Investigation of a semispan tilt-wing VTOL model to determine ground effect on full-span flaps used for yaw control in hovering /
Kalman J. Grunwald.

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Main Author
Grunwald, Kalman J.
Related Names
Langley Research Center.
United States. National Aeronautics and Space Administration.
Language(s)
English
Published
Washington, D.C. : National Aeronautics and Space Administration ; 1966.
Subjects
Ground-effect machines.
Flaps (Airplanes)
Yawing (Aeronautics)
Ailerons.
Physical Description
73 p. : ill. ; 27 cm.
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Limited (search only)   v.3437 University of Illinois at Urbana-Champaign