AXIALLY SYMMETRIC, INVISCID, REAL GAS, NON-ISOENERGETIC FLOW SOLUTION BY THE METHOD OF CHARACTERISTICS
Final rept. Jun 1967-Jun 1968
ARO INC ARNOLD AFS TN
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A numerical procedure is presented for the solution of the characteristic equations for a non-isoenergetic, supersonic, real gas jet expanding into a constant pressure ambience. Included is a procedure for inserting the expansion fan and the embedded shock. Examples are given for high temperature argon jets with radiation.
- Fluid Mechanics