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Material Characterization - Science topic

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I am currently working on a research project for developing a novel additive manufacturing system that uses selective laser melting (SLM) coupled with Fourier Transform Infrared (FTIR) spectroscopy for material characterization of lunar regolith as feedstock for 3D printing infrastructure on the lunar surface. Any data regarding how the system could be developed and integrated would be greatly appreciated.
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Madison Feehan Please do recommend my message if it was helpful
Selective Laser Melting (SLM) and Selective Laser Sintering (SLS) are advanced additive manufacturing technologies used to create three-dimensional objects by selectively melting or sintering layers of material powder. These technologies have applications not only on Earth but also in space. In-space manufacturing using SLM and SLS is gaining attention due to its potential to support long-duration space missions, colonization of other planets, and sustainability in space. Here are some of the technologies being enabled for SLM/SLS manufacturing in-space:
  1. Reduced Gravity Printing: In microgravity environments like the International Space Station (ISS), traditional 3D printing can be challenging due to the absence of gravity. Researchers are developing SLM/SLS systems that can operate effectively in microgravity or reduced gravity environments. This involves addressing issues related to material flow and heat dissipation, among others.
  2. Space-Adapted Materials: The development of materials specifically designed for in-space manufacturing is crucial. These materials need to be stable in a vacuum, have good flow characteristics in microgravity, and be suitable for SLM/SLS processes. Researchers are working on developing space-adapted materials like metal alloys, ceramics, and polymers.
  3. In-Situ Resource Utilization (ISRU): For future lunar or Martian missions, utilizing local resources to produce parts and equipment is a key goal. In-space SLM/SLS systems may need to process lunar regolith or Martian soil to create building materials or spare parts.
  4. Autonomous Systems: Due to the vast distances between Earth and space exploration destinations, autonomous SLM/SLS systems are being developed. These systems can operate with minimal human intervention and can adapt to changing conditions in space.
  5. Radiation Protection: Space is filled with ionizing radiation that can be harmful to both humans and equipment. Researchers are working on ways to incorporate radiation shielding into 3D-printed objects. This could be crucial for long-duration missions beyond Earth's protective magnetic field.
  6. In-Orbit Manufacturing Facilities: The concept of establishing manufacturing facilities in orbit around Earth or other celestial bodies is being explored. These facilities could include SLM/SLS equipment along with other necessary infrastructure to support sustained production.
  7. Closed-Loop Recycling: Space missions have limited resources, so recycling and reusing materials are essential. SLM/SLS systems in space may need to incorporate closed-loop recycling processes to reduce waste and maximize resource utilization.
  8. Teleoperation and Remote Control: For the maintenance and operation of in-space SLM/SLS systems, astronauts or operators on Earth may need to remotely control and monitor the equipment. Teleoperation technologies are being developed for this purpose.
  9. Real-Time Monitoring and Quality Control: Ensuring the quality of 3D-printed objects in space is critical. Real-time monitoring and quality control systems are being integrated into SLM/SLS equipment to detect and correct issues during the printing process.
  10. Collaborative Robotic Systems: Collaborative robots or robotic arms can assist astronauts in setting up, maintaining, and operating SLM/SLS equipment in space. These robots can also provide additional stability in microgravity.
In-space SLM/SLS manufacturing has the potential to revolutionize space exploration by reducing the need to transport all equipment and spare parts from Earth. These technologies are still in development and will continue to evolve as space exploration efforts expand.
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I am currently seeking guidance and insights on the process of composing a comprehensive review article focused on the topic of "Photocatalysis of Cobalt Oxide Nanoparticles." While I have a keen interest in the subject matter, I am uncertain about the proper structure, content organization, and key points that should be covered in a review article.
Specifically, I am seeking advice on the following points:
  1. Structuring the review article: How should I organize the content to ensure a coherent flow of information?
  2. Key elements to include: What are the essential components that must be addressed within the review to provide a comprehensive understanding of the subject?
  3. Literature synthesis: How do I effectively synthesize existing research and findings on the photocatalytic applications of cobalt oxide nanoparticles?
  4. Analyzing research gaps: What strategies can I employ to identify and analyze gaps in the current understanding or areas that require further research?
  5. Citing and referencing: What is the best approach to citing and referencing relevant sources in a review article of this nature?
Furthermore, I am open to suggestions for an appropriate title for the review article. Your expertise and insights would be greatly appreciated in helping me embark on this endeavor effectively and professionally.
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Crafting a comprehensive review on photocatalysis using cobalt oxide nanoparticles requires careful planning and organization. Below, I have outlined a step-by-step guide to help you in this task:
Introduction: Start your review with an introduction that provides background information on photocatalysis and its importance in sustainable energy and environmental applications. Explain the concept of photocatalysis and its potential to address various challenges like water purification, air pollution control, and solar energy conversion. Also, introduce cobalt oxide nanoparticles as one of the promising photocatalytic materials and highlight their unique properties and advantages.
Synthesis Methods: Discuss various synthesis methods for cobalt oxide nanoparticles, including chemical precipitation, thermal decomposition, hydrothermal synthesis, sol-gel method, and others. Describe the principles, advantages, limitations, and key parameters of each method. Include recent advancements in synthesis techniques, such as microwave-assisted synthesis or environmentally friendly methods.
Characterization Techniques: Explain the characterization techniques used to analyze cobalt oxide nanoparticles and assess their photocatalytic properties. Common techniques include X-ray diffraction (XRD), scanning electron microscopy (SEM), transmission electron microscopy (TEM), energy-dispersive X-ray spectroscopy (EDS), UV-Visible spectroscopy, and Fourier transform infrared spectroscopy (FTIR). Detail the information each technique provides and how it helps in understanding the crystal structure, morphology, composition, and optical properties of cobalt oxide nanoparticles.
Photocatalytic Mechanisms: Elaborate on the photocatalytic mechanisms involved in cobalt oxide nanoparticles. Discuss the band structure, electronic transitions, and charge carrier dynamics responsible for the photocatalytic activity of cobalt oxide. Explain the generation, migration, and transfer of charge carriers, as well as the interaction between cobalt oxide nanoparticles and target pollutants or substrates during photocatalytic reactions.
Photocatalytic Applications: Explore the diverse applications of cobalt oxide nanoparticles in photocatalysis. Highlight their performance in degradation of organic pollutants, water splitting for hydrogen production, CO2 reduction, and other relevant areas. Present recent studies, key findings, and limitations of cobalt oxide nanoparticles in each application. Emphasize challenges and opportunities for further enhancement and optimization.
Factors Affecting Photocatalytic Performance: Discuss the factors that affect the photocatalytic performance of cobalt oxide nanoparticles. This includes the effect of nanoparticle size, morphology, crystal structure, doping, surface area, and surface modification. Also, address the influence of reaction parameters like pH, temperature, light intensity, and photocatalyst dosage. Explain how these factors influence the efficiency, selectivity, and stability of cobalt oxide photocatalysts.
Strategies for Enhancing Photocatalytic Activity: Present strategies employed to enhance the photocatalytic activity of cobalt oxide nanoparticles. This may include co-catalyst deposition, heterojunction formation, noble metal doping, ligand engineering, and hybridization with other materials. Explain the mechanisms behind each strategy and their impact on the photocatalytic performance of cobalt oxide.
Conclusion: Summarize the main points discussed in the review, emphasizing the significant advancements, challenges, and future prospects of cobalt oxide nanoparticles in photocatalysis. Provide insights into potential directions for further research and development.
Remember to review and revise your work for clarity, coherence, and accuracy. Cite relevant and up-to-date research articles and review papers to support your claims. Good luck with your comprehensive review on photocatalysis using cobalt oxide nanoparticles!
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May I get your opinion on 3 type detector above? I need feedback from researcher, not manufacturer.
Thanks.
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Hello Muhammad Firdaus Omar, I am also looking for your experience on the x-ray detectors as Elena Elena Lounejeva. Would like to know.
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Characterization Techniques to determine various properties
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Correlation of hole expansion ratio with tensile properties, integrated analysis system using machine vision, ISO 16630 testing, through thickness and edge tests, biaxial tests, advance fracture methods and metallurgical approaches to improve hole expansion are quite common. Different hardening instrument, conical punch, simulation method, ultrastructure expansion microscopy, differential expansion microscopy, SEM, scanning transmission electron microscopy, photoconductive AFM, image processing, nanoscale imaging are couple of important tools to characterize hole expansion limits.
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Shape is strange and I may not able to explain this with an equivalent circuit. So, please some one can help me to explain with proper electrochemistry?
This results came for Supercapacitor measurements
I have repeat this and I continuously got this shape, ensure it wasn't mistake
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Since it is repeatable, please check the linearity of your system and that your data is consistent with the Kramers-Kronig relations. Is it possible also to put some frequency values on the Nyquist plot?
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Can crystallite size and grain size be used interchangeably? Could you please recommend a resource on this topic?
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In materials science, the terms "crystallite size" and "grain size" are often used interchangeably, but they do have different specific meanings:
  • Crystallite size refers to the size of a single crystal in a polycrystalline material. In materials with a high degree of crystallinity, such as many metals and ceramics, the material is composed of many small crystals (crystallites) that are fused together. The size of these individual crystals can have a major impact on the material's mechanical properties. Crystallite size is often determined using techniques like X-ray diffraction (XRD).
  • Grain size refers to the size of a grain in a polycrystalline material, where a grain is a region of the material within which the crystal lattice orientation remains consistent. In other words, a grain contains one or more crystallites, but all of the crystallites within a single grain have the same crystallographic orientation. When the crystallographic orientation changes, you've crossed a grain boundary into a new grain. Grain size can affect the material's mechanical and physical properties and is often measured using optical microscopy.
To put it simply, if a material's grain boundaries coincide with the boundaries of its crystallites (i.e., each grain is a single crystal), then the crystallite size and grain size are effectively the same. However, if a grain contains multiple crystallites (i.e., the crystallites are smaller than the grains), then the crystallite and grain sizes are different.
You may find the following references useful for further reading:
  1. "Physical Metallurgy Principles" by Robert E. Reed-Hill and Reza Abbaschian. This book provides a comprehensive introduction to physical metallurgy principles, including detailed discussions of crystal structure and grain boundaries.
  2. "Characterization of Materials" by Elton N. Kaufmann. This book includes a chapter on microstructure characterisation, which includes crystallite and grain size discussions.
  3. "X-Ray Diffraction: Modern Experimental Techniques" by Olaf Engler and Valeri P. Skripnyuk. This book provides an in-depth discussion of how X-ray diffraction can be used to measure crystallite size.
Remember that while the two terms are often used interchangeably in casual conversation or in certain contexts, they do refer to different concepts, and using them correctly can help avoid confusion.
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If the Electron beam direction is contained by the twinning plane, the TEM pattern shows characteristic satellite spots in the spot pattern of the sample (Refer attachment).It is clear from the spot pattern that the twin spots appear as mirror images across the 11 ̅1 / 1 ̅11 ̅ twinning plane. Till here it is correct. My doubt is why the 11 ̅1 ̅+ twin spot is not adjacent to 002 ̅ + twin spot or why the 1 ̅11 spot from the matrix is not adjacent to the 002 spot from the matrix? What determines the relative positions of the twin spot and the matrix spot?
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The characteristic feature of the diffraction pattern of a twinned sample is due to the different orientations of the twin domains. This results in a splitting of the diffraction spot into two or more spots with different intensities and positions. This is because each twin domain contributes to the diffraction pattern with its own crystal orientation. The number and intensity of the twinned spots depend on the degree of twinning, and the crystal structure of the sample.
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I synthesized a compound that has a minor derivative phase. While obtaining the lattice parameters of the major phase via PowderX, a mismatch between the hkl values obtained in PowderX and the standard hkl values in JCPDS for the major phase was observed.
I would like to know the possible reason for this and how to proceed in correcting the same.
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Dear friend R G Sibiya Stacey
There could be several reasons for the mismatch between the hkl values obtained via PowderX and the standard hkl values in the JCPDS (Joint Committee on Powder Diffraction Standards) database for the synthesized compound. Some possible reasons and suggestions for addressing the issue are as follows:
1. Sample impurities or contamination: The presence of impurities or contamination in the synthesized compound can affect the diffraction pattern and lead to discrepancies in the observed hkl values. It is essential to ensure the purity of the sample through appropriate purification techniques and characterization methods.
2. Crystal structure variations: The synthesized compound may have variations in its crystal structure compared to the standard reference in the JCPDS database. These variations can result from factors such as crystal defects, lattice distortions, or the presence of additional phases. In such cases, it is necessary to refine the crystal structure using advanced diffraction techniques like single-crystal X-ray diffraction or high-resolution powder diffraction to obtain accurate hkl values.
3. Instrumental factors: The mismatch could be attributed to instrumental factors, including sample preparation, instrument calibration, and data collection parameters. It is crucial to ensure proper sample preparation techniques, instrument calibration, and optimization of data collection parameters to minimize errors and obtain reliable results.
To address the issue and correct the mismatch, the following steps are recommended:
1. Characterize the synthesized compound: Employ complementary characterization techniques such as X-ray diffraction (single-crystal or powder), scanning electron microscopy (SEM), energy-dispersive X-ray spectroscopy (EDS), or other suitable techniques to verify the composition, crystal structure, and purity of the synthesized compound.
2. Refine the crystal structure: If there are significant variations in the crystal structure compared to the standard reference, consider refining the crystal structure using advanced diffraction techniques like single-crystal X-ray diffraction or high-resolution powder diffraction. This can provide more accurate hkl values and help identify any deviations from the expected crystal structure.
3. Consult literature and experts: Review relevant scientific literature and consult with experts in the field who have expertise in the synthesized compound or similar materials. They may provide insights into possible structural variations or offer guidance on data analysis and interpretation.
It is important to note that without specific details about the synthesized compound, the experimental conditions, and the observed discrepancies, it is challenging to provide a definitive answer. Therefore, it is advisable to consult scientific literature, relevant research articles, and experts in the field for a more comprehensive understanding of the specific case.
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For my research purpose I need a Composite 3D printing filament.
Please share the cost details to manufacture a 1Kg filament using a twin screw extruder.
And share the combination of filament already fabricated using a twin screw extruder.
And Share the detail of twin screw extruder availability in India. My location is Vellore, Tamilnadu, India. Please share the nearest availability of twin screw extruder.
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Dear Nekin,
Nice question, I believe that it will be difficult to find a well-supported answer!
Hereinafter there are only few considerations from my part.
a) The price of 3D printing composite filaments is determined by a multitude of factors (nature of polymer matrix, fillers, reinforcements, additives, capacity of production, and so on).
b) Traditionally, the twin-screw extruders (TSE ) can be successfully used to produce various composites by melt-compounding, of good quality and with high throughput, which can be proposed for 3D applications.
c) Unfortunately, TSE are less adapted for the direct production of 3D filaments of high quality, even that there are few suppliers that can propose this kind of equipment for one step production, designed mostly for academic research/low-capacity production (e.g., Lestritz, ThermoFischer, etc.). Maybe other RG collegues can help more with information...
d)Please take a look :
Thermo Scientific Process 11 Lab-scale 3D Filament Production System
e) For the production in big quantities of 3D filaments it’s generally agreed that the production in two steps (1. fabrication of composites with TSE; 2. the extrusion of 3D filaments, e;g., using a single screw extruder) has a large number of advantages. I will refrain from more comments...
f) Function of requirements/ your application (type of composite), I suggest you use as starting point the price of 3D filaments/composites that look similar/satisfy your needs, and which are already commercialized in the market!
Success in your R&D project and best regards,
Marius
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In fracture mechanics, the obsolete principle of stress intensity factor K (SIF) is still used, even though it has a limited validity and questionable interpretation.
What experience do you have and what is your opinion?
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Rhys:
This is a question that has been raised for half a century or more - I can remember Keith Miller, when I was a graduate student, opining that delta-K could not be used to describe fatigue-crack growth - nevertheless fracture mechanics is still successfully used today. As long as one is properly aware of the basis and limitations of governing parameters such as K and J, I still believe that they have a powerful application. However, this is not always the case when they are used and accordingly fracture mechanics has become one of the most abused form of mechanics.
If you think that this approach should be dismissed though because of its "limited validity and questionable interpretation", could I respectively ask what you would recommend as a replacement?
cheers Rob
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I have older version of x'pert highscore software and what to do for pdf2, pdf 4? Please suggest me or share the link of x'pert highscore software latest version (free)/ free pdf2, pdf4.
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Both Origin software and X'Pert HighScore software can be used to determine the hkl values of a crystal structure. Here are the steps to follow for each software:
Using Origin software:
1. Open the data file in Origin software and select the graph containing the diffraction pattern.
2. Click on the "Peak Analyzer" button in the toolbar.
3. In the Peak Analyzer window, select the peak of interest by clicking on it.
4. In the "Peak Information" tab, note down the "2Theta" value and the "Counts" value for the peak.
5. Use the Bragg's law equation (2dsinθ = nλ) to calculate the d-spacing value for the peak. Here, n = 1 for first-order diffraction. λ is the wavelength of the X-ray used in the experiment.
6. Use the d-spacing value to calculate the hkl values for the peak using the Miller indices formula (hkl = [n1d1,n2d2,n3d3]).
Using X'Pert HighScore software:
1. Open the data file in X'Pert HighScore software and select the diffraction pattern.
2. Click on the "Peak Fitting" button in the toolbar.
3. In the Peak Fitting window, select the peak of interest by clicking on it.
4. In the "Peak Information" tab, note down the "2Theta" value and the "d-spacing" value for the peak.
5. Use the Bragg's law equation (2dsinθ = nλ) to calculate the wavelength of the X-ray used in the experiment.
6. Use the d-spacing value to calculate the hkl values for the peak using the Miller indices formula (hkl = [n1d1,n2d2,n3d3]).
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Can you suggest some good book /literature for understanding the Rietveld refinement method.
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Modern Powder Diffraction ; B. Toby
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Has a structural explanation been proposed for this?
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It is known that water has unique properties compared to other liquids. This uniqueness is given to it by the nuclear quantum effect, which is understood as the role of the ZPE of water or the zero energy of the quantum harmonic oscillator -О-Н, proton tunneling, entanglement of quantum fluctuations, competition of thermal and quantum fluctuations.
In water ℏω≪kT and quantum effects are covered by thermal fluctuations. They are visible only in its kinetic properties, where quantum fluctuations play a prominent role.
Now the minimum on the temperature dependence of the isothermal compressibility of water at 46 0С becomes clear. This is explained by the presence of water structures LDL and HDL with a size of 1–2 nm. According to the results of the article
feature of the temperature dependence of the isothermal compressibility of water should be represented as follows. Quantum fluctuations of the O-H bond of torsion and tension of water and H-bonds oscillate in a double-well potential with proton tunneling. The energy compromise is maintained so that the energy of quantum fluctuations is equal to the energy of thermal fluctuations to maintain the minimum Gibbs energy of formation of microcavities in water.
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I am currently studying the effects of mechanical properties of GO and rGO on PC/ABS. However, after analysing the data, I found that the tensile strength decreasing, but, for the flexural strength, the data shows and increment when the compatibilizer added into the system.
I have not yet found any answer on this matter. Is there any scientific reasons that can cause this or is it because of the equipment error?
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Hello. Another fact that you should notice is that in some cases when the material loses its ductility, its tensile properties may be affected more than its bending properties.
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I intend to perform mechanical tensile test for my polymer nanocomposites. Does there exists any ASTM standard to follow? Can I also know the dimensions of the specimen to be produced? Lastly, I intend to create a mould for the dog-bone shape. Can we get files online to create the dog-bone mould using 3D printer?
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Yes, there are several ASTM standards available for performing mechanical tensile tests on polymer nanocomposites. Some of the commonly used standards are:
  1. ASTM D638 - Standard Test Method for Tensile Properties of Plastics
  2. ASTM D3039 - Standard Test Method for Tensile Properties of Polymer Matrix Composite Materials
  3. ASTM D882 - Standard Test Method for Tensile Properties of Thin Plastic Sheeting
The dimensions of the specimen depend on the specific ASTM standard chosen for the test. For example, ASTM D638 specifies the dimensions for Type I, II and III specimens. Similarly, ASTM D3039 and ASTM D882 specify the dimensions for different types of specimens.
Regarding the creation of a dog-bone mold using a 3D printer, there are several online resources available that provide files for 3D printing dog-bone molds. Some popular online resources include Thingiverse, GrabCAD, and MyMiniFactory. However, it is important to ensure that the dimensions of the mold are as per the ASTM standards to obtain accurate results.
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Nanoindentation is a attachment with AFM or it is a separate testing procedure? Nanoindentation gives property at nanolevel? Young's modulus, Hardness, Stiffness, Load vs Depth, Load Vs Hardness properties alone cane be obtained using nanoindentation or any other properties can also be known using nanoindentation? Where I can get all these things done in India? Please share your suggestions. Many of the prestigious institutions saying machine under maintenance, machine not working or operator not available.
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Nanoindentation is a separate testing procedure that is often used in conjunction with Atomic Force Microscopy (AFM). It is used to measure properties at the nanoscale, such as Young's modulus, hardness, stiffness, and load vs. depth and load vs. hardness. Other properties can also be measured using nanoindentation, depending on the specific application. In India, there are several institutions that offer nanoindentation services. These include the Indian Institute of Technology (IIT) Delhi, IIT Bombay, IIT Madras, IIT Kanpur, IIT Hyderabad, and the National Institute of Technology (NIT) Surat. Additionally, there are several private companies that offer nanoindentation services, such as NanoTest India, NanoTest Solutions, and NanoTest Technologies. If you are having difficulty finding a nanoindentation service provider, it is possible that the machine is under maintenance or the operator is not available. In this case, it is best to contact the service provider directly to inquire about the availability of the machine and the operator.
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Dear colleagues,
Within the frame of the postdoctoral project INFRA-ART, an integrated spectral library exclusively dedicated to artists' and cultural heritage materials has been developed. The INFRA-ART Spectral Library (https://infraart.inoe.ro/) is an open-access resource that was developed to support other specialists within the heritage science field that work with XRF, infrared (ATR-FTIR), or Raman spectroscopic techniques.
The database is an ongoing compilation of spectra that contains at this moment over 1000 ATR-FTIR and XRF spectra, and a preliminary dataset of Raman spectra, linked to over 500 reference materials (paint components, artist color paints, etc.). The database is keyword searchable and an interactive spectra viewer that allows users to visualize and analyze the spectra of each sample is available.
To support universal access and the reuse of scientific data, the database follows the European Commission’s recommendation on access to scientific information as well as the FAIR Guiding Principles on research data that result from publicly funded research. Users can request access to spectral data of interest via e-mail and subsequent completion of a File Access Request Form.
We invite the cultural heritage research community and other specialists in art history, conservation, or materials science to access and share this resource. Of course, your feedback is welcome. Please share your thoughts, questions, and suggestions below or e-mail us at infraart@inoe.ro.
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Well, I can't help much with the web site part, but if you want I could assemble a searchable database from your spectra, to be offered among the free databases here: https://www.effemm2.de/spectragryph/down_databases.html
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I study the delamination of laminates upper and bottom skins of honeycomb composite structure simple supported from two sides and under bending stress.
I consider the developed tension on the bottom skin as the main peeling force that cause delamination.
Is my thinking correct?
Also, do you suggest textbooks?
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Delamination of laminates in a honeycomb composite structure can occur when there is a failure of the bond between the layers of the composite, resulting in the separation of the layers. In a simple supported structure under bending stress, the forces acting on the structure can cause the layers of the composite to experience different levels of tension and compression, which can lead to the development of shear stresses at the interface between the layers. These shear stresses can cause the bond between the layers to fail, resulting in delamination.
Your thinking that the developed tension on the bottom skin of the honeycomb composite structure can act as the main peeling force causing delamination is generally correct. The tension in the bottom skin can cause the bond between the layers to be subjected to tensile forces, which can lead to the separation of the layers if the bond is not strong enough to resist the forces.
However, it is important to note that the delamination of laminates in a honeycomb composite structure can also be influenced by other factors, such as the properties of the materials used to make the composite, the manufacturing process used to produce the composite, and the loading conditions applied to the composite. It is therefore important to carefully consider all of these factors when evaluating the risk of delamination in a composite structure.
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AssalamoAlaikum Hello Everyone hope you are doing well.
Yesterday I received an email from my supervisor in which he mentioned that to make a new proposal on the Topic of CO2 storage/capture as impurity by using GO (graphene oxide). I haven't worked on it. Could you suggest me some articles that are related to the topic and helpful to understand the topic. Actually I have to submit it in next 5 days so please if you have some information please guide me on this topic.
I am highly thankful to all of you for your time and suggestions (in advance)
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suggest to look for a more intelligent supervisor - this is nonsense. For CO2 storage only cheap bulk material make sense.
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5 wt.% of Mn(NO3)2.4H2O was used as a precursor for the wet impregnation synthesis of MnOx/SiO2. After dehydration at 70 °C, a white paste was obtained and thereafter dried in an oven overnight at 90 °C. After drying, a black powder is obtained.
Why is the powder not retaining its white colour? A colour change of the supported metal nitrate precursor is often associated with metal oxide formation after calcination.
Waters of hydration and physisorbed water would be removed during calcination, under air, at around 100-150 °C, and the decomposition of the Mn(NO3)2 is reported only to occur around 300 °C.
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The silica surface may catalyze the decomposition of the manganous nitrate with oxidation of Mn(2+) to some Mn(3+), forming for example black Mn3O4. If you want to prevent this "early" oxidation, working under nitrogen may help; however, oxygen is also available from the decomposition of nitrate, so I would expect some darkening to still occur.
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Also why the line nearer to the central beam is dark and the one far away from the central beam is Bright?
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The Kikuchi diffraction in TEM is generated via bragg diffraction by inelastic scattering electron, and the diffraction intensities from the front crystal plane and the back plane are different, therefore, one of the Kikuchi lines is bright and the other is dark. The inelastic scattering electron beam density nearer to the central beam is stronger than others far away from the central beam, however, much of the electron beam is diffracted to the dark line direction, thus, the total intensity of the Kikuchi line nearer to the central beam is weaker than the other one.
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I would like to measure the impedance/ capacitance of the dielectric in order to find the moisture of the material by impedance spectroscopy. How can I ascertain that I am detecting (measuring) only the 'moisture content' of the material but not other properties?
How can I validate the value of impedance spectroscopy measured experimentally compared with the theory (or the experimental validation of the results through the theoretical analysis)?
Thanks in advance.
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Thank you again for your assistance and for the provided literature as well.
Best regards,
Tanzila
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Hi all,
I am testing UV-vis spectrophotometer for PDMS, using "Hitachi U-3900"
My holder for solid can only get reflectance(%R) data,
Schematic of test is Figure 1,
PDMS is a very high transparent material, but its %R is very high(Figure 2), it is weird.
I think most of the light passing through the PDMS and reflected by the Aluminium oxide,
In such situation, can I convert reflectance(%R) into transmittance(%T)?
Thank you very much.
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Good day! Here I found brief and complex explanation on reflectance and transmittance phenomenons:
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Hello Investigators,
If I have to measure the temperature on a plates : one with reinforcement and another without reinforcement material during Friction Stir Processing.(Consider the temperature measurement at the middle of Friction stir processed workpiece.
Therefore, In which case the temperature will be more and why?
Suggestion and comments will be highly appreciated.
Thank You
Kind Regards,
Roshan
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Dear Dr.Soumyabrata, Thank you for the proposed solution to the query.
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The basic scenario where the graph is exponential and we may extrapolate to obtain the bandgap in eV is suggested in research publications on energy bandgap approximation using Tauc Plot. Which peak, however, should I take into account for extrapolation when there are multiple peaks in a Tauc Plot?
The appropriate figure is included.
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Have a nice time and good day!
Please read these papers, you will find what you want:
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Dear Researchers :
I have this question and I have an hypothesis:
Why Natural HDPE, when extruded at temperatures about 100 °C (around) it has a white (but pale white), and then when the polymer cools down it color turns between white an yellow.
I understand that this phenomenon it is a general case of all LLDPE, LDPE and HDPE , and in all fabrication processes : Extrusion, injection, molding, pressing, etc.
So this is fundamentally, a chemical characteristic of the material ...
It has to do with a change in the Oxygen concentration in the material ?
Thank you all in advance,
Best Regards !
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Dear Franklin Uriel Parás Hernández, both degradation and crystallization are behind the change in color aspect. My Regards
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In theory, martensite (a titanium alloy) begins to form at temperatures ranging from 575 oC to 800 oC. This wide range of temperature reports creates ambiguity in the descriptive analysis of the related phenomena. Therefore, how do you determine martensite start alloy using experimental work (in this case with DSC analysis) and what is the theory behind these determination temperatures?
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You are most welcome dear Hasfi F. Nurly . Wish you the best always
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I am looking for a method to select a specific size of silica particles (spheres) from a broad range of mixture with different particle size. I need to be selective in the cut-off. I have tried mechanical sieving both in dry and wet form, but its quite laborious, time consuming and lot of water wastage (wet sieving). Can any one suggest any equipment or method for large scale separation (around 10 Kg) ?
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What would be the easiest method to separate silica particles of different particle size in large scale?
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I want to know how to make accurate peak analysis of FTIR results. As an example, I have an absorption band between 700-720 of wave-number, I mean the parabola which makes the peak's shape starts at 700 and ends at 720. Can I consider the results which in the literature report that for example a peak at 700 or 711 relates to the specific functional group? I want to know how much deviation is standard when you want to report that this peak is related to which functional group. What is the standard order of this kind of deviation? I want to know some standards regarding this issue since I found some peaks in my spectrum which have near values to the reported results in literature but they do not have exactly the same reported value. Can someone guide me please? If you can introduce me a quantitative amount for the deviation, I would be thankful.
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Shima Fasahat Accuracy is always assessed by comparison against a known, certified standard. You have to define how close you need/require/want to be near the 'truth'. You also need to look for materials (e.g. from NIST) that satisfy the accuracy parameter you're searching for.
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Material Characterization, Solid State Physics, Surface Science, Spectroscopy, Diffraction
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diffraction - some phenomena at costant freqyency
spectroscopy - as result of frequency variation
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Where can I find XRD central facility for low cost? My neighbouring university charging INR 1500/- per sample. It is too high for me to bear as there are more samples to follow. My parent university doesn't has the facility. Now I have 3 samples only.
Can any one help me in this regard? 
These first three samples are base for my work and based on the results I have to move ahead in my Ph.D.  work.
Any help in this regarding is highly appreciated.
Thanks in advance.
Vara Prasad
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I discovered two distinct phenomena when cracks begin to form at α and β phases in titanium alloys. How does this difference mechanism come about?
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Dear Hasfi,
The reasons for the initiation of cracks are related accumulated internal stresses between the α and β phases in titanium alloys. These external stresses in the process of operation tend to balance. Cracks can be observed in both solid particles and softer particles of the structure. To avoid this negative effect, normalization is performed to a certain extent or the chemical composition of the spawn is changed in order to reduce external stresses.
With respect
Emil Yankov
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This is a window for diverse issues, inquiries, and discussions about X'Pert High Score software to help researchers find the answers they seek in one place and reduce exhausting the experts to answer one question in different windows.
Best wishes to all.
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Dear Siddig Abuelgasim , Kα2 stripping is mostly used for phase analysis to observe the original scan and compare it with the reference patterns. When come to refinement, the Kα2 stripping or any kind of pattern treatment will ruin your R-factor.
The RACHINGER method uses the exact wavelengths of the Kα1 and Kα2 lines and their intensity ratio. The intensity measured at the first point in the profile is assumed to be entirely stemming from Kα1. The dhkl causing the diffraction at this 2θ angle will, of course, also diffract the Kα2 at the angle prescribed by Bragg's law. Because the intensity ratio of the Kα1: Kα2 reflections is exactly 2:1, half of the intensity measured at the low-angle 2θ can be subtracted from the higher angle intensity, which is diffracted by the Kα2 wavelength.
The LADELL determined the profiles of Kα1 and Kα2 peaks of resolved lines, which is used to subtract a portion of the Kα2 intensity from a series of adjacent 2θ points. This method describes the Kα2 profile as the summation of 3, 5 or 7 sub-profiles instead of only 1 sub-profile as in Rachinger methods. The sub-profiles are indicated with levers (positions as wavelength ratios) and weights (intensity ratios).
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Dear Researchers :
Hope this discussion seems interesting for some of you
Is it correct to say :
"All Dielectric Materials are Electrical Insulators, but not all Electrical Insulators are Dielectric Materials" ?
I have this doubt, hopefully someone can provide a correct answer, and: Why not, or Why is it
Best Regards !
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Yes very interesting question:
We can make the comparison simple as follows:
1. An insulator is a material with no free carrier concentrations (electrons) able to conduct electricity meaning here Sigma=0.
2. A dielectric is a material where the carriers are all tightly bound to the crystal atoms i.e. they are not free to move.
- This is similar to the insulator case, but this is true only under static electric field conditions (zero frequency or DC electric field).
- Under High frequency AC electric fields, a dielectric can contribute to the conduction through polarization, which is a type of conduction dominant in dielectrics at high frequencies)
- A simple insulator cannot do the same.
I hope this answers your question.
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If I want to do surface characterization of a material which characterization technique is better SEM or AFM and why? All relevant answers are appreciated!
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Regarding material characterization, “better” depends on the sample under analysis. I would rather say that the best characterization can be obtained by combining SEM and AFM. For instance, if you are analyzing a nanocorrugated surface, SEM can give you the lateral dimensions of your nanofeatures, but you don’t have quantitative information in the vertical direction. On the other hand, AFM images are the result of the convolution of the real morphology with the shape of the AFM tip, so the lateral dimensions are always overestimated, but you can get the real quantitative value of the height of such nanotopographic motifs.
In SEM, besides using the standard secondary electrons detection, you can also take images with back-scattered electrons detection. The signal collected in those images formed with back-scattered electrons depends on the atomic number Z of the elements: higher Z produces a bigger number of back-scattered electrons detected. Consequently, if you are analyzing a composite material with metallic nanoparticles in it, such particles can be clearly distinguished with brighter contrast than the ceramic or the organic compound in the matrix. If the matrix is also metallic, they can also be distinguished if their atomic number is different enough. Moreover, by performing Energy Dispersive X-Ray analysis you can get the composition of the sample.
In AFM, an experienced user can get chemical contrast at the surface of a nanocomposite using the lateral force in contact mode or the phase signal in non-contact mode, which are related to friction and dissipative forces (adhesion, viscoelasticity, etc.), respectively. Furthermore, AFM allows for measuring some mechanical properties, characterizing electric transport (Conductive atomic force microscopy, C-AFM), and modifying the surface of the sample (indentation and even atom manipulation). Finally, advanced modes and special tips give access to other properties, and actually new microscopies are developed from the AFM: Kelvin probe force microscopy (KPFM) to obtain a map of the work function, Magnetic force microscopy (MFM) to characterize the magnetic domain structure of the sample, or Piezo-response Force Microscopy (PFM) to image the piezoelectric domains, to name a few.
I hope it helps, good luck with your research!
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I need S-N curve of N-HA for fatigue analysis.
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Sina Sazesh did you get S-N curve of HAP? I am looking for the same and could not find it anywhere
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Rear view LEED power supply.
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Are you still interested in getting this schematic?
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I-V Characterization of thin-film memristor and Interpretation of Pinched Hysteresis Loop
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Hi, everyone!
I am doing polymer synthesis, but the amount of polymer I can get from one synthesis is very small, about tens of microgram. I am using GPC to characterize it, but the information I can get is very limited.
Could anyone suggest any characterization method to get the polymer structural information that only use very small amount of samples? Better recyclable.
Thank you very much!
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Except the analyses that have been mentioned, you can performe ATR-FTIR analysis to determine its chemical stucture.
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I know that the acceleration voltage and probe current changes the spot size,but how? For instance, reducing the electron beam current diverges the electron beam into the aperture beneath the condenser lens, which transmits lower intensity of electron beam through it. But how does it affects the incident spot size on the specimen? Similarly, how does acceleration voltage changes the spot size?
I have gone through several reference books and literature, but did not get any appropriate explanation. Kindly enlighten me. Thank you!
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Actually beam current IS a spot size. Just not really good wording from some manufacturers.
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Need to do strain controlled fatigue test on ASTM E606 specimen. What I have referred from a research literature they have given strain ratio R, of 0.5 and a frequency of 0.2 Hz and strain levels of 0.7%–3.0%, 70% decline of peak load could anyone tell me how to decide this values ? From where they used the values there is no reference paper they have used in that particular research article.
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Hi Dinesh
Strain controlled fatigue testing is important to study the behaviour of components undergoing either mechanically or thermally induced cyclic plastic strains that cause failure within fewer cycles (<10^5) than high cycle fatigue (>10^5-10^6 cycles).
The testing conditions are usually determined by the specific application you are considering. Doing this preliminary investigation will allow you to get more meaningful and useful results from the strain controlled tests.
So I would recommend to try to collect some initial indicative data to better plan the test conditions (temperature, R, frequency, strain levels). If the components (or an older version of the components) are already in service you can get some good indications by applying some strain gauges and thermocouples to the parts to understand what sort of strains they undergo and at what temperatures. If the components are still in the design phase then you will need to carry out some hand calculations or run some FEA analyses to get a feeling of what strain the parts will experience once in service.
Having said this, in terms of strain levels you can consider that you enter within the high cycle fatigue range when the part undergo loads that generate stresses below half of the yield strength of the material i.e. 0.2% so you want to stay above this value. In general you could run tests at strain level within 0.2% and 20-40%. It depends also by the material and test temperature. Then with the Coffin-Manson equation you can relate cycles to plastic strains.
To determine the values of temperature, frequency and R for your tests, as previously mentioned, it would be better if you use values close to your actual application to collect more reliable and useful data.
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Kindly suggest good books for Surface Morphology as well as electric and magnetic characterization techniques.
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Dear Abhijeet, many thanks for the kind response and explanation. I just found two PhD theses which could be very helpful answering your question:
CHARACTERIZATION OF CERAMIC COMPOSITE MATERIALS USING TERAHERTZ NON-DESTRUCTIVE EVALUATION TECHNIQUES
and
Characterization of Ceramic Matrix Composite Materials using Millimeter-Wave Techniques
(please see attached pdf files)
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How to sift and separate particles of a certain size from a set of particles of different micrometer sizes?
for example we have 1kg of metal powder with size between 20 um to 120 um
we want to separate 30um particles, how can we do this?!
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Respected Madam,
For separating 30 micrometer particles US Sieve Mesh Number 450 is recommended. Refer the attachments for more details.
Hope this information is useful.
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For calculating the crystallite size of a catalyst, we use Scherrer equation. In which FWHM is required. Whether, crystallite size is depends on maximum intensity peak or average of crystallite size of main characteristic peaks?
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I agree with the above answers, you can select the most intense peak or can take an average of all of the peaks with std. Moreover, when you are calculating the crystalline size of all peaks then you can also calculate percent crystallinity by dividing the crystalline area over full area, these simple calculation I do in origin
Hope I answered well!!!
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I am currently working on a epoxy based material and I would like to simulate by using MCNPX in order to determine material properties. Is there a way to use my homogeneous mixture in MCNP? I know that I can simply enter the fractions of isotopes but this materials are note chemically bounded. They are seperate materials and physically mixed. I want to enter in my input as two different materials and then use fractions on cell cards. Is there a way to do that? I searched a lot but could not find any sign.
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You cannot use fractions on cell card. Materials should be defined in the data card and you can only use the material number on the cell card. In the material card you can define a single material containing several different elements with different weight fractions. Even if you want to define a mixture of different alloys you can define it by computing the weight fraction of each element in each alloy.
For example, you know that there are 0.12 'O' and 0.88 'Lu' in Lu2o3 and 0.12 'O' and 0.88 'Yb' in Yb2O3. now you want to produce a material containing 1/3 weight fraction Lu2o3 and 2/3 weight fraction Yb2O3. in the material card you should enter ZAID of 'O' with weight fraction of 0.12, ZAID of Lu with a fraction of 0.293, and ZAID of Yb with weight fraction of 0.586.
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I am writing to ask a favor kindly, I recently finished mi PhD thesis related to nanomaterials (TiO2 nanotubes) and anodizing, and as part of the doctorate cancellation process I need be a reviewer of a master or PhD thesis, If you know of any opportunity to be a reviewer, I would appreciate it if you proposed me.
Regards
Interest Areas
Materials Characterization Surface modification and coatings Thin Films Transmission Electron Microscopy (TEM) High Resolution Transmission Electron Microscopy (HRTEM) Scanning Electron Microscope (SEM) Atomic Force Microscope (AFM) X-ray diffraction (XRD) Biomaterials and Biointerfaces
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My specialization areas are the same topic u have mentioned. So if you prefer you can add reviewer
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Hello,
I am working on the fabrication of perovskite solar cells. I am interested to study charge carrier dynamics and recombination resistance. For that, I need to perform EIS of perovskite films. Please suggest any standard electrolyte for EIS of perovskite films. Thank you!
Kid Regards,
Abdul Sattar
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one of the most used electrolyte is I−/I3 − . Please for more details please follow the paper in the link:file:///C:/Users/Dell/Downloads/materials-12-01998.pdf
Best wishes
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If a well developed laminar flow passes through a tube with a rough inner surface, will the laminar boundary layer merge at the tube center, or it just stabilizes very close to the rough tube wall? The tube inner diameter is around 10 mm.
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In this case you can find boundary layer thickness less than tube radius between zero and tube radius X. The approximate experimental expression for the tube inlet length (L) calculation is: L/D=0.0288ReWhere, d  is tube diameter, Re  is Reynolds number.
For more information please read through the article herewith.
All the best Guo Li
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Can anyone tell me why maximum research group goes for Hummer's, modified hummer's and Improved Hummer's method instead of following Tour's method or some other method. Is this related to something special or just a choice 
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because in this method no toxic gas is produced.
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I wanted to know recent additions of ICDD (JCPDS) files of Zinc oxide. I have ICDD files which were addded before 2003. If anyone knows the recent ICDD files or atleast PDF numbers it will be most helpful to compare my data.
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You can easily get any XRD Reference or JCPDS file here,
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Assuming that there is a special type of advanced high strength steel that has a fully martensitic microstructure and a nominal tensile strength of 1500 MPa. By changing the composition of a single alloying element, i.e. increasing the C content, we can change the morphology and mechanical properties of the steel. How can we effectively compare the changes between the two steels at a fundamental level that goes beyond the general SEM, EBSD, and TEM characterization methodologies? Are there any crystal plasticity models that can be used in this case? Is a crystal plasticity study even valid for martensitic steels?
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Oleksii Sherepenko , as I have understood this question can be divided into 2 parts, namely
1) The influence of the carbon content on morphology of martensite. The alloying has influence on the lattice parameter of both parent and product phases, therefore the interfacial configuration, and the eigenstrains are changing. So both factors, which govern the morphology of product phase (i.e. elastic energy and interfacial energy) are functions of the alloying content. The modelling methodology in this case could be some crystallographic based models, molecular dynamics/monte carlo or phase-field model, depending on the resources available. Also with different content, the parent phase can have different grain size, which also has effect on martensitic transformation.
2) The influence on mechanical properties. From my point of view, the question can be divided in several "isolated" effects
2.a) Solid-solution strengthening. With increase in amount of secondary element solid-solution phase should have increased yield strength
2.b) Morphology of martensite. The size and form of martensites should play a role in the motion of dislocations. The number of interfaces should play a major role here.
About some crystal plasticity models.
There are some models, which take into consideration Petch-Hall effect, for example
It could be used as starting point for further model development.
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If I have to draw a FCC 111 surface, am assuming the miller indices are: [1,0,0], [0,1,0] and [0,0,1]
How can miller indices be determined for orientations like FCC 211 or FCC 110 etc.?
I am trying to build atomic models through ASE Python, so any help in that regard will be greatly appreciated.
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C1s peak at 284.8 corresponding to Adventitious Carbon is a reference for the X-ray photoelectron spectroscopy (XPS. However, when using carbon-based support, say Vulcan carbon (rich in graphitic carbon), r-GO and GO for deposition of active catalyst.
The C1s peak in these cases will be dominated by sp2 carbons, not by Adventitious Carbon.
How to calibrate the XPS data in that case?
How to account for the charging problem?
Thanks in advance
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As Jurgen states, the vulcan carbon should have enough conductivity. If using a monochromatic XPS system then analyse without the charge neutraliser on and ensure the carbon is in contact with the spectrometer (e.g. pressed in to a metallic well on the sample bar), then you shouldn't have an issue. The sp2 carbon will be ~ 284.5 eV depending on how well your spectrometer is calibrated.
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The grain orientation spread is a powerful tool to reveal recrystallization on the structure evolution. However, I still couldn't clearly understand the GOS result shown with the mechanical behavior effect.
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I've attached the picture from the histogram, relative frequency against GOS value (degree). I want to know the correlation between high or low-intensity frequency in low-angle grain boundaries with mechanical behaviors?
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Dear all
How can I interpret negative part of radius of gyration autocorrelation function? What is happen to my system exactly? The ACF I obtaied for my polymer system is like bellow:
Thanks
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Hello Mohammad,
It seem to be a phase transition.
The negative values of the auto-correlation function of the radius of gyration means either an inversion of an angle or a phase transition /structure factot S(q)/, or it is connected to a phase problem of loss of information concerning the phase that can occur when running a calculation.
Pay attention to your simulation box, connected to the Nr. of cores used for that simulation.
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On a synthetic graphite tube production line, this type of defect, similar to scales or the beginnings of cracks (cf. photos), appears regularly, including on unimpregnated tubes, just out of the oven (on the photos, these are tubes that have been impregnated and then brushed with traces of resin at the bottom of the scale). We noticed that our graphite had an abnormally high Fe content (a supplier problem). Do you think that these defects can come from a cast iron inclusion (the carbon of the graphite + Fe) formed locally during the graphitization process? Can such an inclusion at this scale (0.5-2mm) lead to surface flaking? If not, do you have any ideas on the origin of these defects?
Thank you very much for your answers and time,
A french materials engineering trainee in need of knowledge
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sure it maybe
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How to determine the the fatigue values at high stresses ? Because the endurance limit for my material is round about 480 MPa. and the yield point is about 660 MPa.
When I try to find the values in fatigue region at high stresses let's say above 550 MPa and 600 MPa, the material fails immediately after it starts to run and i could feel the heat dissipated. Does it mean anyway that its not possible to have fatigue limit or is it fine to just show the endurance limit ?
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In fatigue experiments the material and its microstructure plays a vital role. Its better you tell which material you are using and its composition. Also let me know whether you are using axial fatigue or rotating beam fatigue ,
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I have scanned a sample with X-rays for quantitative analysisof phases present. In the X-Ray diffraction plot (attached) peaks of phase with fcc and with bcc are easily identified.
But, a peak is still unidentified as shown in the attachment with question marks. The unknown phase should be carbide which is confirmed by optical micrography and SEM studies. To get the exact volume fraction of phases in the sample, lattice parameter of carbide is needed. Since no sister peak of unknown phase (that may be carbide) is obtained no matter how long the angular range of the scanning is employed, we are not able to compute the stiochiometry or lattice parameters of the inidentified phase. How can we move ahead? Can any other technique help us in identifying the unknown phase?
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Variations in the height of the specimen in its holder, whether increasing or decreasing, cause XRD peaks to change from their original location.
Important and useful pathways are connected to the XRD Curve:
Scherrer’s equation:
Particle Size = (0.9 x λ)/ (d cosθ)
λ = 1.54060 Å (in the case of CuKa1) so, 0.9 x λ = 1.38654
Θ = 2θ/2 (in the example = 20/2)
d = the full width at half maximum intensity of the peak (in Rad) – you can calculate it using Origin software.
To convert from angle to rad
Rad = (22 x angle) / (7 x 180) = angle x 0.01746
Example: if d = 0.5 angle (θ)
= (22 x 0.5)/ (7x 180) = 0.00873 rad
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I aim to analyse the permeability of aluminum to liquid gallium by measuring it's velocity at individual grain boundaries using ultrasounds.An ultrasound-based characterization technique is motivated by its higher temporal resolution.
But open to more suggestions regarding the problem statement.
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Please read :
An atomistically informed energy-based theory of environmentally assisted failure
S Ganesan, V Sundararaghavan - Corrosion Reviews, 2015 - De Gruyter
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Recently I tested a novel superhydrophobic coating by means of potential curves. What is odd is that I found a significative change in Ecorr (from 800 to 500 mv in comparison with the bare metal...) but instead of a lowering of Icorr I found an increase in ICorr (10-8 bare metal to 10-7 protected). The coating is conductive (it's C based). I have no idea how to interpret the results. Any ideas?
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@Sarah in my case it was related to the nature of the coating which was conductive. I can share with you the article we published if needed
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Including the so-called kinematic hardening in phenomenological material models allows capturing the accumulation of plastic deformation in materials subjected to cyclic loadings. It determines that the size of the "elastic domain" in the deviatoric stress space remains constant and that upon plastic yielding, the domain is simply translated.
In largely deformed materials in tension, the kinematic hardening may result in a translation of the elastic domain to levels where the initial compression yield-limit becomes now a tensile stress value. This implies that upon unloading a plastically-deformed material (returning to zero loads), it may experience plastic deformation as well. My question is, is that physically possible? If yes, how can it be explained?
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Hi!
Kinematic hardening is only a simplified model that is convenient for describing the Bauschinger effect. More realistic is the combined model that combines isotropic and kinematic hardening.
V.N.
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I have some h-BN powder which I need to use to prepare film by using drop-cast technique on Si/SiO2 substrate . Please tell me which solvents at which proportion should I use along with the experimental procedure.
Which condition will also ensure that the nanoparticles will not form any separated islands on the substrate and will be well dispersed in the solvents?
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I do not believe your suggested method is viable. To get a film of BN you'll need an evaporative technique, IMHO. I hope someone will prove me wrong as I learn more that way.
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How to plot reflectance graph from absorption/transmittance graph taken from UV-Vis spectrophotometer for thin film?
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This works better for me..
R=1-√(T×e^A)
Where, T is transmittance, A is absorbance...
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I am looking for a good quality 6H, <0001> oriented, Si-terminated SiC substrate. Who could be the best vendor ?
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Hi Shantanu.
For 4H-SiC substrates I can recommend CREE and SiCrystal. I do not know whether they still sell 6H-SiC wafers.
If 4H is not an option then maybe you can contact TankeBlue. I think, I have seen that they still sell 6H-SiC wafers.
Yours
Markus
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I carried out research to exploit organic waste and transform them into biological load to create new composite materials, for this reason, I made thermogravimetry analyzes on the two parent materials of my composite, I am looking for is that it is possible to be based on these results to deduce that it is possible to create the alliance, if so how can I analyze the graphical results to do this?
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If two of the components are both organic materials, the simulation is very difficult as the decomposed gas produced during the thermal decomposition can both diffuse through the degrading another component (phase separated) as well as avoid the particle through tortuous paths.(This is an daunting task as you do not know the diffusion coefficient of a constantly degrading organic material through which the fragmented species diffuse through). If one of the component is an inorganic component and only the thermal degradation is the change of the surface species, such as silica, glass flakes, and carbon materials, then you can assume that all the fragmented species do not diffuse through the inorganic particles. Therefore, as long as you know the shape factor, you can then draw a tortuous path and diffusion through this long path.
However, these simulation depends so much on many parameters and accuracy is questionable. Thus, making a composite and run a TGA analysis of the actual composite is much faster and accurate.
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In the case of Ti-alloys, it is confirmed that α stabilizer increases the c/a ratio. What is the mechanism of correlation of the c/a ratio with the unit cell? It is true if increases c/a ratio in HCP structure will linearly decrease unit-cell? or vice versa? What is the mechanism to connect these phenomena?
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Dear Dr.
Ahmad Zafari
Thanks sir.
So, with increasing slightly c/a ratio , is that any correlation mechanism with changing unit cell volume, i.e slightly decrease, increase?
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First of all, whether it is possible to identify the presence of water and its amount on the Silicon substrate by using only FT-IR spectroscopy.
Can ATR-FTIR spectroscopy find out the wettability of a corrugated Silicon surface?
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I am having trouble setting up this problem in HFSS or FEKO. In HFSS, I've tried both FEM and FEBI-IE solvers. With FEKO, I've tried it's MoM solver and default settings. I am would like model model two horn antennas, one in transmit mode and other in receive mode, with a dielectric slab of material in between them. After running the simulations, I'd like to export the s-parameters to apply a material retrieval algorithm like Nicolson-Ross-Weir (NRW) or Newton Raphson to get the permittivity & permeability properties of the dielectric slab.
Link to a paper describing what I'm trying to achieve is below but it was done using CST:
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Hello,
According to your question, I have gone through some papers which I am attaching with it. Kindly go through it, It might be helpful for research.
Thanks,
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I’m doing a simulation of a compression test with an hyperelastic material, defined with Mooney-Rivlin 2 parameters, on Ansys.
I’m obtaining different results making both displacement controlled and load controlled:
If I set a 3 mm linear displacement, I obtain a 30 N force reaction;
If I set a 30 N linear load, I obtain a 4 mm deformation.
I tried changing the strain rate because hyperelastic material should change the deformability with the strain rate, but it doesn’t change at all the results.
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Can you share your Ansys model in .cdb format?
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I know that this is a very difficult question, as the areas of application can vary greatly. However, if you want to operate low as well as high resolution (from a few millimeters to nanometers), need the highest possible beam current for analysis, but also very flexible with regard to large samples or non-conductive samples (low vacuum device), a whole series of devices or manufacturers fall out, as far as I know. If you don't want to constantly change pressure stage apertures, the only manufacturer I can think of at the moment is Zeiss.
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Tijmen Vermeij : you do not exactly know which type of FEI -SEM would be beneficial? I've heard, Mira4 shall be also able to switch between low and high vacuum?
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Hello, I am trying to associate the color of an image to a single numerical value. Images (see attach) correspond to different aloe samples that change in color according to the degree of oxidation (green when there is no oxidation, brown for oxidated ones). I need to associate each image color to a single value since it is the outcome of a design of experiments to evaluate different conditions that can lead (or not) to different degrees of aloe oxidation. I am expecting different color tones for different degrees of oxidation.
I am new to this area, so all recommendation will be really helpful. Thanks!