DID YOU KNOW? DTIC has over 3.5 million final reports on DoD funded research, development, test, and evaluation activities available to our registered users. Click HERE
to register or log in.
AN IBM 7090 PROGRAM FOR COMPUTING TWODIMENSIONAL AND AXIALLY-SYMMETRIC SUPERSONIC FLOW OF AN IDEAL GAS. SUPPLEMENT I. SUBROUTINES FOR COMPUTING THE SHOCK AND FREE STREAMLINE DIVIDING TWO REGIONS OF NONUNIFORM SUPERSONIC FLOW,
BOEING SCIENTIFIC RESEARCH LABS SEATTLE WASH MATHEMATICS RESEARCH LAB
Methods for computing a shock wave and also a free streamline dividing two regions of isoenergetic supersonic flow are explained with computed examples of both twodimensional and axially-symmetric flows. The subroutines as coded in FORTRAN language for the IBM 7094 are listed and the procedures for their use are described. Author
Also available from the author.