Calculation of the dynamic longitudinal stability of a tilt-wing V/STOL aircraft and correlation with model flight tests /
by Joseph R. Chambers and Sue B. Grafton.

Description

Main Author

Chambers, Joseph R.

Related Names

Grafton, Sue B.
Langley Research Center.
United States. National Aeronautics and Space Administration.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration, 1968.

Subjects

Flight testing.
Airplanes > Airplanes / Wings.
Stability of airplanes, Longitudinal.
Vertically rising aircraft.

Note

Work performed at Langley Research Center.
N68-15941.

Physical Description

61 p. : ill. ; 27 cm.

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