4.5 Article Proceedings Paper

High-Rate In-Plane Shear Testing of IM7/8552 Using the Split Hopkinson Tension Bar

期刊

AIAA JOURNAL
卷 59, 期 10, 页码 4257-4263

出版社

AMER INST AERONAUTICS ASTRONAUTICS
DOI: 10.2514/1.J060269

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  1. European-Union [CS2-AIR-GAM-2019]

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The high-rate in-plane shear properties of IM7/8552 carbon/epoxy composite material were investigated, showing an increase in in-plane shear strength with increasing loading rate. The data confirmed the in-plane shear strengths measured at different strain rates. Leveraging a Johnson-Cook-type semilogarithmic scaling law, the study provides a method to describe the evolution of in-plane shear strength with increasing loading rate.
The high-rate in-plane shear properties of IM7/8552 carbon/epoxy composite material were investigated using a split Hopkinson tension bar featuring constant impedance mountings and semiconductor strain gauges in order to maximize the quality of the load signal. The in-plane shear response up to failure was evaluated using digital image correlation and correction terms for fiber rotation. The data confirmed previously determined experimental data reporting an increase of in-plane shear strength with increasing loading rate: In-plane shear strengths of 135 and 175 MPa were measured for strain rates of 320 and 2600 s(-1), respectively. The results indicate that a Johnson-Cook-type semilogarithmic scaling law can be used to describe the evolution of in-plane shear strength with increasing loading rate.

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