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Original article aerodynamic performance of a... For forward flight the asymmetric stroke does not increase the lifting efficiency and propulsive efficiency of the wing simultaneously....
général - core.ac.uk - PDF: pig.sagepub.com
Full scale hover test of a 25 foot tilt rotor... Measured lifting efficiency was 8.35...
Semiempirical method for predicting vortex-induced rolling moments... Two empirical corrections are included to account for the lifting efficiency of an airfoil section and the local stall on the wing....
Airfoil shape for flight at subsonic speeds... A highly cambered trailing edge section improves overall airfoil lifting efficiency....
In-flight lift-drag characteristics for a forward-swept wing aircraft... The lifting efficiency of the X-29A, as defined by the Oswald lifting efficiency fac-tor, e, is about average for a cantilevered monoplane for M = 0.6...


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