Failure Assessment and Reliability Analysis of CFRP Composite Pressure Vessel

Article Preview

Abstract:

A new approach for progressive failure and reliability analysis of carbon fiber reinforced polymeric (CFRP) composite pressure vessel with many base random variables is developed in the paper. The elastic constants of CFRP lamina and geometric parameters of the vessel are selected as the base design variables. CFRP lamina specimen and pressure vessel were manufactured and tested in order to obtain statistics of design variables. The limit state function for progressive failure analysis was set up. Then the progressive failure and reliability analysis of the vessel were performed according to the stiffness degradation model based on Monte Carlo simulation procedure using MATLAB. The distributions of failure loads and the probability of failure of the vessel were obtained. The feasibility and accuracy of the proposed method is validated by good agreement between the simulation and experimental results. Further analysis indicates that the lamina tensile strength in the fiber direction and hoop layer thickness of the vessel have significant influence on the probability of failure of composite pressure vessel.

You might also be interested in these eBooks

Info:

Periodical:

Key Engineering Materials (Volumes 348-349)

Pages:

225-228

Citation:

Online since:

September 2007

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2007 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] R.L. King: The Determination of Design Allowable Properties for Advanced Composite Materials, GEC J Res, Vol. 5(2) (1987), pp.76-87.

Google Scholar

[2] K. Munjal: Use of Fiber Reinforced Composites in Rocket Motor Industry, SAMPE Q, Vol. 1 (1986), pp.1-11.

Google Scholar

[3] M. Miki, Y. Murotsu, T. Tanaka, et al: Reliability of Unidirectional Fibrous Composites, AIAA Journal, Vol. 28(11) (1990), p.1980-(1986).

DOI: 10.2514/3.10508

Google Scholar

[4] P.L. Hall, J.E. Strutt: Probabilistic Physics-of-failure Models for Component Reliabilities using Monte Carlo Simulation and Weibull Analysis: A Parametric Study, Reliab Eng Syst Saf, Vol. 80 (2003), pp.233-242.

DOI: 10.1016/s0951-8320(03)00032-2

Google Scholar

[5] H.K. Jeong, R.A. Shenoi: Probabilistic Strength Analysis of Rectangular FRP Plates using Monte Carlo Simulation, Comput Struct, Vol. 76 (2000), pp.219-235.

DOI: 10.1016/s0045-7949(99)00171-6

Google Scholar

[6] D.M. Frangopol, S. Recek: Reliability of Fiber-reinforced Composite Laminate Plates, Probabilist Eng Mech, Vol. 18 (2003), pp.119-137.

DOI: 10.1016/s0266-8920(02)00054-1

Google Scholar

[7] C.C. Chamis: Probabilistic Simulation of Multi-scale Composite Behavior, Theor Appl Fract Mech, Vol. 41 (2004), pp.51-61.

Google Scholar

[8] W.F. Wu, H.C. Cheng and C.K. Kang: Random Field Formulation of Composite Laminates, Compos Struct, Vol. 49 (2000), pp.87-93.

Google Scholar

[9] F. Yan, D.H. Dai and Z.C. Zhu: Finite Element Analysis Technology of Filament Wound Pressure Vessel Structures, Aerospace, Shanghai, Vol. 6 (2003), pp.33-36.

Google Scholar

[10] S.C. Lin: Reliability Predictions of Laminated Composite Plates with Random System Parameters, Probabilist Eng Mech, Vol. 15 (2000), pp.327-338.

DOI: 10.1016/s0266-8920(99)00034-x

Google Scholar

[11] F.K. Chang, K.Y. Chang: A Progressive Damage Model for Laminated Composites Containing Stress Concentrations, J. Comp. Mater., Vol. 21 (1987), pp.834-855.

DOI: 10.1177/002199838702100904

Google Scholar