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
Article (Journal)
English
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Measurements of motions of large swept-wing airplane in rough air
Engineering Index Backfile | 1958
|Engineering Index Backfile | 1958
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