Analysis of Aerodynamic Composites & Advanced Materials Using Modeling & Simulation for Blended/Hybrid Wing Body Designs
2022-26-1136
05/26/2022
- Event
- Content
- In the Era of 21st Century, accurate precision, performance and advancement of surface of high speed Aerospace Vehicle is essentially necessary with the type of material, selection of wing type, determination of dimensioning and performance factors with the proper propulsion analysis. For certain critical applications the characterization of any hybrid design of any high speed vehicle is necessary especially in its full trajectory which requires number of various or spontaneous Computational Fluid Dynamics (CFD) calculations with different analytical factors. Performing the detailed CFD calculations, design factors using CATIA V5, MATLAB, Solid works & ANSYS for different flow conditions and geometries. We observed that performance factor of our given design model gave efficient and long endurance varying the coefficient scale of heat transfer during the steady flight time maintaining the difference in temperature of our hybrid design model and it's skin temperature. We used our simple prepared composite material which is sturdy, cost effective and easy for self-destruction during any defense flight operation through a command line protocols which is proposed to perform all operations with calculative long flight endurance with the methodology where our CFD simulations are done to validate the number of high performance speed cases which involves the Aerodynamic heat along with the control of high speed aerodynamic flow as well. The computational analysis of heat, material, design ratios and surface temperature gave us the matches of well performed experimental and flight endurance data. Keywords: Hybrid Design, Computational Fluid Dynamics, Thermal Analysis, Aerodynamic Flow, UAV Surfacing, Composite Material.
- Citation
- Kaushik, I., and Saini, S., "Analysis of Aerodynamic Composites & Advanced Materials Using Modeling & Simulation for Blended/Hybrid Wing Body Designs," SAE Technical Paper 2022-26-1136, 2022, .