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A Method For Solving Parameters At The End Of A Complete Flutter Of Two Colliding Objects With Non-Fixed Constraints
A Method For Solving Parameters At The End Of A Complete Flutter Of Two Colliding Objects With Non-Fixed Constraints
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机译:具有非固定约束的两个碰撞对象完全颤动结束时的参数求解方法
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#$%^&*AU2020100577A420200528.pdf#####Abstract The invention proposes a method for solving parameters at the end of a complete flutter of two colliding objects with non-fixed constraints, which comprises the following steps: obtaining model input parameters at the time to of flutter, wherein the model input parameters include the mass ratio of the two colliding objects, the position coordinates, velocity, acceleration and coefficient of restitution of each colliding object, and the said mass ratio and coefficient of restitution are both constant; establishing a first solution model to obtain the end time too of the flutter; establishing a second solution model to obtain the position parameters of the two colliding objects at the end time too of the flutter; establishing a third solution model to obtain the velocity parameters of the two colliding objects at the end time too of the flutter. The invention continues the numerical simulation directly from a certain flutter time, which can skip the flutter process, and directly obtain the time when the flutter ends and the positions and velocities of the two colliding objects at that time, thereby increasing the calculation accuracy and reducing the calculation time.Descriptions with Drawings Obtain model input parameters at the time of flutter Establish a first solution model to obtain the end time the flutter |Establish a second solution model to obtain the S position parameters of the two colliding objects S3 at the end time of the flutter Establish a third solution model to obtain the velocity parameters of the two colliding objects at the end time S4 of the flutter Fig.1 1 2 Fe(sinD1) Fig.2
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