Add to ORKGMethod for predicting compressible turbulent boundary layers in adverse pressure gradients applied to hypersonic air breathing propulsio
Several methods for predicting the separation point for a compressible turbulent boundary layer were...
Mathematical analysis of Reynolds analogy for turbulent heat transfer, skin friction, and boundary l...
Compressibility transformation properties and high speed turbulent boundary layer flow with mass tra...
Computer program predicts growth of boundary layers along any surface where air is flowing. Two inte...
Measurements have been made of the mean-flow and turbulence properties in adiabatic turbulent bounda...
The hypersonic compressible turbulent boundary layer in an adverse pressure gradient along a cylindr...
An integral method for predicting boundary layer development in turbulent flow regions on two-dimens...
Calculation of compressible turbulent boundary layers with pressure gradients and heat transfe
A computer program was developed to do the calculations for two-dimensional or axisymmetric configur...
An analysis of the incompressible turbulent boundary layer, developing under the combined effects of...
A differential method is proposed for the prediction of a broad range of turbulent boundary layers o...
A wind-tunnel model was developed to study the two-dimensional turbulent boundary layer in adverse a...
Methods of predicting integral parameters and skin friction coefficients of turbulent boundary layer...
A wind-tunnel model was developed to study the two-dimensional turbulent boundary layer in adverse a...
Attached supersonic turbulent boundary layers, with a wide range of adverse pressure gradient streng...
Several methods for predicting the separation point for a compressible turbulent boundary layer were...
Mathematical analysis of Reynolds analogy for turbulent heat transfer, skin friction, and boundary l...
Compressibility transformation properties and high speed turbulent boundary layer flow with mass tra...
Computer program predicts growth of boundary layers along any surface where air is flowing. Two inte...
Measurements have been made of the mean-flow and turbulence properties in adiabatic turbulent bounda...
The hypersonic compressible turbulent boundary layer in an adverse pressure gradient along a cylindr...
An integral method for predicting boundary layer development in turbulent flow regions on two-dimens...
Calculation of compressible turbulent boundary layers with pressure gradients and heat transfe
A computer program was developed to do the calculations for two-dimensional or axisymmetric configur...
An analysis of the incompressible turbulent boundary layer, developing under the combined effects of...
A differential method is proposed for the prediction of a broad range of turbulent boundary layers o...
A wind-tunnel model was developed to study the two-dimensional turbulent boundary layer in adverse a...
Methods of predicting integral parameters and skin friction coefficients of turbulent boundary layer...
A wind-tunnel model was developed to study the two-dimensional turbulent boundary layer in adverse a...
Attached supersonic turbulent boundary layers, with a wide range of adverse pressure gradient streng...
Several methods for predicting the separation point for a compressible turbulent boundary layer were...
Mathematical analysis of Reynolds analogy for turbulent heat transfer, skin friction, and boundary l...
Compressibility transformation properties and high speed turbulent boundary layer flow with mass tra...