文件名称:simulation
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利用弹簧近似和网格重构相结合的非结构动网格技术,耦合求解 Euler方程及弹道方程,模拟飞行在 46千
米高空、0°攻角、马赫数6.5、壳片分离初速分别为 6mPs ,12mPs、壳片分离角速度分别为 0°/s ,50°/s ,150°/s的子母弹
抛壳动态过程。-The use of spring approximation and mesh reconstruction of a combination of non-structural dynamic grid technology, coupled equations for solving Euler equations and ballistics, flight simulation at 46 km altitude, 0 ° angle of attack, Mach 6.5, the shell-chip separation velocity, respectively 6mPs , 12mPs, angular separation of the shell pieces were 0 °/s, 50 °/s, 150 °/s of the cluster bombs thrown shell dynamic process.
米高空、0°攻角、马赫数6.5、壳片分离初速分别为 6mPs ,12mPs、壳片分离角速度分别为 0°/s ,50°/s ,150°/s的子母弹
抛壳动态过程。-The use of spring approximation and mesh reconstruction of a combination of non-structural dynamic grid technology, coupled equations for solving Euler equations and ballistics, flight simulation at 46 km altitude, 0 ° angle of attack, Mach 6.5, the shell-chip separation velocity, respectively 6mPs , 12mPs, angular separation of the shell pieces were 0 °/s, 50 °/s, 150 °/s of the cluster bombs thrown shell dynamic process.
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子母弹抛壳过程非定常流动的数值模拟.pdf