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3PAN ZhongWen 1,2 ,XING YuFeng 1 ,ZHU LiWen 2 ,DONG Kai 2 &SUN Mu 2 1Solid Mechanics Research Center,Beijing University of Aeronautics and Astronautics,Beijing 100191,China,2 Beijing Astronautics Systems Engineering Institute,Beijing 100076,China.Liquid propellant analogy technique in dynamic modeling of launch vehicle[J].Science China(Technological Sciences),2010,53(8):2102-2110. 被引量：11
