It was found that, when airplane was rotated positively in pitch through angle of stall at rates of order of 0.1° per second, maximum lift coefficient was considerably higher than that obtained in standard tests, in which forces are measured with angles of attack fixed; all tests made on Fairchild 22. (10¢)
Comparative flight and full-scale wind-tunnel measurements of maximum lift of airplane
Nat Advisory Committee Aeronautics -- Report
1938
7 pages
Bibliography
Report
Englisch
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Comparative flight and full-scale wind tunnel measurements of maximum lift of airplane
Engineering Index Backfile | 1938
|Comparative flight and full-scale wind-tunnel measurements of maximum lift of airplane
Engineering Index Backfile | 1938
|