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
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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
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