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Shear yield strength

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Fibre Metal Laminates

Abstract

Shear loads in an aircraft fuselage will occur as a result of bending and torsion. Yield values under shear are necessary during the design phase since the material should not deform plastically below the limit load. The Metal Volume Fraction (MVF) method for shear yield strength prediction of Glare laminates was investigated. The maximum deviation of the Iosipescu shear test data from the prediction line is 6.5%. The results indicate a good applicability of the MVF method.

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References

  1. H.F. Wu, W.J. Slagter and J.L. Verolme, A pilot study of metal fraction approach for fiber metal laminates, Product Design and Mechanical Division, Alcoa Technical Center, U.S.A., Faculty of Aerospace Engineering, Delft University of Technology, The Netherlands, ATC Report No. 57-92-17, SLC Report No. SL-020-B, December 1992.

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  2. A.C. Mattousch, Shear properties of Glare 3–3/2–0.2 and Glare 3–3/2–0.3, SLI report TD-R-95-001, 7 March 1995.

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  3. P.K. Kuijpers, The influence of material changes on the shear strength of Glare 3 laminates, report B2v-98-30, Delft University of Technology, November 1998.

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  4. P.L. Kuijpers, Results of shear tests, report B2v-99-36, Delft University of Technology, October 1999.

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  5. M. Hagenbeek, The MVF method for shear yield strength prediction, report B2v-99-26, Delft University of Technology, October 1999.

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© 2001 Springer Science+Business Media Dordrecht

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Hagenbeek, M. (2001). Shear yield strength. In: Vlot, A., Gunnink, J.W. (eds) Fibre Metal Laminates. Springer, Dordrecht. https://doi.org/10.1007/978-94-010-0995-9_8

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  • DOI: https://doi.org/10.1007/978-94-010-0995-9_8

  • Publisher Name: Springer, Dordrecht

  • Print ISBN: 978-1-4020-0391-2

  • Online ISBN: 978-94-010-0995-9

  • eBook Packages: Springer Book Archive

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