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FORMULATING THE CUTTING OF ONE-DIMENSIONAL STRUCTURE UNDER IMPACT LOAD

机译:在冲击载荷下配制一维结构的切割

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Under impact loading in middle position, the cutting problem of one-dimensional plane structure (with two fixed edges) is studied in this research. The impact loading is supplied by a flying plane with narrow cut-in edge. After the front cut-in edge goes through the structure, the impact loading is maintained by the friction between the flying plane and the fracture face of structure for a short time. Then the plane is rested in the structure fracturing zone or passes though the structure. In practical problems,it is required to determine the deformation and fracture of structure by the velocity-mass parameter and the geometry of impact load. In this research, the deformation of structure is characterized by the deflection angular in the fracture position. The deformation stress is balanced by the acceleration force of flying plane through the friction coupling. The related impact-fracture equations are formulated in this research. The final equation shows the deflection angular of the structure is completely determined by the mechanical parameters of structure, the mass of flying plane, the friction parameter between the flying plane and the fracturing face of the structure, and the initial velocity of impact. When the friction parameter is taken as one, the equation can be used to evaluate the risk of fracturing for given initial velocity and mass. Generally, the obtained equation is non-linear. For simple case, analytical results are obtained to explain the cutting phenomenon.
机译:在中间位置的冲击载荷下,在该研究中研究了一维平面结构的切割问题(具有两个固定边缘)。冲击载荷由飞行器提供,飞行器具有窄切割边缘。在前切割边缘通过该结构之后,通过飞行平面与结构的裂缝面之间的摩擦保持冲击载荷。然后将平面搁置在结构压裂区中或通过结构通过。在实际问题中,需要通过速度 - 质量参数和冲击载荷的几何形状来确定结构的变形和断裂。在该研究中,结构的变形特征在于裂缝位置中的偏转角度。通过摩擦耦合飞行平面的加速力平衡变形应力。在本研究中配制了相关的冲击骨折方程。最终的等式示出了结构的偏转角度完全由结构的机械参数,飞行平面的质量,飞平面之间的摩擦参数和结构的压裂面,以及初始速度的冲击。当摩擦参数作为一个时,可以使用等式来评估给定初始速度和质量压裂的风险。通常,所获得的等式是非线性的。对于简单的情况,获得分析结果以解释切割现象。

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