Results are presented of a flight investigation conducted to survey the flow field generated by airplanes flying a t supersonic speeds. The pressure signatures of an F-100, an F-104, and a B-58 airplane, representing widely varying configurations, a t distances from 120 t o 425 f e e from the generating aircraft and at Mach numbers from 1.2 t o 1.8 are shown. Calculations were made by using Whitham's method and were compared with the experimental results.
Experimental and Calculated Flow Fields Produced by Airplanes Flying at Supersonic Speeds
1960-11-01
Sonstige
Keine Angabe
Englisch
Experimental and calculated flow fields produced by airplanes flying at supersonic speeds
Engineering Index Backfile | 1960
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Tema Archiv | 1978
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|Engineering Index Backfile | 1938
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