A method for calculating strain energy release rates in preliminary design of composite skin/stringer debonding under multi-axial loading

A method for calculating strain energy release rates in preliminary design of composite skin/stringer debonding under multi-axial loading

Bibliographic Details
Main Author: Krueger, Ronald
Corporate Author: Langley Research Center
Other Authors: Minguet, Pierre J, O'Brien, T. Kevin
Format: Government Document Book
Language:English
Published: Hampton, Va. : [Springfield, Va. : National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service, distributor, 1999]
Series:NASA technical memorandum 209365
Subjects:
Composite materials
Crack closure
Debonding (Materials)
Fracture mechanics
Loads (Forces)
Plane strain
Strain energy release rate
Strain rate

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Stanford University

Holdings details from Stanford University
Call Number: NAS 1.15:209365

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