Codes have been written for a fast evaluation of steady, compressible two-dimensional, inviscid flows, either subsonic or transonic, with or without bow shocks and imbedded shocks. The computational speed is provided by a novel sweeping technique, based on the "lambda" integration scheme. The concept has already been successfully applied to one-dimensional problems. Applications can be made to flows inducts, airfoils and blunt bodies in supersonic flight.STATUS: Phase I Only
