[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 …
Study of Effect of Protrusions on Cones in Hypersonic Flow
VCM Chandrakumar, SR Nagaraja - Recent Developments in Mechanics …, 2022 - Springer
Protrusions are the discontinuities on the surface. It can be sheet joints or control surfaces
that cause protrusion. In low speed flow, the boundary layer thickness is higher so that …
that cause protrusion. In low speed flow, the boundary layer thickness is higher so that …