From power spectral techniques, frequency-response functions are obtained for deflection and twist responses at three spanwise locations to vertical gusts, and results compared with those obtained for reference quasi-static aircraft; analysis of effects of deflection velocity and twisting motions on local angles of attack.
Analysis of flight-test measurements of wing structural deformations in rough air of large flexible swept-wing airplane
NASA -- Memo
1959
46 pages
Aufsatz (Zeitschrift)
Englisch
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Some structural response characteristics of large flexible swept-wing airplane in rough air
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