Object of paper is to obtain lower bounds for resulting sonic boom, in track of aircraft, by appropriate design of aircraft geometry; aircraft, flying straight and level at supersonic speeds, is subject to various constraints on its total lift, volume, area distribution and center-of-pressure position.
Lower bounds for sonic bangs in far field
Aeronautical Quarterly
Aeronautical Quarterly ; 18 , Part 1
1967
21 pages
Article (Journal)
English
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