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在高g基础上,对低g环境下的液体晃动问题作了理论分析与实验研究。应用在火箭工程中作线性分析时,获得了低g液体晃动问题的分析方法与解决此问题的实验手段。
On the basis of high g, theoretical analysis and experimental research on liquid sloshing in low g environment are carried out. When used in rocket engineering for linear analysis, the analytical method of low g liquid sloshing problem and the experimental method to solve this problem are obtained.