O. SCHRENK's method for finding wing lift distribution can be taken further in order to determine pitching moment coefficient about quarter-chord point of mean chord at no-lift; fore and aft position of standard mean chord. See also Engineering Index 1944 p 57.
Wing pitching moment coefficient
Aircraft Eng
Aircraft Engineering ; 17 , n 197
1945
2 pages
Article (Journal)
English
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Wing Pitching Moment Coefficient
Emerald Group Publishing | 1945
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