Method of determining overall lift and induced drag of wing fuselage combination in incompressible flow; wing panel circulation distribution required for minimum induced drag is presented for various ratios of body diameter to wing span along with values of minimum induced drag. Translation from Prikladnaya Matematika i Mekhanika 1957.
On lift properties and induced drag of wing-fuselage combination
NASA -- Report
1959
8 pages
Report
English
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