Aeorelastic analysis for helicopter rotor blades with time-variable, nonlinear structural twist and multiple structural redundancy-mathematical derivation and program user's manual /
Richard L. Bielawa.

Description

Main Author

Bielawa, Richard L.

Related Names

United Technologies Research Center.
United States. National Aeronautics and Space Administration.
Langley Research Center.
U.S. Army Air Mobility Research and Development Laboratory.

Language(s)

English

Published

Washington : National Aeronautics and Space Administration ; 1976.

Subjects

Equations of motion.
Composite materials > Composite materials / Analysis.
Aeroelasticity > Aeroelasticity / Mathematical models.
Rotors (Helicopters) > Rotors (Helicopters) / Aerodynamics.

Note

Prepared under Contract no. NAS. 1-10960 by United Technologies Research Center, East Hartford, Conn. for Langley Research Center and U.S. Army Air Mobility R & D Laboratory.
Cover title.

Physical Description

vi, 150 p. : ill. ; 27 cm.

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