Development of an analysis for the determination of coupled helicopter rotor/control system dynamic response /
by Lawrence R. Sutton and Stephen A. Rinehart.

Description

Main Author

Sutton, Lawrence R.

Related Names

Rinehart, Stephen A.
Langley Research Center.
Rochester Applied Sciences Associates.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration ; 1975.

Subjects

Helicopters > Helicopters / Control systems > Helicopters / Control systems / Computer simulation.
Wakes (Aerodynamics) > Wakes (Aerodynamics) / Computer simulation.
Rotors (Helicopters) > Rotors (Helicopters) / Aerodynamics > Rotors (Helicopters) / Aerodynamics / Computer simulation.

Note

Pt. II by Sutton only.
"Prepared by Rochester Applied Science Associates ... for Langley Research Center."
Cover title.

Physical Description

2 v. : ill. ; 27 cm.

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