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AN EXPERIMENTAL AND NUMERICAL STUDY OF BALLISTICIMPACTS ON A TURBINE CASING MATERIAL ATVARYING TfMEIERATURES

机译:涡轮机壳体材料呈TFMeieratures的涡轮机壳体材料的实验和数值研究

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An experimental and numerical study of ballistic impacts on steel plates at various temperatures (700°C, 400°C and room temperature) has been carried out. The motivation for this work is the blade-off event that may occur inside a jet engine turbine. The material used in this study is the FV535 martensitic stainless steel, which is one of the most commonly used materials for turbine casings. Based on material test data, a Modified Johnson-Cook model was calibrated for numerical simulations using the LS-DYNA explicit finite element code. To check the mesh size sensitivity, 2D axisymmetric finite element models with three different mesh sizes and configurations were used for the various temperatures. Both the formation of adiabatic shear bands in the perforation process and the modeling of the thermal softening effects at high temperatures have been found crucial in order to achieve good results.
机译:已经进行了各种温度(700℃,400℃和室温)在钢板上的弹道冲击的实验和数值研究。这项工作的动机是在喷气机涡轮机内可能发生的叶片截止事件。本研究中使用的材料是FV535马氏体不锈钢,这是涡轮机壳体最常用的材料之一。基于材料测试数据,使用LS-DYNA显式有限元代码校准修改的Johnson-Cook模型。为了检查网格尺寸灵敏度,使用具有三种不同网格尺寸和配置的2D轴对称有限元模型,用于各种温度。为了达到良好的效果,发现穿孔过程中的绝热剪切带的形成和高温下的热软化效果的建模。

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