The properties of 2-D shock wave/turbulent boundary layer interaction flows were calculated by using a compressible turbulent Navier-Stokes numerical computational code. Interaction flows caused by oblique shock wave impingement on the turbulent boundary layer flow were considered. The oblique shock waves were induced with shock generators at angles of attack less than 10 degs in supersonic flows. The surface temperatures were kept at near-adiabatic (ratio of wall static temperature to free stream total temperature) and cold wall (ratio of wall static temperature to free stream total temperature) conditions. The computational results were studied for the surface heat transfer, velocity temperature correlation, and turbulent shear stress in ...
A preliminary experimental investigation was conducted to study two crossing, glancing shock waves o...
AbstractIt is of great significance to improve the accuracy of turbulence models in shock-wave/bound...
Analytical study of separated flows induced by shock wave-boundary layer interactio
Research on the topic of shock wave/turbulent boundary-layer interaction was carried out during the ...
Direct numerical simulations are employed to investigate a shock wave impinging on a turbulent bound...
A computation procedure is described for predicting flow fields which develop when successive intera...
Experimental data for a series of two- and three-dimensional shock wave/turbulent boundary layer int...
An experiment, thoroughly documenting the flow field resulting from the interaction of a shock wave ...
The research performed was an experimental program to help develop turbulence models for shock wave ...
Shock boundary–layer interactions occur in many high-speed aerodynamic flows and they can have a not...
The paper presents results of calculations for 2-D supersonic turbulent compression corner flows. Th...
Turbulent velocity and thermal correlations from direct numerical simulation data of a ...
The feasibility of using streamwise surface heat transfer measurements to detect the presence of flo...
It is of great significance to improve the accuracy of turbulence models in shock-wave/boundary laye...
An analysis of turbulent boundary layer flow characteristics and the computational procedure used ar...
A preliminary experimental investigation was conducted to study two crossing, glancing shock waves o...
AbstractIt is of great significance to improve the accuracy of turbulence models in shock-wave/bound...
Analytical study of separated flows induced by shock wave-boundary layer interactio
Research on the topic of shock wave/turbulent boundary-layer interaction was carried out during the ...
Direct numerical simulations are employed to investigate a shock wave impinging on a turbulent bound...
A computation procedure is described for predicting flow fields which develop when successive intera...
Experimental data for a series of two- and three-dimensional shock wave/turbulent boundary layer int...
An experiment, thoroughly documenting the flow field resulting from the interaction of a shock wave ...
The research performed was an experimental program to help develop turbulence models for shock wave ...
Shock boundary–layer interactions occur in many high-speed aerodynamic flows and they can have a not...
The paper presents results of calculations for 2-D supersonic turbulent compression corner flows. Th...
Turbulent velocity and thermal correlations from direct numerical simulation data of a ...
The feasibility of using streamwise surface heat transfer measurements to detect the presence of flo...
It is of great significance to improve the accuracy of turbulence models in shock-wave/boundary laye...
An analysis of turbulent boundary layer flow characteristics and the computational procedure used ar...
A preliminary experimental investigation was conducted to study two crossing, glancing shock waves o...
AbstractIt is of great significance to improve the accuracy of turbulence models in shock-wave/bound...
Analytical study of separated flows induced by shock wave-boundary layer interactio