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Rapid Determination of the High Cycle Fatigue Limit Curve of Carbon Fiber Epoxy Matrix Composite Laminates by Thermography Methodology: Tests and Finite Element Simulations

机译:热成像方法论快速测定碳纤维环氧基质复合层压板的高循环疲劳极限曲线:试验和有限元模拟

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Self-heating measurements under cyclic loading allow a fast estimation of fatigue properties of composite materials. The tensile fatigue behavior of a high stress carbon fiber epoxy-matrix composite laminates is examined at room temperature. Tension-tension cyclic fatigue tests are also conducted under load control at a sinusoidal frequency of 5 Hz to obtain high-cycle fatigue stress curves (S-N). The fatigue limits of the different composite lay-ups tested were successfully compared with data resulting from the self-heating test method on the same laminates. This comparison reveals a good agreement between the two methods dedicated to stress fatigue limit determination. In addition, a tomographic analysis is used to perform comparisons at the microscale between both fatigue methods. The nonlinear heat transfer laminate theory is used for self-heating tests simulation. Self-heating simulations involving conduction, convection, and boundary radiation are performed with the Finite Element code Cast3M.
机译:循环荷载下的自加热测量允许快速估计复合材料的疲劳性能。在室温下检查高应力碳纤维环氧基质复合层压材料的拉伸疲劳行为。张力张力环状疲劳试验也在载荷控制下以5Hz的正弦频率进行,以获得高循环疲劳应力曲线(S-N)。与由相同层压板上的自加热试验方法产生的数据成功进行了测试的不同复合铺层UPS的疲劳限制。这种比较揭示了两种方法之间的良好一致性,致力于应力疲劳极限确定。另外,断层分析用于在两种疲劳方法之间进行微观尺寸的比较。非线性传热层压材料理论用于自加热试验模拟。涉及传导,对流和边界辐射的自加热模拟进行了有限元码CAST3M。

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