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Derivation of a tapered p-version beam finite element/

Main Author:	Hinnant, Howard E.
Corporate Authors:	United States National Aeronautics and Space Administration Scientific and Technical Information Division, United States. National Aeronautics and Space Administration. Scientific and Technical Information Division, Langley Research Center
Format:	Book
Language:	English
Published:	Washington: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989
Series:	NASA technical paper AVSCOM technical report 2931
Subjects:	Girders > Vibration > Mathematical models Helicopters > Vibration > Mathematical models Airframes > Vibration > Mathematical models Vibration (Aeronautics) > Mathematical models Structural analysis (Engineering) Finite element method

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