Structural Behavior of Burned Composites
{"Image DocumentName": "Structural Behavior of Burned Composites", "Image ImageDescription": "The laminate was found to fail quickly under any stress above 10% of the nominal buckling stress for all of the heat flux cases. The 10 kW/m2 case only heated the laminate above the epoxy\u2019s viscous softening temperature (50-100\u00b0C), but not above the matrix decomposition temperature. The 25 kW/m2 case heated the laminate above both the epoxy viscous softening temperature and the matrix decomposition temperature ( \u00b0C), but not above the fiber oxidation temperature. The 50 kW/m2 case heated the laminate enough that it reached the viscous softening temperature, the matrix decomposition temperature and the fiber oxidation temperature (>500\u00b0C). [5]", "Image XResolution": "37", "Image YResolution": "37", "Image ResolutionUnit": "Pixels/Centimeter", "Image Software": "SlidePlayer", "Image YCbCrPositioning": "Centered"}