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Volume 12 Issue 07
July 2026
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Author(s)
Dr. Nirmal Kumar Kund
Abstract
In The Present Research, A 2D Numerical Model Is Developed To Investigate Supersonic Turbulent Fluid Flow Over A Backward Facing Sharp Edge Step By Using Hybrid RANS-LES Model. It Pertains To The Spalart-Allmaras Model Involving A Viscosity-like Variable
Keywords
Supersonic
Turbulent Flow
Backward Facing
Sharp Edge Step
Hybrid RANS-LES
Lip Shock.
Paper ID
IJSARTV3I1218142
Publication Date
December 2, 2017
Research Area
Production Engineering