Add to ORKGHypervelocity wind tunnel investigation of turbulent boundary undergoing adverse pressure gradient and cross flow along plane of symmetr
A wind-tunnel model was developed to study the two-dimensional turbulent boundary layer in adverse a...
Hypersonic airbreathing propulsion has been under research since the mid 1960s and will continue to...
Method for predicting compressible turbulent boundary layers in adverse pressure gradients applied t...
Crossflow effects on compressible turbulent boundary layer over bodies of revolutio
Attached supersonic turbulent boundary layers, with a wide range of adverse pressure gradient streng...
Measurements have been made of the mean-flow and turbulence properties in adiabatic turbulent bounda...
An investigation was conducted on a turbulent boundary layer near a smooth surface with pressure gra...
The hypersonic compressible turbulent boundary layer in an adverse pressure gradient along a cylindr...
Behavior of high speed turbulent boundary layer with heat transfer and streamwise pressure gradien
Measurements have been made of the mean flow properties and turbulent fluctuations in adiabatic turb...
A detailed study of two strong adverse pressure gradient flows, one with a free-stream velocity of 3...
Evaluation of turbulent shear models and prediction of compressible turbulent boundary layers by met...
The title of this presentation is the title of our research grant. While transition study is the obj...
A survey of turbulence measurements in compressible flows is presented. The majority of turbulence m...
A wind-tunnel model was developed to study the two-dimensional turbulent boundary layer in adverse a...
A wind-tunnel model was developed to study the two-dimensional turbulent boundary layer in adverse a...
Hypersonic airbreathing propulsion has been under research since the mid 1960s and will continue to...
Method for predicting compressible turbulent boundary layers in adverse pressure gradients applied t...
Crossflow effects on compressible turbulent boundary layer over bodies of revolutio
Attached supersonic turbulent boundary layers, with a wide range of adverse pressure gradient streng...
Measurements have been made of the mean-flow and turbulence properties in adiabatic turbulent bounda...
An investigation was conducted on a turbulent boundary layer near a smooth surface with pressure gra...
The hypersonic compressible turbulent boundary layer in an adverse pressure gradient along a cylindr...
Behavior of high speed turbulent boundary layer with heat transfer and streamwise pressure gradien
Measurements have been made of the mean flow properties and turbulent fluctuations in adiabatic turb...
A detailed study of two strong adverse pressure gradient flows, one with a free-stream velocity of 3...
Evaluation of turbulent shear models and prediction of compressible turbulent boundary layers by met...
The title of this presentation is the title of our research grant. While transition study is the obj...
A survey of turbulence measurements in compressible flows is presented. The majority of turbulence m...
A wind-tunnel model was developed to study the two-dimensional turbulent boundary layer in adverse a...
A wind-tunnel model was developed to study the two-dimensional turbulent boundary layer in adverse a...
Hypersonic airbreathing propulsion has been under research since the mid 1960s and will continue to...
Method for predicting compressible turbulent boundary layers in adverse pressure gradients applied t...