Modal Analysis on the Simulation of the Missile Launchers Based on ABAQUS

Cong Huang; Yi Jiang; Heng Zhang

doi:10.4028/www.scientific.net/AMM.716-717.676

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 716-717Modal Analysis on the Simulation of the Missile...

Modal Analysis on the Simulation of the Missile Launchers Based on ABAQUS

Abstract:

One of the inevitable problems in the missile launchers is vibration, which can lead to failure of missile launchers. The3D model of the missile launchers is created and the modal analysis is adopted by the ABAQUS. The results show that the missile launchers will have resonance. The vibration mode diagram of the missile launcher’s structure is analyzed and the weakness of the missile launchers was found. The theory for the missile launchers design and manufacture is provided.

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Periodical:

Applied Mechanics and Materials (Volumes 716-717)

Pages:

676-678

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.716-717.676

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Online since:

December 2014

Authors:

Cong Huang*, Yi Jiang, Heng Zhang

Keywords:

ABAQUS, Missile Launchers, Modal Analysis

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* - Corresponding Author

References

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