Method is developed for determining twist of swept-back wing with prescribed spanwise lift distribution; explicit formulas are derived for case that lift is given at eight points of semi-span. (see also - n 8 (discussion) Oct p 320-1)
Influence of sweep on spanwise lift distribution of wings
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 10 , n 3
1943
4 pages
Article (Journal)
English
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