Analysis of Fatigue Crack Growth Behavior in the Stiffened Panels with Bonded Symmetric Stiffener

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  • Published : 2000.05.01

Abstract

The stiffened panel is representative of a large portion of aircraft construction and therefore has much practical importance. In this paper, the influence of various shape parameters on the stress intensity factors and the fatigue crack growth in the panels with bonded composite stiffeners are studied experimentally. Results are presented as crack growth rates for various values of crack lengths, stiffness ratios, and stiffening Materials.

Keywords

References

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