Investigation of a semispan tilting-propeller configuration and effects of ratio of wing chord to propeller diameter on several small-chord tilting-wing configurations at transition speeds /
Kenneth P. Spreemann.

Description

Main Author

Spreemann, Kenneth P.

Related Names

Langley Research Center.
United States. National Aeronautics and Space Administration.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration, 1963.

Subjects

Winged aircraft.
Space vehicles.
Propellers, Aerial.
Airplanes > Airplanes / Wings.

Physical Description

31 p. : ill. ; 27 cm.

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