CFD based 3D aero analysis system for high-speed mixer-ejector exhaust nozzles
30th Joint Propulsion Conference and Exhibit ; 1994 ; Indianapolis , IN , U.S.A.
1994-01-01
Conference paper
Electronic Resource
English
CFD Based 3D Aero Analysis System For High-Speed Mixer-Ejector Exhaust Nozzles
British Library Conference Proceedings | 1994
|A method for estimating thrust for mixer/ejector nozzles
AIAA | 1998
|