NASA STI Repository (National Aeronautics and Space Administration) · 1984 · 65 citations · 10 references
Open access
Natural SciencesMaterials EngineeringMaterials ScienceMechanical Behavior Of MaterialsStructural AnalysisStructural EngineeringComposite MaterialsComposite Structure AnalysisFiber-reinforced CompositesStrength Of MaterialsStress AnalysisStress-strain BehaviorDelaminationDelamination GrowthDelamination MechanicsImperfection SensitivityLaminate TheoryStability Analysis Of Composite StructuresSuperposition AnalysisThermal Loads
The effect of various parameters on instability related delamination growth was studied. The configuration studied consisted of a thick composite laminate with a single through width delamination located near one surface. Both mechanical and thermal loads were considered. It is assumed that GI and GII govern delamination growth. An approximate superposition stress analysis was developed which gives closed form expressions for GI and GII. It is found that both GI and GII are very sensitive to delamination length and location through the thickness and that the magnitude of GI is also sensitive to initial imperfection. Critical loads for delamination growth are calculated based on three growth criteria. Large differences in the predictions highlight the need for a verified mixed mode delamination growth criterion.
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Buckling of Bars, Plates, and Shells
D. O. BRUSH, B. O. Almroth, John W. Hutchinson · Journal of Applied Mechanics · 1975 · 1.7K citations · Full text