The effect of bridging on fatigue crack growth behavior in Aramid Patched Aluminum Alloy(APAL) |
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Authors: | S W Oh W J Park C W Hue H K Yoon K B Lee |
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Affiliation: | 1. Department of Mechanical Engineering, Dong-A University, Pusan, Korea 2. Department of Mechanical Engineering, Dong-Eui Univ., Pusan, Korea 3. Han-Kuk Fiber Glass Co. Ltd., Kyungnam, Korea
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Abstract: | A new hybrid composite (APAL: Aramid Patched Aluminum Alloy), consisting of a 2024-T3 aluminum alloy plate sandwiched between
two aramid/epoxy laminate (HK 285/RS 1222), was developed. Fatigue crack growth behavior was examined at stress ratios of
R=0.2, 0.5 using the aluminum alloy and two kinds of the APAL with different fiber orientation (0°/90° and 45° for crack direction).
The APAL showed superior fatigue crack growth resistance, which may be attributed to the crack bridging effect imposed by
the intact fibers in the crack wake. The magnitude of crack bridging was estimated quantitatively and determined by a new
technique on basis of compliances of the 2024-T3 aluminum alloy and the APAL specimens. The crack growth rates of the APAL
specimens were reduced significantly as comparison to the monolithic aluminum alloy and were not adequately correlated with
the conventional stress intensity factor range(ΔK). It was found that the crack growth rate was successfully correlated with the effective stress intensity factor range (ΔK
eff
=K
br
-K
ct
) allowing for the crack closure and the crack bridging. The relation between da/dN and theΔK
eff
was plotted within a narrow scatter band regardless of kind of stress ratio (R=0.2, 0.5) and material (2024-T3 aluminum alloy,
APAL 0°/90° and APAL±45°). The result equation was as follow:da/dN=6.45×10−7(ΔK
eff
)2.4. |
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Keywords: | Hybrid Composite Aramid/Epoxy Prepreg Fatigue Crack Growth Behavior Effective Stress Intensity Factor Range Crack Bridging Crack Closure |
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