Procedure determines supersonic-nozzle contours that allow higher nozzle-exit wall pressures, reducing chamber pressure without causing wall-flow separation as encountered in optimum large-area-ratio nozzle designs. Procedure applies to chemical-laser nozzles, jet-engine and gas turbines, wind tunnels and rocket nozzles.
Nonseparating High-Area-Ratio Supersonic Nozzles
NASA Tech Briefs ; 8 , 2
01.11.1984
Sonstige
Keine Angabe
Englisch
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