COMPBLII: Compressible, variable pressure boundary layer program for arbitrary gaseous mixtures
Abstract
A code has been written to calculate the boundary layer over a body for a compressible, variable pressure flow with an arbitrary gaseous mixture. This code was written to handle internal flows as well as external flows. For this reason, combustion gases at elevated temperatures are of interest and are treated. The boundary layer equations are solved using an integral technique.
 Publication:

NASA STI/Recon Technical Report N
 Pub Date:
 October 1981
 Bibcode:
 1981STIN...8411427A
 Keywords:

 Boundary Layer Flow;
 Compressible Flow;
 Computer Programs;
 Computerized Simulation;
 Two Dimensional Flow;
 Gas Mixtures;
 Laminar Boundary Layer;
 Least Squares Method;
 Pressure Gradients;
 Reynolds Number;
 Thermal Conductivity;
 Fluid Mechanics and Heat Transfer