NASA NTRS · 19830000656
Supersonic-Nozzle Shock-Wave Analysis
Abstract
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.
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Wagner, W. R., Ratekin, G. H.. 1984-11-01. Supersonic-Nozzle Shock-Wave Analysis. https://ntrs.nasa.gov/citations/19830000656
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