Derivation of a tapered p-version beam finite element /
Howard E. Hinnant.

Description

Main Author

Hinnant, Howard E.

Related Names

Langley Research Center. Aerostructures Directorate.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; 1989.

Subjects

Finite element method.
Structural analysis (Engineering)
Vibration (Aeronautics) > Vibration (Aeronautics) / Mathematical models.
Airframes > Airframes / Vibration > Airframes / Vibration / Mathematical models.
Helicopters > Helicopters / Vibration > Helicopters / Vibration / Mathematical models.
Girders > Girders / Vibration > Girders / Vibration / Mathematical models.

Note

Research done at Langley Research Center, USAARTA-AVSCOM, Aerostructures Directorate.

Physical Description

42 p. : ill. ; 28 cm.

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