Analytical procedure used to modify design of high-pressure-ratio nozzles to reduce vibration during start-up and shutdown. Nozzles used in jet engines, laser nozzles and diffusers, wind tunnels, gas turbines and rocket engines.
Supersonic-Nozzle Shock-Wave Analysis
NASA Tech Briefs ; 8 , 2
1984-11-01
Miscellaneous
No indication
English
Unsteady Pressure-Sensitive Paint Measurement for Oscillating Shock Wave in Supersonic Nozzle
British Library Conference Proceedings | 2008
|Shock wave noise of supersonic aircraft
Engineering Index Backfile | 1960
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