Pressure signatures of F-100, F-104, and B-58 aircraft at distances from 120 to 425 ft from generating aircraft and at Mach numbers from 1.2 to 1.8 are shown; calculations made by using G.B.Whitham's method gave good agreement with experimental results; procedure for calculating F(y) function used relating to flow field is also given.
Experimental and calculated flow fields produced by airplanes flying at supersonic speeds
NASA -- Tech Note
1960
24 pages
Article (Journal)
English
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Welding keeps airplanes flying
Tema Archive | 1978
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