Numerical Analysis of Multiscale Progressive Damage for Solid Rocket Motor Composite Shell

Jiu Ling Zhao; Bo Gao; Xue Ren Wang; Bao Shun Zhou

doi:10.4028/www.scientific.net/AMM.574.219

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Design and Performance Analysis of Compressor in Solid Propellant Air Turbo Rocket (SPATR)
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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 574Numerical Analysis of Multiscale Progressive...

Numerical Analysis of Multiscale Progressive Damage for Solid Rocket Motor Composite Shell

Abstract:

In this study, the evolution of laminates in four damages are analyzed based on the established multiscale reinforced composite material damage model from a single cell model, single plate model to multilayer fiber model of carbon fiber. The validity of the model is verified by numerical simulation of laminate tensile test. Based on the established model to calculate the [±26/90₂]₃ damage evolution of SRM due to withstand pressure in the straight section and the results show that: the calculation is consistent with the experimental results of displacement, and the role of a variety of common damages result in reduced performance of the housing.

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Periodical:

Applied Mechanics and Materials (Volume 574)

Pages:

219-223

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.574.219

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Online since:

July 2014

Authors:

Jiu Ling Zhao*, Bo Gao, Xue Ren Wang, Bao Shun Zhou

Keywords:

Composite Shell, Multiscale Progressive Damage, Numerical Analysis, Solid Rocket Motor (SRM)

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* - Corresponding Author

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