Accession Number:

AD0623298

Title:

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,

Personal Author(s):

Corporate Author:

BOEING SCIENTIFIC RESEARCH LABS SEATTLE WASH MATHEMATICS RESEARCH LAB

Report Date:

1965-08-01

Abstract:

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

Supplementary Note:

Also available from the author.

Pages:

0053

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File Size:

0.00MB

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