Once the satellite structure, shrunk through this method, is connected with the rocket model, coupled loads computation can then be conducted.
用这种方法减缩之后的卫星结构和火箭模型结合后,可以进行载荷耦合计算工作。
Once the satellite structure, shrunk through this method, is connected with the rocket model, coupled loads computation can then be conducted.
用这种方法减缩之后的卫星结构和火箭模型结合后,可以进行载荷耦合计算工作。
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