REVIEWS IN STRUCTURAL DYNAMICS ANALOGY TECHNIQUE OF LAUNCH VEHICLE

PAN Zhongwen; ZENG Yaoxiang; LIAN Yongzheng; XING Yufeng

doi:10.6052/1000-0992-12-063

Volume 42 Issue 4

Jul. 2012

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PAN Zhongwen, ZENG Yaoxiang, LIAN Yongzheng, XING Yufeng. REVIEWS IN STRUCTURAL DYNAMICS ANALOGY TECHNIQUE OF LAUNCH VEHICLE[J]. Advances in Mechanics, 2012, 42(4): 406-415. doi: 10.6052/1000-0992-12-063

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PAN Zhongwen, ZENG Yaoxiang, LIAN Yongzheng, XING Yufeng. REVIEWS IN STRUCTURAL DYNAMICS ANALOGY TECHNIQUE OF LAUNCH VEHICLE[J]. Advances in Mechanics, 2012, 42(4): 406-415. doi: 10.6052/1000-0992-12-063

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REVIEWS IN STRUCTURAL DYNAMICS ANALOGY TECHNIQUE OF LAUNCH VEHICLE

doi: 10.6052/1000-0992-12-063

1 Beijing Institute of Astronautical System Engineering , Beijing 100076, China
2 The Solid Mechanics Institute, Beihang University, Beijing 100191, China

Funds: The project was supported by the Eleventh Five General Armament Department Advanced Research Project (51320103), Space-Support Project (618010604-02) and 973 National Defense Project (613133).

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Corresponding author: PAN Zhongwen
Received Date: 2012-03-20
Rev Recd Date: 2015-05-31
Publish Date: 2012-07-25

Abstract

Abstract

First in this paper, based on different kinds of launch vehicles, domestic and overseas overall modal analysis and experiments verification are respectively reviewed. Then dynamics modeling techniques are respectively summarized from three directions, such as dynamics modeling of cylindrical shell- stiffened, dynamics simulation of liquid propellant, prediction methods of local mode shape-slope. Finally, further research directions are suggested based on the development needs of structural dynamics of launch vehicles.
- overall model,
- experiments verification,
- cylindrical shell-stiffened,
- liquid propellant,
- mode shapeslope

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References(81)

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