Flight test data obtained at altitude of 5000 ft are analyzed to determine effects of airplane vertical translation and pitching motions; power spectral techniques used to determine contributions of these motions to angles of attack; results compared with direct gust induced angle of attack.
Experimental measurements of effects of airplane motions on wing and tail angles of attack of swept-wing bomber in rough air
NACA -- Tech Note
1958
25 pages
Report
Englisch
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Measurements of motions of large swept-wing airplane in rough air
Engineering Index Backfile | 1958
|Engineering Index Backfile | 1959
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