Data show that CLmax may vary by as much as 14% depending on altitude and wing loading at which tests are made, position or motion of propeller, and rate at which angle of attack is changing when maximum lift coefficient is obtained.
Flight tests of airplane showing dependence of maximum lift coefficient on test conditions
Nat Advisory Committee Aeronautics -- Tech Note
1937
12 pages
3 Supp plates, 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
|