The present report discusses launcher flow-field data from complementary cold-gas test programs conducted at the University of Texas at Austin. Based on these data, flow-field models for the constrictive launcher configurations have been defined as a function of the nozzle-exit location and of the stagnation pressure in the nozzle reservoir. The conclusions are based on the configurations of the present experimental program.
Experimental Study of an Underexpanded, Supersonic Nozzle Exhausting into a Constrictive Launch Tube
1975
61 pages
Report
No indication
English
Underexpanded jets exhausting from a rectangular channel into a slot ambient space
American Institute of Physics | 2021
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