Perturbations of N-shaped acoustic wave packet produced by aircraft motion are analyzed for case when N approaches caustic curve; equation is derived for maximum boom intensity in focalization zone.
Geometrical acoustics, sonic boom of supersonic aircraft, and focalization
Acoustique geometrique, bruit balistique des avions supersoniques et focalisation
Journal de Mecanique ; 4 , n 2
1965
53 pages
Article (Journal)
English
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