Perforated wall nozzle providing variable Mach number supersonic flow for external stream simulation in rocket propulsion tests
A perforated-wall nozzle for variable Mach number testing.
FLIGHT TEST, SIMULATION AND SUPPORT CONFERENCE ; 1968 ; LOS ANGELES, CA
1968-09-01
Miscellaneous
No indication
English
Optimization design of variable Mach number wind tunnel nozzle by rotating profile
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