Modeling Mach Number and Temperature Distributions in Supersonic Nozzle Flow
46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
2010-01-01
Conference paper
Electronic Resource
English
Mach Number and Temperature Effects on Mach Wave Emission from Supersonic Jets
British Library Conference Proceedings | 2008
|Attenuation of sound in a low mach number nozzle flow
TIBKAT | 1979
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