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Volume 12 Issue 07
July 2026
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Author(s)
Dr. Nirmal Kumar Kund
Abstract
A Suitable Numerical Model Is Developed To Estimate Supersonic Flow Past A 3D Open Cavity. The Studies Involve Supersonic Flow Over The 3D Open Cavity Having Length-to-depth Ratio Of 2, Including The Supersonic Free-stream Mach Number Of 2 In Addition To
Keywords
Numerical Simulation
Cavity
LES
Velocity Vector
Coefficient Of Pressure
OASPL.
Paper ID
IJSARTV4I119541
Publication Date
January 12, 2018
Research Area
Production Engineering