A general and effective approach for the optimal design of fiber reinforced composite structures
Source abstract
Abstract
This paper presents a general and effective procedure based on a mathematical programming approach for composite structures optimal design, under weight, stiffness and strength criteria. Effective means that the developed approach is able to find a local optimum in few iterations, even with a large number of design variables. In addition, as the formulation may include strength constraints, it is shown that not only plies thickness but also fiber orientations should be considered as design variables. Besides this, it is explained how these angular variables can improve the structural performance. The generality of the approach is related to the fact that the developed optimization technique is not only dedicated to the design of particular laminates configurations, but is also reliable for general problems including isotropic and/or anisotropic materials, as well as other structural responses. The design problem formulation relies on a direct parameterization of the laminates in terms of the physical design variables, that is orientations and thicknesses, and not on alternative ones like the lamination parameters. Numerical applications, including a non-homogeneous composite membrane design problem and an industrial test case, are presented.
Source: openaire · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Composite Structure Analysis and Optimization · Topology Optimization in Engineering · Structural Analysis and Optimization
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (30)
Show source-provided references
1. Grenestedt JL. Lay-up optimization of composite structures. PhD Thesis, Report 92–94, Royal Institute of Technology of Stockholm, Department of Lightweight Structures; 1992.
2. Optimum design of laminated composite plates using lamination parameters10.2514/3.49033 ↗
3. Miki M. Design of laminated fibrous composite plates with required flexural stiffness. In: Vinson J, Taya M, editors. Recent advances in composites in the United States and Japan, ASTM STP 864 1985: p. 387–400.10.1520/STP32802S ↗
4. Lay-up optimization against buckling of shear panels10.1007/BF01743281 ↗
5. Stiffness design method of symmetric laminates using lamination parameters10.2514/3.11304 ↗
6. Composite plate optimization only requires one parameter10.1007/BF01743518 ↗
7. A procedure for designing laminated plates with required stiffness properties. Application to thin quasi-isotropic quasi-homogenous uncoupled laminates10.1177/002199839903302005 ↗
8. On the design of some particular orthotropic plates with non-standard ply orientations10.1106/V4U2-LTQE-Q1JG-3WN2 ↗
9. A family of MMA approximations for structural optimization10.1007/s00158-002-0238-7 ↗
10. Composite structures optimization using sequential convex programming10.1016/S0965-9978(02)00053-4 ↗
11. BOSS/Quattro. Samtech, Liège, Belgium. Available from: www.samtech.be.
12. SAMCEF. Système d’Analyse des Milieux Continus par Eléments Finis, Samtech, Liège, Belgium. Available from: www.samtech.be.
13. Bruyneel M, Fleury C. The key role of fibers orientations in the optimization of composite structures. Internal Report OA58, LTAS-Multidisciplinary Optimization, University of Liège; 2001.
14. Optimum laminate design for strength and stiffness10.1002/nme.1620070410 ↗
15. Topology optimization of continuum structures with local stress constraints10.1002/(SICI)1097-0207(19981230)43:8<1453::AID-NME480>3.0.CO;2-2 ↗
16. Optimal design of laminated plates and shells10.1016/0263-8223(94)90024-8 ↗
17. On laminate configurations for simultaneous failure10.1177/002199838802200305 ↗
18. Foldager JP. Design of composite structures. PhD Thesis, Special Report No. 39, Aalborg University, Institute of Mechanical Engineering, Denmark; 1999.
19. Determining the real lay-up of a laminate corresponding to optimal lamination parameters by genetic search10.1007/s001580050160 ↗
20. Hammer VB. Design of composite laminates with optimized stiffness, strength, and damage properties. PhD Thesis, Report DCAMM S72, Technical University of Denmark; 1997.
21. Dual methods for convex separable problems
22. Sequential convex programming for structural optimization problems
23. Bruyneel M, Vermaut O, Fleury C. Two point based approximation schemes for optimal orientation in laminates. In: Third ISSMO/UBCAB/UB/AIAA World Congress on structural and multidisciplinary optimization, Amherst, NY, May; 1999 [CD Proceedings].
24. The method of moving asymptotes–A new method for structural optimization10.1002/nme.1620240207 ↗
25. Bruyneel M. Schémas d’approximation pour la conception optimale de structures en matériaux composites. PhD Thesis. Collection des Publications de la Faculté des Sciences Appliquées, no 219, University of Liège; 2002 [in French].
26. Note on topology optimization of continuum structures including self-weight10.1007/s00158-004-0484-y ↗
27. Svanberg K. A globally convergent version of MMA without line search. In: First World Congress of Structural and Multidisciplinary Optimization-WCSMO1, Goslar, Germany, 1995; p. 9–16.
28. Composite laminate stiffnesses and their derivatives
29. Cunningham · 1998
30. Vanderplaats · 1984