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Flugmechanik
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Women in Flight Research at NASA Dryden Flight Research Center from 1946 to 1995, Number 6
Wing X-7A (Tv-14) - Determination of Deformation Due to Flight Loads
Wing Surface Pressure Data from Large-Scale Wind-Tunnel Tests of a Propeller-Driven STOL Model
Wings of the Nation. Volume 19, Number 12, 1968 (Selected Articles)
Wings of the Minimum Induced Drag: Spanload Implications for Aircraft and Birds
Wing Rock Prediction Method for a High Performance Fighter Aircraft
Wing pressure distributions from subsonic tests of a high-wing transport model
Wing Pressure Distributions from Subsonic Tests of a High-Wing Transport Model
Wing pressure-distribution measurements up to 0,866 Mach number in flight on jet-propelled airplane