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Volume 12 Issue 07
July 2026
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Author(s)
Dr. Nirmal Kumar Kund
Abstract
The Current Study Encompasses The Development Of A Suitable Numerical Model Concerning The Supersonic Flow Past A Three-dimensional Open Cavity With Length-to-depth Ratio Of 2. The Mach Number Of The Supersonic Free-stream Is 2 In Addition The Reynolds Nu
Keywords
Numerical Simulation
Open Cavity
Spoiler
LES
Velocity Vector
OASPL.
Paper ID
IJSARTV4I119561
Publication Date
January 15, 2018
Research Area
Mechanical Engineering