A computer program is described capable of determining the properties of a compressible turbulent boundary layer with pressure gradient and heat transfer. The program treats the two-dimensional problem assuming perfect gas and Crocco integral energy solution. A compressibility transformation is applied to the equation for the conservation of mass and momentum, which relates this flow to a low speed constant property flow with simultaneous mass transfer and pressure gradient. The resulting system of describing equations consists of eight ordinary differential equations which are solved numerically. For Part 1, see N72-12226; for Part 2, see N72-15264.Computer program manual J. Schneider, J. Boccio ... SIMQ The service routine, identical in both programs, except for a single common block in the PILOT2 version, solves the system of linear ordinary differential equations AY = B by matrixanbsp;...
|Title||:||Calculation of Turbulent Boundary Layers with Heat Transfer and Pressure Gradient Utilizing a Compressibility Transformation|
|Author||:||J. Schneider, J. Boccio|