Application is made of O. SCHRENK'S approximate method (indexed in Engineering Index 1940 p 54, from Nat Advisory Committee Aeronautics -- Tech Memo n 948 Aug 1940) to two cases, one wing without twist and other, same wing with twist.
Wing lift distribution
Aircraft Eng
Aircraft Engineering ; 16 , n 188
1944
3 pages
Article (Journal)
English
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Emerald Group Publishing | 1944
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