Virtual Prototype Based Fatigue Life Research on some Missile Erecting System

Chang Lin Hu; Li Yuan Ma; Hui Li; Yong Jun Li

doi:10.4028/www.scientific.net/AMR.706-708.1676

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 706-708Virtual Prototype Based Fatigue Life Research on...

Virtual Prototype Based Fatigue Life Research on some Missile Erecting System

Abstract:

With some ballistic missile erecting system as subject, a virtual prototype is constructed, for virtual measuring of the load spectrum of the erecting system. By FEM analysis and damage analysis, the dangerous position of is uncovered, and the stress-time history is obtained. By use of material fatigue feature curve in combination with the stress-time history, the fatigue life of system components is studied.

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Periodical:

Advanced Materials Research (Volumes 706-708)

Pages:

1676-1679

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.706-708.1676

Citation:

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Online since:

June 2013

Authors:

Chang Lin Hu, Li Yuan Ma, Hui Li, Yong Jun Li

Keywords:

Erecting, Fatigue Life, Launch Device, Virtual Prototype

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References

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