Abstract
In this paper, a procedure for optimizing the fiber orientations near a hole in a single layer of multilayer composite laminates for increased strength is presented. A symmetric six-layer [(C-0)/+45/-45]s laminate with central hole is considered. Within the ±45° layers, the fiber orientations are fixed. The C-0 layer is divided into two fields: a small near field around the hole and a relatively large far field away from the hole. In the far field, the fiber orientations are fixed at 0°, and in the near field, the fiber orientations are assumed to have continuous distribution represented by piecewise bilinear interpolation functions. The Tsai–Wu-criterion-based failure load magnitudes of [(C-0)/+45/-45]s and [C-0]6 designs are maximized by iteratively alternating between a gradient-based search and a genetic algorithm. The results show that the load-carrying capacity of composite laminates with hole can be greatly increased through the optimization of continuous fiber orientation distribution within a small area around the hole in the C-0 layer, and the optimum fiber orientation distribution pattern in the C-0 layer is similar to that of the corresponding principal stress orientation distribution. The [(C-0)/+45/-45]s design is only a few percent weaker than the [C-0]6 design, which is important for carrying off-design loadings.
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References
7 Gunderson SL, Lute JA (1993) The use of preformed holes for increased strength and damage tolerance of advanced composites. J Reinf Plast Comp 12:(5)559–569
8 Huang J, Haftka RT, Rapoff RJ (2003) Optimization design of composite plates with holes for increased strength. In: Proceed-ings of the 44th AIAA/ASME/ASCE/AHS/ASC conference on structures, structural dynamics, and materials, Norfolk, VA
12 Huang J, Venkataraman S, Rapoff RJ, Haftka RT (2003) Optimization of axisymmetric elastic modulus distributions around a hole for increased strength. J Struct Multidisc Optim 25(4):225–236
3 Hyer MW, Charette RF (1991) Use of curvilinear fiber format in composite structure design. AIAA J 29(6):1011–1015
4 Hyer MW, Lee HH (1991) The use of curvilinear fiber format to improve buckling resistance of composite plates with central circular holes. Comp Struct 18:239–261
1 Jegley DC, Tatting BF, Gürdal Z (2003) Optimization of elastically tailored tow-placed plates with holes. In: Proceedings of the 44th AIAA/ASME/ASCE/AHS/ASC conference on structures, structural dynamics, and materials, Norfolk, VA
2 Katz Y, Haftka RT, Altus E (1989) Optimization of fiber directions for increasing the failure load of a plate with a hole. In: Proceedings of the ASC 4th technical conference on composite materials, Blacksburg, VA, 3–5 October 1989
5 Nagendra S, Kodiyalam S, Davis JE (1995) Optimization of tow fiber paths for composite design. In: Proceedings of the 36th AIAA/ASME/ASCE/AHS/ASC conference on structures, structural dynamics, and materials and AIAA/ASME forum on adaptive structures, New Orleans, LA
6 Parnas L, Oral S, Ceyhan Ü (2003) Optimum design of composite structures with curved fiber courses. J Comp Sci Tech 63:1071–1082
10 Vanderplaats, Miura & Associates (1993) DOT user’s manual, Colorado Springs, CO
11 Wall M (2003) GAlib: A C++ library of genetic algorithm components, version 2.4.5. Freeware available at http://lancet.mit.edu/ga/[accessed 8 May 2003]
9 Yau SS, Chou TW (1988) Strength of woven-fabric composites with drilled and molded holes. Composite Materials Testing and Design, ASTM STP972, American Society for Testing and Materials, Philadelphia, pp 423–437
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Huang, J., Haftka, R. Optimization of fiber orientations near a hole for increased load-carrying capacity of composite laminates. Struct Multidisc Optim 30, 335–341 (2005). https://doi.org/10.1007/s00158-005-0519-z
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DOI: https://doi.org/10.1007/s00158-005-0519-z