It is shown that strip theory, that is, treating each chord-wise strip aerodynamically as portion of infinite unswept wing, is exact in determining contribution of any flexible or rigid body mode to generalized aerodynamic force on any rigid body mode; this result is approximation to correct result when second mode involved is flexible mode.
Generalized aerodynamic forces on Delta wing with supersonic leading edges
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 21 , n 11
1954
10 pages
Article (Journal)
English
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Aerodynamic flutter derivatives for flexible wing with supersonic and subsonic edges
Engineering Index Backfile | 1955
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