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TOPOLOGY OPTIMIZATION OF POLYMER COMPOSITE WING LOAD-BEARING ELEMENT GEOMETRY

Volumen 50, Edición 3, 2019, pp. 325-339
DOI: 10.1615/TsAGISciJ.2019031136
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SINOPSIS

The topological optimization of a wing and wing box for isotropic and anisotropic materials under operational loads at several angles of attack is performed. The geometrical parameters of carbon fiber elements with a reinforcement pattern different from quasi-isotropic and having different orientation steps of the layers are obtained. The most loaded zones of the structure and the geometric shape of the reinforcement area of the elements are analyzed. The results are considered and used in developing methods of designing a polymer composite wing using parametrical modeling.

REFERENCIAS
  1. Zhu, J.H., Zhang, W.H., and Xia, L., Topology Optimization in Aircraft and Aerospace Structures Design, Arch. Comput. Methods Eng., 23(595):1-28, 2015.

  2. Komarov, V.A., Kishov, E.A., and Charkviani, R.V., Topology Optimization in Designing Heavily Loaded Nodes of Aviation Structures, Polyot, 8:16-23, 2018.

  3. Stanford, B.K. and Dunning, P.D., Optimal Topology of Aircraft Rib and Spar Structures under Aeroelastic Loads, J. Aircraft, 52:1298-1311, 2015.

  4. Krog, L., Tucker, A., Kemp, M., and Boyd, R., Topology Optimization of Aircraft Wing Box Ribs, in Proc. of 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Albany, NY, AIAA Paper 2004-4481, pp. 1-11, 2004.

  5. Vasiliev, B.E. and Magerramova, L.A., Analysis of the Possibility of Applying Topological Optimization in the Design of Uncooled Turbin Blades, Vestnik SGAU, 14(3):139-147, 2015.

  6. Bashin, K.A., Torsunov, R.A., and Semenov, S.V., Methods of Topological Optimization of Structures Applied in the Aerospace Industry, Vestnik PNIPU, 51:51-61, 2017.

  7. Grishin, V.I. and Koledov, M.N., Rational Design of Structures in Accordance with Strength Criteria Using Computing Systems, TsAGI Sci. J, 43(2):247-256,2012.

  8. Rao, J.S., Kiran, S., Kamesh, J.V., Padmanabhan, M.A., and Chandra, S., Topology Optimization of Aircraft Wing, in Proc. ofAltair India S. Asia Hyper Works Technology Conference, Bangalore, India, pp. 1-9,2008.

  9. Rao, J.S. and Kiran, S., Concept Design of Composite Aircraft Wing, in Proc. of ASME International Mechanical Engineering Congress & Exposition, Vancouver, Canada, IMECE Paper 2010-37206, pp. 1-9,2010.

  10. Maksimov, P.V., Krotkikh, A.A., and Ronzhin, B.I., Implementation of the Algorithm based on the Level-Set Method to Solve the Problem of Topological Optimization of Aviation Elements, Nauchno-Tekhnich. Vestn. Povolz., 9:107-110,2018.

  11. Dunning, P.D., Stanford, B.K., and Kim, H.A., Level-Set Topology Optimization with Aeroelastic Constraints, in Proc. of 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, AIAA SciTech Forum, Kissimmee, FL, AIAA Paper 2015-1128, pp. 1-19, 2015.

  12. Dunning, P.D., Stanford, B.K., and Kim, H.A., Aerostructural Level Set Topology Optimization for a Common Research Model Wing, in Proc. of 10th AIAA Multidisciplinary Design Optimization Conference, National Harbor, MD, AIAA Paper 2014-0634, pp. 1-21, 2014.

  13. Felix, L., Gomes, A.A., and Suleman, A., Topology Optimization of a Wing Including Self-Weight Load, in Proc. of 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Structures, Structural Dynamics, and Materials and Co-Located Conferences, Boston, AIAA Paper 2013-1869, pp. 1-17, 2013.

  14. Munk, D.J., Vio, G.A., and Cooper, J.E., Topology Optimization of Representative Aircraft Wing Geometries with an Experimental Validation, in Proc. ofInternational Forum on Aeroelasticity and Structural Dynamics, Como, Italy, pp. 1-12,2017.

  15. Lukomskii, D.K., Ripetskii, A.V., Freilekhman, S.A, and Petrakova, E.V., Topological Optimization of an Object based on Three-Dimensional Modelling, Sovrem. Nauka: Aktual. Probl. Teor. Prakt.. Ser.: Estestv. Tekhnich. Nauki, 11:79-83,2018.

  16. Alexandrin, Yu.S., Tuktarov, S.A., and Chedrik, V.V., Structural Design of Helicopter Wing based on Topology and Global-Local Optimization, TsAGI Sci. J, 48(1):81-96, 2017.

  17. Yang, W., Yue, Z., Li, L., and Wang, P., Aircraft Wing Structural Design Optimization based on Automated Finite Element Modelling and Ground Structure Approach, Eng. Optim., 48(1):94-114, 2016.

  18. Walker, D., Liu, D., and Jennings, A., Topology Optimization of an Aircraft Wing, in Proc. of 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Kissimmee, FL, AIAA Paper 2015-0976, pp. 1-8,2015.

  19. Sleesongsom, S., Bureerat, S., and Tai, K., Aircraft Morphing Wing Design by Using Partial Topology Optimization, Struct. Multidisci. Optim., 48(6):1-20,2013.

  20. Podugu, P. and Ananthasuresh, G.K., Topology Optimization-Based Design of a Compliant Aircraft Wing for Morphing Leading and Trailing Edges, in Proc. of ASME International Mechanical Engineering Congress & Exposition, Vancouver, Canada, IMECE Paper 2010-38159, pp. 1-9, 2010.

  21. Aage, N., Andreassen, E., Lazarov, B.S., and Sigmund, O., Giga-Voxel Computational Morphogenesis for Structural Design, Nature, 550(7674):84-86,2017.

  22. Xinxing, T., Wenjie, G., Chao, S., and Xiaoyong, L., Topology Optimization of Compliant Adaptive Wing Leading Edge with Composite Materials, Chin. J. Aeronaut., 27(6):1488-1498, 2014.

  23. Zhao, Y., Guo, W., Duan, S., Xing, L., A Novel Substructure-Based Topology Optimization Method for the Design of Wing Structure, Int. J Simul. Multidisci. Des. Optim. (IJSMDO), 8(A5):1-9, 2017.

  24. Sivapuram, R., Dunning, P.D., and Kim, H.A., Simultaneous Material and Structural Optimization by Multiscale Topology Optimization, Struct. Multidisci. Optim., 54(5):1267-1281, 2016.

  25. Kishov, E.A. and Komarov, V.A., Topology Optimization of Load-Bearing Structures by the Method of Convex Linearization, Vestnik SGAU, Aerokosmich. Tekh., Tekhnol. Mashinost., 17(1):137-149, 2018.

  26. Venediktov, M.O. and Prokopov, V.S., Topology Optimization with Stress Constraints, in Proc. of XVII International Research-to-Practice Conference on Systems of Design, Technological Preparation of Production and Control of the Lifecycle Stages of an Industry Product (CAD/CAM/PDM-2017), pp. 446-448, Moscow, 2017.

  27. Boyarshinova, I.N. and Ilyinykh, M.S., Combined Technique of Optimal Design of Structures with the Purpose to Reduce Weight, Tsifr. Sred. Proizvod. Inzhen. Anal., pp. 24-31, Tula, Russia, 2017.

  28. James, K.A., Kennedy, G.J., and Martins, J.R.R.A., Concurrent Aerostructural Topology Optimization of a Wing Box, Comput. Struct., 134:1-17, 2014.

  29. Bashin, K.A., Torsunov, R.A., and Semenov, S.V., Methods of Topological Optimization of Structures Applied in Aerospace Industry, Vest. Permsk. Natsion. Issledovat. Politekh. Univ.. Aerokosmich. Tekhn., 51:51-61,2017.

  30. Mikhailovskii, K.V. and Baranovski, S.V., Technique of Designing the Polymer Composite Wing based on Parametrical Modelling, Part 3: Choice and Validation of Optimal Schemes of Reinforcement of Load-Bearing Elements, Izvest. VUZov. Mashinostr., 5(698):75-84, 2018.

CITADO POR
  1. Baranovski S. V., Mikhailovskiy K. V., The methods of designing an ultralight carbon fiber wing using parametrical modeling, XLIV ACADEMIC SPACE CONFERENCE: dedicated to the memory of academician S.P. Korolev and other outstanding Russian scientists – Pioneers of space exploration, 2318, 2021. Crossref

  2. Magidov I.S., Mikhailovskiy K.V., Topological Optimization of the Strength Element of the Aircraft Compartment Made of Metal-Matrix Composite Material, Proceedings of Higher Educational Institutions. Маchine Building, 1 (742), 2022. Crossref

  3. Baranovski S V, Mikhailovskiy K V, Selection and justification of polymer composite wing structural arrangement using parametrical modeling, IOP Conference Series: Materials Science and Engineering, 934, 1, 2020. Crossref

  4. Baranovski S V, Mikhailovskiy K V, Selection and justification of polymer composite wing load-bearing elements design parameters with material anisotropy and airload, IOP Conference Series: Materials Science and Engineering, 934, 1, 2020. Crossref

  5. Baranovski S V, Mikhailovskiy K V, Ultralight structurally optimized carbon fibre reinforced polymer composite wing designing based on parametric modelling and topology optimization, IOP Conference Series: Materials Science and Engineering, 1060, 1, 2021. Crossref

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