Theoretical methods developed by G.B.WHITMAN and F.WALKDEN are used to study possibilities of using aerodynamic interference to reduce or suppress shock wave noise due to lift by conventional aircraft; wind tunnel experiments with wing body configurations are conducted and are analyzed in light of theoretical indications.
Shock wave noise of supersonic aircraft
SAE -- Paper
SAE Meeting ; 1960 Noise
1960
12 pages
Conference paper
English
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SHOCK WAVE NOISE OF SUPERSONIC AIRCRAFT
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