Transition characteristics of a VTOL aircraft powered by four ducted tandem propellers /
Edwin E. Davenport and Kenneth P. Spreemann.

Description

Main Author

Davenport, Edwin E.

Related Names

Spreemann, Kenneth P.
Langley Research Center.
United States. National Aeronautics and Space Administration.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration : 1964.

Subjects

Vertically rising aircraft > Vertically rising aircraft / Testing.
Ducted fans.

Physical Description

55 p. : ill. ; 27 cm.

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