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Computer Program for Calculating Supersonic Flow about Circular, Elliptic, and Bielliptic Cones by the Method of Lines
E. B. Klunker
Jerry Curtis South
Ruby M. Davis
出版
National Aeronautics and Space Administration
, 1972
URL
http://books.google.com.hk/books?id=Exb-HAAACAAJ&hl=&source=gbs_api
註釋
A user's manual for a computer program which calculates the supersonic flow about circular, elliptic, and bielliptic cones at incidence and elliptic cones at yaw by the method of lines is presented. The program is automated to compute a case from known or easily calculated solution by changing the parameters through a sequence of steps. It provides information including the shock shape, flow field, isentropic surface properties, entropy layer, and force coefficients. A description of the program operation, sample computations, and a FORTRAN 4 listing are presented.
