Static and dynamic longitudinal stability derivatives of a powered 0.18 scale model of a fan-in-wing VTOL aircraft /
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

Fan-in-wing aircraft.
Stability of airplanes, Longitudinal.
Vertically rising aircraft.

Note

Work performed at Langley Research Center.
N68-15894.

Physical Description

64 p. : ill. ; 27 cm.

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