Type of flow is associated with thrust vector control of rocket motors by gas injection, and occurs when gaseous fuel is injected into supersonic burner; analytic model of flow-field was constructed in which conservation of momentum is applied to control volume at jet nozzle exit; series of flat-plate experiments was conducted with normal, sonic jets at external flow Mach numbers of 2.61, 3.50, and 4.54; comparisons of trends predicted by analysis with two-dimensional force data from experiments and other sources showed good agreement; results of correlation of data obtained from experiments with finite-span slots.
Study of interaction of gaseous jets from transverse slots with supersonic external flows
AIAA J
AIAA Journal ; 6 , n 2
1968
8 pages
Article (Journal)
English
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Penetration of Gaseous Jets in Supersonic Flows
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