Aswin M RUniversity of Illinois, Urbana-Champaign | UIUC · Department of Aerospace Engineering
Aswin M R
Master of Engineering
Pursuing MEng in Aerospace Systems Engineering at University of Illinois Urbana Champaign
About
5
Publications
1,269
Reads
How we measure 'reads'
A 'read' is counted each time someone views a publication summary (such as the title, abstract, and list of authors), clicks on a figure, or views or downloads the full-text. Learn more
3
Citations
Introduction
Currently, I'm a master's student at University of Illinois Urbana-Champaign undertaking Master of Engineering Aerospace Systems Engineering. I've been working in the CFD section for almost two years. My other strong domains include mathematics, aerodynamics and orbital space flight mechanics. Currently into software based numerical calculations.
And feel free to contact me anytime for research collab.
Additional affiliations
January 2024 - July 2024
Position
- Graduate Apprentice
Description
- - Performed IR thermal testing in vacuum and ambient conditions on various specimen models using IR Lamps upto 100 W/cm2 heat flux. - Design and ray tracing analysis done on 500 mm filament IR Lamp positioned on a High-Performance Radiant Heater (HPRH) which is simulated to conduct 130 W/cm2 heat flux over 200x200mm specimen surface uniformly. - Testing of CO2 LASER of 80W done on 50x50mm specimen surface with the help of LASER Power Meter and Thermophile Sensor.
Education
August 2024 - December 2025
July 2019 - July 2023
Publications
Publications (5)
The purpose of this paper is to get a complete study of flow parameters over a typical solid rocket motor and further analyze it according to the desired particular needs. Solid rocket motor consists of key inert components, namely the motor case, igniter case, and nozzle. The motor attached to the thrust vector control mechanism in a large-scale r...
![Fig. 4. Heat exchange-nozzle cross section [ 28 ] .](profile/Aswin-M-R/publication/377794784/figure/fig4/AS:11431281277504257@1726101386067/Heat-exchange-nozzle-cross-section-28_Q320.jpg)
![Fig. 5. MEMS based 3-Watt CMOS resistojet [30] .](profile/Aswin-M-R/publication/377794784/figure/fig5/AS:11431281277512956@1726101386661/MEMS-based-3-Watt-CMOS-resistojet-30_Q320.jpg)
Resistojets generate heat by passing an electric current through a resistive element, thereby heating a propellant at high pressure, which is subsequently expanded through a nozzle resulting in a supersonic exhaust jet. Specific impulse of a resistojet decides the performance of the thruster. Hence the goal here is to achieve highest specific impul...
A CubeSat is a scaled-down satellite usually having less than 10 kg of mass and is used for various applications including communication, navigation, Internet, and so on. The components required for a 3U satellite have been discussed in this paper. The structural design has been done based on the results achieved through static structural and vibra...
This paper is mainly focused on Supersonic Laminar Flow at Mach 3 for biconvex and double wedge airfoils. The coefficient of lift (Cl), coefficient of drag (Cd), and coefficient of moment along the respective airfoils are being analysed. The geometry of these is generated using the Designmodeler of ANSYS. Further, meshing is also achieved by ANSYS...
