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,
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)
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 01, 1965
- Accession Number
- AD0623298
Entities
People
- F. Edward Ehlers
Organizations
- Boeing