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    Computer program for calculating the flow field of supersonic ejector nozzles (1974)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: An analytical procedure for computing the performance of supersonic ejector nozzles is presented. This procedure includes real sonic line effects and an interaction analysis for the mixing process between the two streams. The procedure is programmed in FORTRAN 4 and has operated successfully on IBM 7094, IBM 360, CDC 6600, and Univac 1108.
    Keywords: PROPULSION SYSTEMS
    Type: NASA-TN-D-7602 , E-7476
    Format: application/pdf
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