SCHRENK'S method for finding the wing lift distribution which has already been given in AIRCRAFT ENGINEERING can be taken further in order to determine the Pitching Moment Coefficient, CM0, about the quarter-chord point of the mean chord at no-lift.
Wing Pitching Moment Coefficient
Aircraft Engineering and Aerospace Technology ; 17 , 7 ; 204-205
1945-07-01
2 pages
Article (Journal)
Electronic Resource
English
Wing pitching moment coefficient
Engineering Index Backfile | 1945
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