Investigation of a Two-step Nozzle in the Langley 11-inch Hypersonic Tunnel
1950-09-01
Sonstige
Keine Angabe
Englisch
BOUNDARY LAYER - NOZZLES , WIND TUNNELS - PRESSURE , AIR FLOW - NOZZLES , NOZZLES, HIGH-PRESSURE , WIND TUNNELS - AIR FLOW , WIND TUNNELS, HYPERSONIC , WIND TUNNEL TESTS - NACA - HYPERSONIC (11 INCHES) , WIND TUNNELS - NACA - HYPERSONIC (11 INCHES) , PHOTOGRAPHY - AIR FLOW - NOZZLES , SCHLIEREN METHOD
Investigation of two-step nozzle in Langley 11-inch hypersonic tunnel
Engineering Index Backfile | 1950
|Engineering Index Backfile | 1950
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