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NASA NASA-TN-D-3437

NASA NASA-TN-D-3437 1966-JUN-01 nvestgaton of a semspan tlt-wng VTOL MODEL to determne ground effect on full-span flaps used for yaw control n hoverng

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Hovering force-test on semispan tilt-wing VTOL MODEL to determine ground effect on full-span flaps used for yaw control

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