Phenomenological Methodology for Designing Optimal Styling in the Design of Panels of Aircraft Structures Made of Laminated Composite Material

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The article solves the problem of rapid design of optimal stacking of a polymer laminated composite material of the traditional scheme. The existing engineering technique for laying design is based on constructive-force decomposition. However, this approach does not take into account the joint work of the layers. A solution is proposed that is based on the search for phenomenological dependencies for designing optimal styling parameters. The problem is solved by calculating the carrying capacity of a large number of styling options, searching among them for optimal solutions.

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8-14

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February 2020

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© 2020 Trans Tech Publications Ltd. All Rights Reserved

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[1] O. Erdal, F. O. Sonmez, Optimum design of composite laminates for maximum buckling load capacity using simulated annealing, Compos. Sturct. 71(1) (2005) 45-52.

DOI: 10.1016/j.compstruct.2004.09.008

Google Scholar

[2] M. Akbulut, F. O. Sonmez, Optimum design of composite laminates for minimum thickness, Comp. Struct. 86(21-22) (2008) 1974-1982.

DOI: 10.1016/j.compstruc.2008.05.003

Google Scholar

[3] Cycom 977-2 Composite Material: Impact Test Results, Nasa Technical Reports Server (Ntrs), Washington: BiblioGov, (2013) p.40.

Google Scholar

[4] I. M. Daniel, O. Ishai, Engineering Mechanics of Composite Materials, New York: Oxford University Press, (1994) p.396.

Google Scholar

[5] Z. Gurdal, R. T. Haftka, P. Hajela, Design and optimization of laminated composite materials, Hoboken, New Jersey: John Wiley & Sons, (1999).

Google Scholar

[6] M. C. Y. Niu, Composite airframe structures: practical design information and data, Hong Kong: Hong Kong Conmilit Press Ltd. (1992) p.664.

Google Scholar

[7] G. H. Staab, Laminar composites, Oxford: Butterwort-Heinemann, (1999) p.314.

Google Scholar

[8] S. W. Tsai, Rules of composites design: A review, Metal matrix composites: Proceedings of the ninth international conference on composite materials, ed. Miravete A. - Madrid: University of Zaragora, Woodhead publishing limited, 1 (1993) 113-119.

Google Scholar

[9] V. V. Vasil'yev, Mechanics of composite structures, Moscow: Mashinostroyeniye, (1988) p.272.

Google Scholar

[10] V. V. Vasil'yev, Designing structures of aircraft made of composite materials, Textbook, Moscow: Drofa, (2005) p.784.

Google Scholar

[11] E. M. Vu, Criteria for the destruction of anisotropic media, Composite materials, ed.by Brautman L. i Krok R, 8 (1978) 401-481.

Google Scholar

[12] L. A. Dement'yeva et al. of composite materials based on adhesive prepregs. Adhesives. Sealants. Technology, Moscow: Nauka i tekhnologii, 6 (2012) 19-24.

Google Scholar

[13] V. A. Komarov, A. V. i Chernyayev, Comparative analysis of various approaches to the design of structures of thin-walled elements made of composite materials, Vestnik of Samara University. Aerospace and Mechanical Engineering, Samara: SGAU, 1 (2009) 155-159.

DOI: 10.18287/2541-7533-2021-20-2-45-52

Google Scholar

[14] K. S. Mishurov, K. A. Pavlovskiy, E. S. Imametdinov, The influence of the environment on the properties of carbon fiber VKU-27L, Trudy VIAM, 3 (2018) 60-67.

DOI: 10.18577/2307-6046-2018-0-3-60-67

Google Scholar

[15] A. V. Chernyayev, Optimization of elements of aircraft structures made of composite materials in a discrete formulation, Doctor's thesis, Samara: Samara University, (2012) p.151.

Google Scholar