The analysis uses a compressibility transformation and utilizes higher order closure rules to complete the transformation. By requiring that the momentum equations in differential form be satisfied at the wall and at the sublayer edge, correspondence rules are obtained which relate the variable property (VP) flow to a constant property (CP) flow in which mass transfer and pressure gradient occur simultaneously. A new CP formulation is developed and numerical results for a variety of cases are presented. Comparisons with earlier forms of the transformation and with experiment are included. For the zero pressure gradient case some differences between the various predictions are observed. For the several pressure gradient cases examined, the r...
A modified form of the wall-wake profile which is applicable to flows with heat transfer is presente...
The development of an invariant model designed expressly for the computation of shear flows is discu...
A transformation is derived from first principles to reduce the boundary-layer equations for a gener...
An analysis of the incompressible turbulent boundary layer, developing under the combined effects of...
Compressibility transformation properties and high speed turbulent boundary layer flow with mass tra...
Calculation of compressible turbulent boundary layers with pressure gradients and heat transfe
A computer program is described capable of determining the properties of a compressible turbulent bo...
Computer program for determining properties of high speed turbulent boundary layer with heat transfe...
An analysis of the incompressible turbulent boundary layer, developing under the combined effects of...
Behavior of high speed turbulent boundary layer with heat transfer and streamwise pressure gradien
Equations and closure methods for compressible turbulent boundary layers are discussed. Flow phenome...
A computer program was developed to do the calculations for two-dimensional or axisymmetric configur...
Computer program predicts growth of boundary layers along any surface where air is flowing. Two inte...
Attached supersonic turbulent boundary layers, with a wide range of adverse pressure gradient streng...
A modified Reynolds analogy between skin friction and heat transfer which depends upon local pressur...
A modified form of the wall-wake profile which is applicable to flows with heat transfer is presente...
The development of an invariant model designed expressly for the computation of shear flows is discu...
A transformation is derived from first principles to reduce the boundary-layer equations for a gener...
An analysis of the incompressible turbulent boundary layer, developing under the combined effects of...
Compressibility transformation properties and high speed turbulent boundary layer flow with mass tra...
Calculation of compressible turbulent boundary layers with pressure gradients and heat transfe
A computer program is described capable of determining the properties of a compressible turbulent bo...
Computer program for determining properties of high speed turbulent boundary layer with heat transfe...
An analysis of the incompressible turbulent boundary layer, developing under the combined effects of...
Behavior of high speed turbulent boundary layer with heat transfer and streamwise pressure gradien
Equations and closure methods for compressible turbulent boundary layers are discussed. Flow phenome...
A computer program was developed to do the calculations for two-dimensional or axisymmetric configur...
Computer program predicts growth of boundary layers along any surface where air is flowing. Two inte...
Attached supersonic turbulent boundary layers, with a wide range of adverse pressure gradient streng...
A modified Reynolds analogy between skin friction and heat transfer which depends upon local pressur...
A modified form of the wall-wake profile which is applicable to flows with heat transfer is presente...
The development of an invariant model designed expressly for the computation of shear flows is discu...
A transformation is derived from first principles to reduce the boundary-layer equations for a gener...