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
01.09.1968
Sonstige
Keine Angabe
Englisch
Design and calibration of variable Mach Number nozzle
Engineering Index Backfile | 1955
|Perforated Walls Interference Corrections for Models Testing at High Subsonic Mach Number
British Library Conference Proceedings | 1993
|