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

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Author

Ronald Krueger

Contributions

Minguet, Pierre J. - Contributor
O'Brien, T. Kevin. - Contributor
Langley Research Center. - Contributor

Publication

1999 - National Aeronautics and Space Administration, Langley Research Center, Hampton, Va, Virginia

Language

English

Word Count

0 words, Guess

Page Count

0 pages

Physical Format

Microform

Identifiers

OCLC Control Number43302028
Open LibraryOL17592108M

Subjects

Topics

Strain ratePlane strainCrack closureLoads (Forces)Fracture mechanics Composite materials Debonding (Materials)

Series Statement

NASA/TM -- 1999-209365.
NASA technical memorandum -- 209365.

Other Editions

A method for calculating strain energy release rates in preliminary design of composite skin/stringer debonding under multi-axial loadingMicroformNational Aeronautics and Space Administration, Langley Research Center1999

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