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- W2332480212 abstract "Thickness-tapered cruciform specimens have previously been used to measure the biaxial strength of various carbon/epoxy cross-ply laminates. In the present work an alternative specimen production method was investigated that requires no machining of the gage section. A total of 27 specimens were tested to produce a complete failure envelope in the σ1-σ2 stress space. Results were compared with five specimens produced by the previous manufacturing method. In addition, finite element analysis (FEA) was conducted on both these specimens and resulting strains were to within 5% of the measured experimental results. Additional geometries were machined into the specimens in the continued effort to improve the specimen geometry to promote failure within the gage section for all stress ratios. Three separate modifications were made and seven specimens of each were tested at various stress ratios. Comparisons are made between experimental and FEA results." @default.
- W2332480212 created "2016-06-24" @default.
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- W2332480212 date "2004-04-19" @default.
- W2332480212 modified "2023-09-24" @default.
- W2332480212 title "Biaxial Strength Measurements of IM7/977-2 Carbon/Epoxy Laminates Using Tabbed Cruciform Specimens" @default.
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- W2332480212 doi "https://doi.org/10.2514/6.2004-1641" @default.
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