NASA NTRS · 19740012321
Computer program for calculating the flow field of supersonic ejector nozzles
Abstract
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.
Keep this discovery
Explore connections, maps & timelines
Anderson, B. H.. 1974-04-01. Computer program for calculating the flow field of supersonic ejector nozzles. https://ntrs.nasa.gov/citations/19740012321
Cite the original work for its findings. Save a collection to share your selection of sources.