Description of method developed to estimate percentage of lift carried by airfoil-section fuselage; acceptance by NACA of lift distribution of 25% for airfoil-section fuselage and 75% for wings proposed by M. WATTER in Dec 26 1935 issue, previously indexed. (Supp)
Lift slope and distribution on Burnelli aeroplanes
Flight
Flight ; 29 , n 1434 ; p 37-39 + 44
1936
Aufsatz (Zeitschrift)
Englisch
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