AN IBM 7090 PROGRAM FOR COMPUTING TWO-DIMENSIONAL AND AXIALLY – SYMMETRIC SUPERSONIC FLOW OF AN IDEAL GAS SUPPLEMENT I. SUBROOUTINES FOR COMPUTING THE SHOCK AND FREE STREAMLINE DIVIDING TWO REGIONS OF NON-UNIFORM SUPERSONIC FLOW

摘要

Methods for computing a shock wave and also a free streamline dividing two regions of is energetic supersonic flow are explained with computed examples of both two-dimensional 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.