Liquid propellant analogy technique in dynamic modeling of launch vehicle

Author:

Pan ZhongWen,Xing YuFeng,Zhu LiWen,Dong Kai,Sun Mu

Publisher

Springer Science and Business Media LLC

Subject

General Engineering,General Materials Science

Reference12 articles.

1. Wang Y, Zhu L W. Summary of some key technologies on dynamics of large launch vehicle. Missil Space Vehicl, 2000, 1: 29–37

2. Wang L S, Zhang D W. Several problems in structural finite element analysis of launch vehicles. Struct & Environ Eng, 1988, 3: 45–53

3. Xia Y L, Yu W L. Experimental investigation for dynamic characteristics of liquid sloshing in an ellipsoidal tank. J Astron, 1991, 4: 70–76

4. Yang M, Li J F. Determination of damping ratio of the small-amplitude liquid sloshing within the cylindrical container with a ring baffle. Chin J Theor Appl Mech, 2006, 5: 660–667

5. Zhou H, Li J F, Wang T S. Mesh update algorithm in ALE finite method within free surface flow. Chin J Theor Appl Mech, 2006, 3: 660–667

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