Flow fields around asymmetrical micro vortex generators in supersonic flow
L Hristozova, R Sebastian, AM Schreyer - Aerospace Science and …, 2024 - Elsevier
Motivated by the favorable effects of asymmetrical vortical structures on shock-wave
boundary layer interactions, we performed implicit large-eddy simulations to analyze the …
boundary layer interactions, we performed implicit large-eddy simulations to analyze the …
[HTML][HTML] Design considerations for efficient spanwise-inclined air-jet vortex generators for separation control in supersonic and hypersonic flows
R Sebastian, AM Schreyer - Aerospace Science and Technology, 2024 - Elsevier
Shock-wave/boundary-layer interactions and associated flow separation are frequently
occurring phenomena in many high-speed flow applications. Injection of spanwise-inclined …
occurring phenomena in many high-speed flow applications. Injection of spanwise-inclined …
[PDF][PDF] Control of shock-induced flow separation with Air-Jet vortex generators
DP Ramaswamy - 2023 - researchgate.net
Shock-wave/boundary-layer interactions (SWBLIs) are complex flowfields commonly
encountered in many high-speed aerospace applications. A strong shock wave imposes a …
encountered in many high-speed aerospace applications. A strong shock wave imposes a …