supercomputer.
I appreciate your advice
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Dear Z. Albu, can you share the link on the paper you publishe ? Thank's a lot!
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dear friends
I was trying to study problems with finite friction involving indentation of a thin layer bonded on a substrate. As you can see from the theory
there are large differences between frictionless and infinite friction cases both at punch/layer and layer/substrate interface. However, particularly for incompressible materials, in ANSYS the contact results with finite friction are unreliable and I gave up in trying to setup contact stiffness parameters to find reasonable results --- here we know analytically some limit behaviour for frictionless and very high friction results, so we can check the intermediate case.
Do you think other FEM code could do better? To setup the mesh for the flat punch is extremely simple, so we could try with your help in other codes.
thanks
Mike
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in order to insert the friction please change the contact171 element to contact 172 in the code I sent. The friction properties can be assigned using the command TB. Please refer to the ansys help for more details or use the following link
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When I simulate GaN Transistor, and define the interfaces, s-device simulation fails giving the following message in the log file:
"Turning on fermi and thermionic (TE) should also specify the keyword 'formula=1' in the 'thermionicemission' section of the parameter file, otherwise results can be wrong in higher carrier density cases. in the future, the corrected fermi TE model (formula=1) will become default when using fermi statistics and users are urged to switch to the corrected fermi te model as soon as possible. !"
It also gives "Newton didn't converge. step size is less than min-step" in the (.out file).
Why it fails? is it a mesh problem or the parameter file has a problem ?
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Hi Bassant
1- you should specify in parameter file:
ThermionicEmission {
Formula=1
}
or Formula =2 check in sdevice Manual for your material used !
do you now how to edit the parameter file?
2- for the convergence problem :
try to use a small Minstep => 1e-15 for exemple
Good luck
Younes
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Generally, interface polarization disappears at MHz, but why do many literature test frequencies in GHz but interface polarization occurs?
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Yüzeyde frekansın yüksek olması polarizasyonun oluşmasına, polarizasyonun oluşması arayüz oluşumuna neden olur.
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Hey folks!
I'm using TNT version 1.6 for MAC but I can't open my matrix because of this message: "error parsing instructions from graphic interface". I tried to reinstall the software, but it didn't work. Does anyone have an idea what's happening?
Cheers!
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This tends to be a generalized error message in many software applications pertaining to the GUI interface. However, each software application is precise about when it generates this error. Try sending a "Bug Report" here: https://www.lillo.org.ar/phylogeny/tnt/
Saludos!
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I implemented trap on the drift layer of diode with Sentaurus TCAD simulation (it is bulk trap, not interface). How can I measure the concentration of the implemented trap?
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plot and add etrapcharge htrapcharge and go tdr file then you can see
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How can I effectively model the interface between two sequentially cast layers of Normal concrete in Abaqus, where the first layer (20cm thick) is cast, and the second layer (5cm thick) is poured within an hour before the initial setting of the first layer? Additionally, should I simulate stages of curing and hardening for the Normal concrete material, or is it sufficient to address this through material interaction modelling?
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Ahmad Al-shiekh, you do not need to simulate stages of curing and hardening for the Normal concrete material if you are only interested in the behavior of the concrete at a specific point in time, especially when it is hardened concrete. In this case, it is sufficient to address this through material interaction modeling. To effectively model the interface between two sequentially cast layers of normal concrete in Abaqus, you can use the following steps:
  • Create a surface element set for each of the two concrete layers.
  • Define a surface-based cohesive behavior for the interface. This can be done by specifying the tensile strength, shear strength, and fracture energy of the interface.
  • Assign the surface-based cohesive behavior to the surface element sets for the two concrete layers.
  • Define a contact interaction between the two concrete layers. This should be a contact with adhesion, and you should specify the same surface element sets for the master and slave surfaces.
  • Set the friction coefficient between the two concrete layers to a value that is appropriate for the interface condition.
  • Simulate it and you are done.
I hope it helps. If you are facing any difficulties, let me know on my WA; https://wa.me/+923440907874.
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Dear All, I am trying to run the VUMAT-UMAT interface provided on soilmodel.com (https://soilmodels.com/download/vumat_umatinterface-zip/) with the Sand Hypoplasticity. However, when I run the simulation Abaqus returns the following error: “Problem during linking – Single Precision Abaqus/Explicit User Subroutines. This error may be due to a mismatch in the Abaqus user subroutine argument”. The versions of the programs that I am using are: Abaqus 2020, the Visual Studio 2019, and OneAPI compiler v2022. When I run the Abaqus verification, it says PASS for everything (also subroutines), so I assume they are correctly linked. Someone had the same problem and knows how to solve it?
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How can I know if it is correctly linked?
When I run the Abaqus verification, it says PASS for everything, also for subroutines
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Best regard,
I get an error when I try to compile the * .sln file in VS 2019, after being generated by the Cmake interface.
My error output is:
"Compile operation started: project: release-version-info, configuration: Debug x64 ------
1> Generating release version information
1> - The source code for this GROMACS installation is different from the officially released version.
2> ------ Compile operation started: project: libgromacs, configuration: Debug x64 ------
2> Building NVCC (Device) object src / gromacs / CMakeFiles / libgromacs.dir / nbnxm / cuda / Debug / libgromacs_generated_nbnxm_cuda.cu.obj
2> nvcc fatal: Unknown option '-std: c ++ 17'
2> CMake Error at libgromacs_generated_nbnxm_cuda.cu.obj.Debug.cmake: 224 (message):
2> Error generating
2> C: /Users/USUARIO/Downloads/gromacs-2021.2/build/src/gromacs/CMakeFiles/libgromacs.dir/nbnxm/cuda/Debug/libgromacs_generated_nbnxm_cuda.cu.obj
2>
2>
2> C: \ Program Files (x86) \ Microsoft Visual Studio \ 2019 \ Community \ MSBuild \ Microsoft \ VC \ v160 \ Microsoft.CppCommon.targets (241.5): error MSB8066: Custom build of "C: \ Users \ USER \ Downloads \ gromacs-2021.2 \ src \ gromacs \ nbnxm \ cuda \ nbnxm_cuda.cu; C: \ Users \ USER \ Downloads \ gromacs-2021.2 \ src \ gromacs \ nbnxm \ cuda \ nbnxm_cuda_data_mgmt.cu; C: \ Users \ USER \ Downloads \ gromacs-2021.2 \ src \ gromacs \ nbnxm \ cuda \ nbnxm_cuda_kernel_F_noprune.cu; C: \ Users \ USER \ Downloads \ gromacs-2021.2 \ src \ gromacs \ nbnxm \ cuda \ nbnxm_cuda_kernel_F: USER \ Downloads \ gromacs-2021.2 \ src \ gromacs \ nbnxm \ cuda \ nbnxm_cuda_kernel_VF_noprune.cu; C: \ Users \ USER \ Downloads \ gromacs-2021.2 \ src \ gromacs \ nbnxm \ cuda \ nbnxm_cuda_prune_cu; C: USER \ Downloads \ gromacs-2021.2 \ src \ gromacs \ nbnxm \ cuda \ nbnxm_cuda_kernel_pruneonly.cu; C: \ Users \ USER \ Downloads \ gromacs-2021.2 \ src \ gromacs \ domdec \ gpuhaloexchange_impl.cu; C: \ Users \ USUARIO Downloads \ gromacs-2021.2 \ src \ gromacs \ utility \ cuda_version_information.cu; C: \ Users \ USER \ Downloads \ gromacs-2021.2 \ src \ gromacs \ mdlib \ leapfrog_gpu.cu; C: \ Users \ USER \ Downloads \ gromacs-2021.2 \ src \ gromacs \ mdlib \ lincs_gpu.cu; C: \ Users \ USUARIO \ Downloads \ gromacs-2021.2 \ src \ gromacs \ mdlib \ settle_gpu.cu; C: \ Users \ USER \ Downloads \ gromacs-2021.2 \ src \ gromacs \ mdlib \ update_constrain_gpu_impl.cu; C: \ Users \ USER \ Downloads \ gromacs-2021.2 \ src \ gromacs \ mdlib \ gpuforcereduction_impl.cu; C: \ Users \ USER \ Downloads \ gromacs-2021.2 \ src \ gromacs \ listed_forces \ gpubonded_impl.cu; C: \ Users \ USUARIO \ Downloads \ gromacs-2021.2 \ src \ gromacs \ listed_forces \ gpubondedkernels.cu; C: \ Users \ USER \ Downloads \ gromacs-2021.2 \ src \ gromacs \ nbnxm \ nbnxm_gpu_data_mgmt.cpp; C: \ Users \ USER \ Downloads \ gromacs-2021.2 \ src \ gromacs \ ewald \ pme_ .cu; C: \ Users \ USUARIO \ Downloads \ gromacs-2021.2 \ src \ gromacs \ ewald \ pme_gpu_3dfft.cu; C: \ Users \ USUARIO \ Downloads \ gromacs-2021.2 \ src \ gromacs \ ewald \ pme_solve.cu; C : \ Users \ USER \ Downloads \ gromacs-2021.2 \ src \ gromacs \ ewald \ pme_spread.cu; C: \ Users \ USER \ Downloads \ gromacs-2021.2 \ src \ gromacs \ ewald \ pme_gpu_program_impl.cu; C: \ Users \ USER \ Downloads \ gromacs-2021.2 \ src \ gromacs \ ewald \ pme_pp_comm_gpu_impl.cu; C: \ Users \ USER \ Downloads \ gromacs-2021.2 \ src \ gromacs \ ewald \ pmeg_force_force_sender. cu; C: \ Users \ USER \ Downloads \ gromacs-2021.2 \ src \ gromacs \ ewald \ pme_coordinate_receiver_gpu_impl.cu; C: \ Users \ USER \ Downloads \ gromacs-2021.2 \ src \ gromacs \ ewald \ pme_gpu_internal.cpp; C: \ Users \ USER \ Downloads \ gromacs-2021.2 \ src \ gromacs \ ewald \ pme_gpu_timings.cpp; C: \ Users \ USER \ Downloads \ gromacs-2021.2 \ src \ gromacs \ gpu_utils \ device_stream_manager.cpp; C: \ Users \ USER \ Downloads \ gromacs-2021.2 \ src \ gromacs \ gpu_utils \ device_stream.cu; C: \ Users \ USER \ Downloads \ gromacs-2021.2 \ src \ gromacs \ gpu_utils \ gpu_utils.cu; C: \ Users \ USER \ Downloads \ gromacs -2021.2 \ src \ gromacs \ gpu_utils \ pinning.cu; C: \ Users \ USER \ Downloads \ gromacs-2021.2 \ src \ gromacs \ gpu_utils \ pmalloc_cuda.cu; C: \ Users \ USER \ Downloads \ gromacs-2021.2 \ src \ gromacs \ hardware \ detecthardware.cpp; C: \ Users \ USER \ Downloads \ gromacs-2021.2 \ src \ gromacs \ h ardware \ device_management_common.cpp; C: \ Users \ USER \ Downloads \ gromacs-2021.2 \ src \ gromacs \ hardware \ device_management.cu; C: \ Users \ USER \ Downloads \ gromacs-2021.2 \ src \ gromacs \ mdtypes \ state_propagator_data_gpu_impl. cpp; C: \ Users \ USER \ Downloads \ gromacs-2021.2 \ build \ CMakeFiles \ a9116bcf4bc4115e626ce4c6578cc5c1 \ baseversion-gen.cpp.rule "terminated with code 1.
2> Compilation of project "libgromacs.vcxproj" finished - ERROR.
3> ------ Compile operation started: project: gmx, configuration: Debug x64 ------
3> LINK: fatal error LNK1104: cannot open file '.. \ .. \ lib \ Debug \ gromacs.lib'
3> Compilation of project "gmx.vcxproj" finished - ERROR.
========== Compile: 1 correct, 2 incorrect, 15 updated, 0 skipped ========== ".
I have CUDA 11.4, Win 10 64bit and FFTW 3.3.5 installed. I would be very grateful if you could guide me in solving this error, as I wish to be able to compile on my own any new version of Gromacs on Windows that might be released in the future.
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You can ask always your gromacs -related questions (only) in the GROMACS forum and get your answer directly from gmx experts: https://gromacs.bioexcel.eu/
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A special issue of Nanomaterials (ISSN 2079-4991).
Deadline for manuscript submissions: 20 February 2024
Special Issue Information
Dear Colleagues,
In the face of major national scientific and technological needs, aiming at the national "double carbon" and "rural revitalization" strategic goals, the environmental application and technological innovation breakthrough of new functional engineering nanomaterials for water pollution control is an important scientific and technological guarantee to fight the battle for blue water. It is important to build new methods and principles for the efficient purification of new pollutants based on solar energy and atmospheric oxygen and other green energy sources; to reveal the interaction mechanism of the three elements of process, effectiveness and mechanism of environmental chemistry of new pollutant control; to clarify the influence law and principle of action of interface characteristics and process parameters on the control of new pollutants; to quantitatively establish the structure–effect relationship of the surface interface from the microscopic scale; to solve the bottleneck problems of catalytic activity abatement, selectivity and poor stability; and to form a long-term mechanism of new pollutant treatment.
Dr. Huinan Che Dr. Runren Jiang Guest Editors
Manuscript Submission Information
Manuscripts should be submitted online at www.mdpi.com by registering and logging in to this website. Once you are registered, click here to go to the submission form. Manuscripts can be submitted until the deadline. All submissions that pass pre-check are peer-reviewed. Accepted papers will be published continuously in the journal (as soon as accepted) and will be listed together on the special issue website. Research articles, review articles as well as short communications are invited. For planned papers, a title and short abstract (about 100 words) can be sent to the Editorial Office for announcement on this website.
Submitted manuscripts should not have been published previously, nor be under consideration for publication elsewhere (except conference proceedings papers). All manuscripts are thoroughly refereed through a single-blind peer-review process. A guide for authors and other relevant information for submission of manuscripts is available on the Instructions for Authors page. Nanomaterials is an international peer-reviewed open access semimonthly journal published by MDPI.
Please visit the Instructions for Authors page before submitting a manuscript. The Article Processing Charge (APC) for publication in this open access journal is 2900 CHF (Swiss Francs). Submitted papers should be well formatted and use good English. Authors may use MDPI's English editing service prior to publication or during author revisions.
Keywords
  • environmental applications
  • engineering nanomaterials
  • photocatalytic production
  • degradation of new pollutants
  • water purification
Published Papers
This special issue is now open for submission.
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Nanomaterials is fully open access. Manuscripts are peer-reviewed, and a first decision is given to authors approximately 12.7 days after submission. An article processing charge (APC) of CHF 2900 currently applies to all accepted papers. For further details on the submission process, please see the instructions for authors at the journal website (https://www.mdpi.com/journal/nanomaterials/instructions). Submitted papers should not be under consideration for publication elsewhere.
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Is it just a theoretical concept? If so, how is it modeled? Is it a consequence of poor physical contact?
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Thank you Haseeb Ahmad,
I found another explanation that may be helpful.
A space-charge layer is formed when two materials with different chemical potentials are brought in contact with each other, and the atoms or electrons are unable to migrate to establish local charge neutrality. Near the interface the atoms and electrons are driven toward the material with the lowest chemical potential (highest voltage). But if only one charged species, either electrons or ions, is able to migrate this will create a region in which charge builds up, the so-called space charge interface layer.
Reference:
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How can I calculate normal and shear stiffness of interface between the FRP ,epoxy resin and concrete ?
 I am using DIANA for it. Please suggest me.
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You should also be aware of the failure mode of FRP. the values you are seeking would be important when your failure mode is governed by FRP debonding. If you expect FRP rupture, you can consider as perfect bond (i.e. fixed contact surface) between interface of the FRP, matrix and concrete substrate.
Bests
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I was trying to create a FEM model of an LVI and CAI experiment. For the CAI simulation, the load displacement curve I obtained is way too stiff compared to the experimental result. The maximum compression load is already quite similar with the experiment. Is there parameters that I can change to reduce the compressive stiffness ?
The simulation model was created in the ABAQUS Explicit solver. The composite plate is divided into 16 layers of laminate and 15 layers of interfaces. Each layer of laminate and interface have thickness of 0.215 mm and 0.025 mm respectively. The laminate was meshed with SC8R and use the Hashin damage model. The interface layer is modelles using COH3D8 elements and the QUADS damage criterion and energy based Benzeggah damage evolution.
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Mohamad Khorashad
Here is the comparison between the abaqus and experimental result. I have tried using denser and coarser mesh but the curve gradient does not change. As for the damage, the lvi delamination area is bigger on the simulation, but the peak force is similar as seen in the lvi curve.
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When I used Diana to build a two-dimensional micro-modeling, I did not know where to set the constraint of the boundary interface. There were problems in the properties of the interface materials between each brick and between masonry brick and frame.
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the pdf file do not open and also kindly share the exact tutorial for micro modelling
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Reservoir Engineering
1. Feasible to capture the transition between (a) and (b) @ laboratory-scale?
(a) where, an oil phase gets disconnected into blobs (and remain strongly influenced by local pressure field near a flood front, which mostly remain to be transient - even in a steady-state displacement process); and remain trapped and the way the oil/water menisci gets migrated @ pore-scale;
(b) where, continuous mobility of water/oil/gas phases occur @ macroscopic-scale, where averaged quantities are both interpolated as well as extrapolated?
2. If displacement of oil from water-wet porous sedimentary rock by water-flooding leads to an entrapment of a considerable fraction of oil, then,
would it remain feasible to capture the role of buoyancy and inertial forces in addition to the interplay between capillary and viscous forces @ laboratory-scale?
3. If pore-level displacement is initiated by an externally imposed flow, then, how exactly to capture the complex interplay between local topology and pore-scale geometry with capillarity along with the complex interplay between buoyancy, inertial and viscous forces?
Even, if we manage to capture such complex physics, how could we capture the spontaneous rupture of an oil neck (choke-off) and its associated spontaneous withdrawal of head meniscus out of a pore body @ lab-scale?
4. Can we deduce the details on the length distribution of blobs towards determining the oil recovery efficiency upon mobilizing the entrapped oil blobs by lowering IFT @ lab-scale?
If each curved meniscus supports a difference in oil and water pressure resulting from its associated IFT, then, would it remain feasible to distinguish the interface between oil and water within a water-wet reservoir into zones that consists of a meniscus which essentially obey Young-Laplace equation of capillary hydrostatics; and those zones that connect the menisci (zones of positive/negative Gaussian curvatures associated with the menisci of oil-water interface) @ laboratory-scale?
If so, how exactly the physics of thin films along with capillary hydrostatics will be up-scaled to Darcy-scale?
5. In EOR applications, whether any meniscus would be able to move by spontaneously developing excess capillary pressure that would cause oil to flow?
6. Feasible to ensure that a jump (when a pore body gets evacuated of oil and filled with water) remains more likely to be upstream than downstream, which would make the displacement front more stable, while oil entrapment remaining less frequent @ lab-scale?
7. If displacement of oil or any non-wetting fluid from an initially saturated porous medium by water or any wetting fluid consists of advancement of head menisci (jumps); consequent break-offs and choke-offs of neck menisci; and creation of isolated oil or non-wetting fluid blobs in the process, which remain to be deterministic and reproducible, then, can we replicate the above physics @ lab-scale?
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It is possible to deduce some information about the length distribution of oil blobs entrapped in a porous medium by mobilizing them at the lab-scale using methods such as lowering the interfacial tension (IFT). However, accurately determining the length distribution of these blobs may be challenging and may require additional analysis techniques.
When mobilizing entrapped oil blobs, reducing the IFT can help to reduce capillary forces that hold the blobs in place and allow them to be mobilized more easily. By observing the mobilization process, you can gain insights into the behavior of the oil blobs. However, directly measuring the length distribution of the mobilized blobs can be difficult.
To estimate the length distribution, you may need to employ imaging techniques such as microscopy or advanced imaging methods like X-ray microcomputed tomography (micro-CT). These techniques can provide visual information about the size and shape of the mobilized blobs, allowing you to analyze their length distribution.
Additionally, you can use image analysis software to analyze the obtained images and extract quantitative data on the length distribution of the mobilized blobs. This analysis may involve measuring the length of individual blobs or characterizing the blob population statistically.
Keep in mind that analyzing the length distribution of oil blobs at the lab-scale provides insights into the behavior of entrapped oil in controlled conditions. However, the results may not directly represent the behavior of oil blobs in real-world reservoirs, as they can be influenced by various factors such as rock properties, fluid composition, and reservoir heterogeneity. Therefore, it's important to consider the limitations and assumptions of the lab-scale experiments when interpreting the results and applying them to larger-scale scenarios. (ChatGPT)
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Hi,
I am modeling a reinforced concrete(RC) slab in DIANA FEA.
The RC slab is simply mounted on a steel girder (see config 1) Therefore, there is no bonding between the RC slab and the steel girder. In order to satisfy these interface conditions, it is set as shown in Figure 2. When a vertical downward pressing force (bending stress) from the center of the slab is applied, it is expected that the slab located on the girder will be lifted up (as in the principle of lever). See Fig 3). As expected, the upward displacement of the slab on the girder occurred, but in some sections it appeared as if it had been bonded and no lifting occurred (See Figure 4) Please advise why this is happening and what interface setting should be done.
Thank you.
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Dear Lee,
Could still be lifting up and just a scale issue in the picture. The collor yellow in the picture can be tension or 0. You can output the stress of the interface. stress total tracti to be sure. Or change the legenda with a 0 value in it.
Ab van den Bos
NLyseConsultants.com for all your FEA projects within the built environment.
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For a single layer anti-reflective coating, people generally say if the layer thickness is λ/4, the reflection could reduce and transmission increase.
As the figure, because the light was reflected by second interface and therefore there was additional optical path of λ/2, resulting destructive interference of reflection. Because 1-F(reflection)=T(transmission) ; so T increases.
However, if we think the transmission in the same way. The destructive interference of transmission also happens, doesn't it? How could we say the transmission increase?
If anyone is familiar with anti-reflective coating? Please help me. THANKS!
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You're correct that an anti-reflective coating works by causing destructive interference of reflected light. This process increases the transmission by decreasing the amount of light that is reflected. However, it seems there is a misunderstanding of how this process affects the transmitted light.
When light encounters a boundary between two different materials, some is reflected, and some is transmitted. In the case of an anti-reflective coating, the coating is designed so that the reflected light from the top surface of the coating and the reflected light from the boundary between the coating and the surface beneath it interfere destructively, effectively cancelling each other out. This decreases the amount of reflected light.
This destructive interference of reflected light does not decrease the amount of transmitted light. Rather, it increases it. This is because the total amount of light must be conserved. If less light is being reflected, then more must be transmitted. Therefore, an anti-reflective coating increases the transmission of light through the coated surface by decreasing the reflection.
To address the part about transmission interference: the key here is phase shift upon reflection versus transmission. For normal incidence, there is a phase shift of 180 degrees upon reflection from a medium of higher refractive index, but no phase shift for transmission. Therefore, in the case of an anti-reflective coating, the two reflected waves from the front and back surfaces of the film undergo destructive interference, while the transmitted waves do not. They constructively interfere to give higher transmission.
Hence, it's not quite accurate to say that the transmitted waves destructively interfere in the same way that the reflected waves do, due to the phase shift differences in reflection and transmission. As a result, the transmission of light increases, as less light is reflected away due to the destructive interference occurring with reflection.
The best example of this is eyeglasses with an anti-reflective (AR) coating.
Without an AR coating, light can reflect off the surfaces of the eyeglasses, which can be distracting and reduce the overall clarity of vision. This reflected light can come from any light source, including computer screens, overhead lighting, or sunlight.
When an AR coating is applied to the lenses of the eyeglasses, the coating is engineered to be a quarter of the wavelength of the light to be eliminated. This means that when light hits the lens, it's reflected off both the outer surface of the AR coating and the boundary between the AR coating and the lens surface beneath it. Because of the carefully engineered thickness of the AR coating, these two reflected light waves interfere destructively and cancel each other out, resulting in very little reflected light.
This destructive interference for reflection does not reduce the transmitted light - it increases it. The transmitted light waves do not destructively interfere because of the phase shift differences in reflection and transmission I mentioned in the previous response. So, more light can pass through the lens to the eye, which improves vision clarity and reduces distractions from reflected light.
The outcome is that you get clearer vision with less glare, as more of the light can transmit through the lens, rather than being reflected away.
Another example can be solar panels. Solar panels also use anti-reflective coatings to ensure that as much light as possible is absorbed by the panel and converted into electricity, rather than being reflected away. By minimizing the reflection, the transmission of light into the panel increases, boosting its efficiency.
In both these examples, the principle is the same - the anti-reflective coating reduces the amount of reflected light through destructive interference, which in turn increases the transmission of light.
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Hey there! I would like to conduct an event study with the buy-and-hold approach and that website was suggested to me. It talks about long run event studies but I could not find it on the ARC interface and I was wondering if it is there and I am just missing it. Thank you very much!
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The website Eventstudytools provides tools and resources to conduct event studies, including the BHAR (Buy-and-Hold Abnormal Return) approach. The BHAR approach is commonly used in event studies to calculate abnormal returns over a specific event period.
Eventstudytools is a comprehensive platform that offers a range of functionalities to analyze the impact of events on financial markets. It provides pre-built event study templates, customizable event windows, and statistical tests to measure abnormal returns. These tools can help researchers and analysts assess the significance of events and their impact on stock prices or other financial variables.
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I really need an idea on new work to start.
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I believe there are a lot of potential application areas for 2D materials. At the frontier of the research field, you could try looking at defect engineering in 2D materials e.g graphene, MoS2 for room temperature single photon emission. This I believe have a lot of relevance for future quantum devices. Best of luck.
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Dear colleagues,
We recently purchased a cable to synchronise the different signals from the Biodex System 3 isokinetic through a PowerLab 8/35 DAQ and LabChart software (ADInstruments). After thorough testing, we have not been able to get the signals to appear in the software. Please, find attached the information of the cable characteristics we followed.
We contacted Biodex (USA and Spanish providers) and they told us that it was necessary to have a tool installed on the computer called Analog Signal Access Interface (ASA Utility)(https://www.biodex.com/physical-medicine/products/software-updates/legacy-software/analog-signal-access-interface).
However, they told us that everything related to the System 3 model was discontinued and they could not provide us with this software.
We would like to kindly request, if possible, if you could share with us a digital copy of the installation file of the ASA Utility. If not, we would like to know if you know of any other possible solution to this problem.
Thank you very much for the attention and help.
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Thank you so much for your answer!
Actually, we do not have the Research ToolKit or ASA Utility installed on our Biodex System 3.
We contacted Biodex and ask them if they could provide us with the installation tool but they said that the System 3 was no longer supported by Biodex due to its age and they didn't have the parts anymore :(
So at the moment, we don't have any solution yet.
Best regards.
Antonio
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Hello,
I'm working on simulating 3D VIV with ANSYS FLUENT. To start with easy point, I made the cylinder static, but Karman Vortex Street just didn't show up. The fluid domain was separated into inner region (finer meshes) and outer region (coarser meshes). And I noticed that the quantities crossing the interface of 2 regions was discontinuous as the pic shows. I tried different combinations of mesh types, but it came out the same.
Does anyone know the answer?
Note that the interface of 2 regions is non-conformal, and Matching was selected in Interface Options panel.
Please help me, thanks a lot!
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you may have put some undesired inflation layers at the interface..
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As to the title, I have computed a gas-liquid two-phase flow by "laminar-flow,level-set ". I wish to get the velocity of the head of the bubble vs. time, i.e., the velocity of the interface(phils=0.5). How could i get this velocity? Thanks a lot.
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Bharat Soni thank you so much for your idea. it is helpful.
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Hi all,
In the Young's equation, σsg = σsl + σlg ⋅ cosθ.
When the surface tension of liquid( σlg ) is known, surface energy of solid(σsg) is known too.
After measure the contact angle between solid and liquid,
Is it possible that the interfacial tension between the liquid and the solid(σsl) be negative?
If a negative value is valid, does that mean it is exothermic when forming a solid-liquid interface?
However, I still cannot determine whether negative surface energy is reasonable or not.
Thank you very much.
Sincerely
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If you just have a single solid material in equilibrium with a single liquid, or a gas/vacuum, then the surface energy is always positive.
If the surface energy would be negative, then molecules of the solid reduce their free energy when they go from being surrounded by other solid molecules, to being surrounded by the fluid. This means that the solid will want to make as much fluid/solid interface as it can, to lower its energy. The best way to do this is for the molecules of solid to dissolve into the fluid (as then each molecule of solid is completely surrounded by fluid, and there's a huge area solid/fluid interface). I.e. a solid with a negative surface energy should spontaneously vaporise/dissolve.
Another way to see this, is that for simple solid/vacuum interfaces, the surface energy scales like U/a^2, where U is cohesion energy between molecules in the solid, and a is molecule size (e.g. intro chapter of Capillarity and Wetting by de Gennes et al). So negative surface energy -> negative cohesion energy.
It's more complicated when you don't just have simple solid/fluid interfaces. i.e. if you have molecules that can adsorb to the interface, then in principle, you could have negative surface energies. It's certainly unusual though.
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It is possible to read the acceleration values from the microcontroller above? I have been struggling as the datasheet didn't explain this or because I am a novice
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Yes, you can interface CN0533 or ADXL1004 with ESP32. The ESP32 has a variety of communication interfaces, including I2C, SPI, UART, and more, so you should be able to connect the two devices. The process will depend on the specific communication protocol you are