Perforated wall nozzle providing variable Mach number supersonic flow for external stream simulation in rocket propulsion tests
A new concept of a variable-Mach-number perforated wall nozzle for providing a supersonic external stream in rocket-propulsion testing.
FLIGHT TEST, SIMULATION AND SUPPORT CONFERENCE ; 1968 ; LOS ANGELES, CA
1968-03-01
Conference paper
No indication
English