In design of high speed aircraft, problem of relating structure loads to prescribed flight envelope leads often to necessity of airframes being considerably stronger than past experience suggests; one aspect of problem considered, namely, influence of elasticity upon aircraft derivatives from which tail loads are computed.
Aspect of deformation of swept wings in steady supersonic flight
Roy Aeronautical Soc -- J
Royal Aeronautical Society -- Journal ; 58 , n 527
1954
11 pages
Article (Journal)
English
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