Abstract
The blunt notch strength of FMLs is discussed with respect to the deformation and failure phenomena of the individual constituents. The influence of metal plasticity, the splitting and delamination phenomena in the composite layers, and fibre failure are discussed. Various failure criteria and theories are presented to describe the blunt notch strength in the major material axes and under off-axis angles with respect to these axes.
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References
Bosker OJ (1998) Blunt notch strength of aluminium 2024-T3, report B2v-98-33. Delft University of Technology, Delft
BrĂ¼gemann V (2003) Test procedures for fibre metal laminates, report TD-R-03-005. Fibre Metal Laminates Centre of Competence, Delft, The Netherlands
ASTM Standard D5766/D5766M, Standard test method for open-hole tensile strength of polymer matrix composite Laminates1. ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
Beumler T (2004) Flying GLARE®, A contribution to aircraft certification issues on strength properties in non-damaged and fatigue damaged GLARE® structures. PhD dissertation, Delft University of Technology, Delft, The Netherlands
Bosker OJ (1998) Uni-axial blunt notch strength of GLARE 3 and GLARE 4, report B2v-98-28. Delft University of Technology, Delft
Bosker OJ (1998) Overview of existing literature on the blunt notch strength of GLARE, report B2v-98-35. Delft University of Technology, Delft
Ypma M (2000) Overview of tests concerning the influence of temperature and environmental exposure on GLARE, report B2v-00-41. Delft University of Technology, Delft
Hooijmeijjer PA (2000) Blunt notch strength of GLARE at elevated test temperatures, report B2v-00-68. Delft University of Technology, Delft
Mortier W, Pellenkoft FJ (2001) Blunt notch strength of open hole versus filled hole, report B2v-01-04. Delft University of Technology, Delft
Pellenkoft FJ, Mortier WJ (2001) Influence hole diameter on blunt notch strength, report B2v-01-05. Delft University of Technology, Delft
Hooijmeijjer PA (2001) Experimental project to assess the failure mechanisms during blunt notch of GLARE under 45°, report B2v-01-33. Delft University of Technology, Delft
Borgonje B (2009) GLARE outdoor exposure program: blunt notch strength—final issue, report B2v-02-40. Delft University of Technology, Delft
Hooijmeijer PA (1998) Blunt notch strength of spliced GLARE, inside doubler, preliminary thesis. Delft University of Technology, Delft
Mattousch A (1993) Open hole properties of some GLARE grades, report TD-R-93-014. Structural Laminates Company
van Rijn JCFN (1995) Blunt notch behaviour of GLARE3, NLR CR 95237 L. National Aerospace Laboratory NLR
Bosker OJ (1998) Finite element calculations to predict the uni-axial on-axis and off-axis blunt notch strength of GLARE and comparison with test results, report B2v-98-34. Delft University of Technology, Delft
Hagenbeek M (2000) Investigation into applicability of analytical methods for blunt notch strength prediction of FML’s, report B2v-00-57. Delft University of Technology, Delft
Bosker OJ (2000) Progress on the development of a GLARE blunt notch strength prediction tool, report B2v-00-66. Delft University of Technology, Delft
Bosker OJ (1998) Development of a GLARE blunt notch strength prediction tool for the Airbus A3XX. MSc thesis, Delft University of Technology, Delft
Vermeeren CAJR (1995) The residual strength of fibre metal laminates. PhD dissertation, Delft University of Technology, Delft
van Rijn JCFN (1994) Stress distribution around a circular hole in a fibre metal laminate finite width plate specimen, NLR TP 94058 L. National Aerospace Laboratory NLR
van Rijn JCFN (1994) Preliminary model for the blunt notch behaviour of fibre metal laminates, NLR TP 94532 L. National Aerospace Laboratory NLR
Peterson RE (1953) Stress concentration design factors. Wiley, New York
Hagenbeek M (2001) Investigation of the finite width and notch size effect for the analytical blunt notch strength prediction method, report B2v-01-20. Delft University of Technology, Delft
Vermeeren CAJR (1990) The blunt notch behaviour of metal laminates: ARALL and GLARE, report LR-617. Delft University of Technology, Delft, The Netherlands
Lekhnitskii SG (1968) Anisotropic plates (Translated from the Second Russian Edition by S.W. Tsai and T. Cheron). Gordon and Breach Science Publishers, Inc., New York
Tan SC (1987) Laminated composites containing an elliptical opening. I. Approximate stress analyses and fracture models. J Compos Mater 21:925–948
Bosker OJ, de Kraker L (1998) Determination of optimum blunt notch specimen geometry, report B2v-98-37. Delft University of Technology, Delft
Mattousch A (1993) Test procedures for fiber metal laminates, report TD-R-93-003. Structural Laminates Company, Delft, The Netherlands
Wu G, Tan Y, Yang J-M (2007) Evaluation of residual strength of notched fiber metal laminates. Mater Sci Eng A 457:338–349
Yeh P-C, Chang P-U, Yang J-M, Wu PH, Liu MC (2011) Blunt notch strength of hybrid boron/glass/aluminum fiber metal laminates. Mater Sci Eng A 528:2164–2173
Meziere Y (2000) Experimental project to assess the failure mechanisms during blunt notch of GLARE, report B2v-00-47. Delft University of Technology, Delft
Rensma E (2007) Investigation of innovative concepts for hybrid structures. MSc thesis, Delft University of Technology, Delft
Rooijen RGJ (2006) Bearing strength characteristics of standard and steel reinforced GLARE. PhD dissertation, Delft University of Technology, Delft
Sun CT, Quinn BJ, Tao J, Oplinger DW (1996) Comparative evaluation of failure analysis methods for composite laminates, report DOT/FAA/AR-95/109. Department of Transportation, Federal Aviation Administration, Washington D.C
Bosker OJ (2000) GLARE uni-axial blunt notch test results, report B2v-99-27. Delft University of Technology, Delft
Bosker OJ (2001) Blunt notch strength. In: Vlot A, Gunnink JW (eds) Fibre metal laminates—an introduction. Kluwer Academic Publishers, Dordrecht, The Netherlands
Whitney JM, Nuismer RJ (1974) Stress fracture criteria for laminated composites containing stress concentrations. J Compos Mater 8:253–265
Nuismer RJ, Whitney JM (1975) Uniaxial failure of composite laminates containing stress concentrations. Fract Mech Compos ASTM-STP 593:117–142
Konish HJ, Whitney JM (1975) Approximate stresses in an orthotropic plate containing a circular hole. J Compos Mater 9:157–166
Karlak RF (1977) Hole effects in a related series of symmetrical laminates. In: Ornie JA, Crossman FW (eds) Failure modes in composites IV. The Metallurgical Society of AIME, Warundale, PA, pp 105–117
Pipes RB, Wetherhold RC, Gillespie JW (1979) Notched strength of composite materials. J Compos Mater 13:148–179
Pipes RB, Gillespie JW, Wetherhold RC (1979) Superposition of notched strength of composite laminates. Polym Eng Sci 19:1151–1155
van Rijn JCFN (1992) The use of composite fracture models to describe the blunt notch behaviour of metal laminates. NLR TP 92061 U, National Aerospace Laboratory NLR
MĂ¼ller RPG (1995) An experimental and analytical investigation on the fatigue behaviour of fuselage riveted lap joints, the significance of the rivet squeeze force, and a comparison of 2024-T3 and GLARE 3. PhD dissertation, Delft University of Technology, Delft
Hooijmeijjer PA (2002) GLARE 2 under small off-axis angles, report B2v-02-01. Delft University of Technology, Delft
Borgonje B (2001) Blunt notch strength testing under shear loading, report B2v-01-12. Delft University of Technology, Delft
Bosker OJ (2000) GLARE bi-axial blunt notch test results, report B2v-00-30. Delft University of Technology, Delft
Herakovich CT, Aboudi J, Lee SW, Strauss EA (1988) Damage in composite laminates: effects of transverse cracks. Mech Mater 7(2):91–107
Bosker OJ (2001) Tsai-Hill failure criterion to predict the bi-axial blunt notch strength of GLARE, report TD-R-00-014. Structural Laminates Industries
BrĂ¼gemann VP (2002) Validation of the load introduction for bi-axial blunt notch tests, report B2v-02-37. Delft University of Technology, Delft
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Alderliesten, R. (2017). Blunt Notch Strength. In: Fatigue and Fracture of Fibre Metal Laminates. Solid Mechanics and Its Applications, vol 236. Springer, Cham. https://doi.org/10.1007/978-3-319-56227-8_5
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DOI: https://doi.org/10.1007/978-3-319-56227-8_5
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