Whitham's theory for predicting boom intensity is combined with lifting effects to assess shock noise of aircraft flying at supersonic speeds; investigation limited to steady level flight conditions; boom intensity evaluated at ground points along aircraft's track.
Investigation of lifting effects on intensity of sonic booms
Roy Aeronautical Soc -- J
Royal Aeronautical Society -- Journal ; 64 , n 598
1960
7 pages
Article (Journal)
English
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