Supercritical wing sections. III. [codes K and corrections to H, in FORTRAN IV for CDC 6600]

A survey is given on computational flow research on the design and analysis of supercritical wing sections supported by the National Aeronautics and Space Administration at the Energy Research and Development Administration Mathematics and Computing Laboratory of New York University. The work was performed under NASA Grants NGR 33-016-167 and NGR 33-016-201 and ERDA Contract EY-76-C-02-3077. Computer programs listed and described have applications in the study of flight of modern aircraft at high subsonic speeds. One of the codes generates cascades of shockless transonic airfoils that are expected to increase significantly the efficiency of compressor and turbines. Good simulation of physically observed flows was achieved. 31 figures. (RWR)