Box method for obtaining generalized air forces on oscillating wing in supersonic flow consists of representing wing by grid of square boxes and determining influence of one box on another; aerodynamic pressure influence coefficients when tabulated, permit flutter analysis of arbitrary wing with arbitrary normal modes to be carried out in routine way.
Aerodynamic flutter derivatives for flexible wing with supersonic and subsonic edges
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 22 , n 10
1955
8 pages
Aufsatz (Zeitschrift)
Englisch
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Generalized aerodynamic forces on Delta wing with supersonic leading edges
Engineering Index Backfile | 1954
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