Advances in Aerodynamics is affiliated with Computational Aerodynamics Institute, China Aerodynamics Research and Development Center and Chinese Aerodynamics Research Society.
Influence of the shock wave-turbulence interaction on the swirl distortion in hypersonic inlet
This study uses the Large Eddy Simulation (LES) technique to conduct an exhaustive analysis of the flow characteristics within the Rectangular-to-Elliptical shape Transition (REST) inlet under Mach 6 condition...