Investigation of flow field set up by transverse gas jet issuing into supersonic stream, such as occurring in applications to jet-flaps and to thrust vector control for rocket motors; results of wall and impact pressure measurements throughout core of interaction field, and flow visualization tests, are reported for 11 tests differing by injected mass rate, injection station Mach number, and primary to secondary stagnation pressure ratio; measurements are used to reconstruct true structure of flow and suggest characteristic features which are outlined.
Interaction of supersonic stream and transverse supersonic jet
AIAA J
AIAA Journal ; 2 , n 11
1964
8 pages
Article (Journal)
English
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