Theory for calculation of total forces acting on purely supersonic wings; method applies to wings having arbitrary downwash distribution (stationary or nonstationary) and is valid whenever all of wing edges are supersonic; general 3-dimensional nonstationary problem is reduced to equivalent 2-dimensional problem.
Nonstationary motion of purely supersonic wings
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 18 , n 5
1951
13 pages
Article (Journal)
English
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