Determination of pressure distribution over thin, finite wing in supersonic flow due to prescribed incidence that varies slowly in time (so that square of reduced frequency may be regarded as negligible) is reduced to pair of steady flow problems.
First-order formulation of unsteady supersonic flow problem for finite wings
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 23 , n 6
1956
5 pages
Aufsatz (Zeitschrift)
Englisch
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First-order theory for unsteady motion of thin wings at supersonic speeds
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