Wind-tunnel investigation of longitudinal aerodynamic characteristics of a powered four-duct-propeller VTOL model in transition /
Kenneth P. Spreemann.

Description

Main Author

Spreemann, Kenneth P.

Related Names

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

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration : 1966.

Subjects

Rocket engines > Rocket engines / Thrust.
Wind tunnels.
Space shuttles > Space shuttles / Longitudinal stability.
Vertically rising aircraft > Vertically rising aircraft / Aerodynamics.

Physical Description

125 p. : ill. ; 27 cm.

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