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- H.T. Hahn
- Nonmetallic Materials Division Air Force Materials Laboratory Wright Patterson Air Force Base, Ohio 45433
抄録
<jats:p> This paper extends the nonlinear behavior of unidirectional laminae of Reference [1] to that of laminated composites. A comparison between the theory and experimental results is shown through the analysis of uniaxial tension behavior of various laminates. The effect on buckling stress owing to nonlinearity is illustrated for a ±45° angle-ply laminate with simply- supported edges. </jats:p>
収録刊行物
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- Journal of Composite Materials
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Journal of Composite Materials 7 (2), 257-271, 1973-02
SAGE Publications
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詳細情報
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- CRID
- 1364233268514557440
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- NII論文ID
- 30026521578
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- ISSN
- 1530793X
- 00219983
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- データソース種別
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- Crossref
- CiNii Articles