Treatment of problem of wing of finite span has been on basis of 2-dimensional theory, corrected for effect of wake; problem of 3-dimensional flow considered; correction formulas given.
Theoretical correction for lift of elliptic wings
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 9 , n 1
1941
3 pages
Aufsatz (Zeitschrift)
Englisch
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