Shock-induced heating and transition to turbulence in a hypersonic boundary layer
The interaction between an incident shock wave and a Mach-6 undisturbed hypersonic
laminar boundary layer over a cold wall is addressed using direct numerical simulations …
laminar boundary layer over a cold wall is addressed using direct numerical simulations …
Investigating unsteady dynamics of cylinder-induced shock-wave/transitional boundary-layer interactions
Shock-wave/boundary-layer interactions in laminar and fully turbulent boundary layers have
been widely investigated in previous efforts, but relatively little research has been conducted …
been widely investigated in previous efforts, but relatively little research has been conducted …
Unsteady analysis of shock-wave/boundary-layer interaction experiments at Mach 4.2
Using a recently developed Schlieren-based shock-detection algorithm, experiments were
conducted in the 20 in. Mach 6 wind tunnel facility at NASA Langley Research Center to …
conducted in the 20 in. Mach 6 wind tunnel facility at NASA Langley Research Center to …
Image-based analysis of shock-wave/boundary-layer interaction unsteadiness
SHOCK-wave/boundary-layer interactions (SWBLIs) in laminar and turbulent boundary
layers have been studied extensively over the past several decades [1, 2] with unsteadiness …
layers have been studied extensively over the past several decades [1, 2] with unsteadiness …
High-speed Schlieren imaging of cylinder-induced hypersonic-shock-wave–boundary-layer interactions
High-speed schlieren imaging was implemented to monitor the shock structure and quantify
the flow dynamics of a cylinder-induced shock-wave–boundary-layer interaction (SBLI) as …
the flow dynamics of a cylinder-induced shock-wave–boundary-layer interaction (SBLI) as …
RANS-based numerical simulation of shock wave/turbulent boundary layer interaction induced by a blunted fin normal to a flat plate
E Kolesnik, E Smirnov, A Smirnovsky - Computers & Fluids, 2022 - Elsevier
Results of refined RANS-based numerical simulation of shock wave/turbulent boundary
layer interaction induced by a blunted fin mounted on a flat plate are presented. The RANS …
layer interaction induced by a blunted fin mounted on a flat plate are presented. The RANS …
Investigation of a Cylinder-Induced Transitional Shock Wave-Boundary Layer Interaction using Laser Diagnostics
Shock wave-boundary layer interactions (SWBLI) are a fundamental unsteady flow
phenomenon experienced during supersonic flight and have thus been a focus of active …
phenomenon experienced during supersonic flight and have thus been a focus of active …
Study of the dynamics of transitional shock wave-boundary layer interactions using optical diagnostics
Shock wave-boundary layer interactions (SWBLI) are a significant source of uncertainty in
the analysis of supersonic flows and pose a technical challenge to the development of air …
the analysis of supersonic flows and pose a technical challenge to the development of air …
Experimental investigation of a cylinder-induced transitional shock wave-boundary layer interaction
HOCK wave-boundary layer interactions (SWBLI) are a significant source of uncertainty in
the analysis of supersonic flows and pose a technical challenge to the development of air …
the analysis of supersonic flows and pose a technical challenge to the development of air …
Analysis of shock-wave/boundary-layer interaction experiments at mach 1.8 and mach 4.2
Shock-wave/boundary-layer interactions (SWBLI) are a fundamental unsteady flow
phenomenon experienced during supersonic flight and have thus been a focus of active …
phenomenon experienced during supersonic flight and have thus been a focus of active …