Abstract
A multicriterion model has been developed for the optimum design of a carbon fiber panel with strengthening ribs under both normal and tangential stress relative to minimalization of both mass and cost. The panel packet consists of elementary layers reinforced in two, three, or four directions with several types of reinforcement filaments for models both homogeneous and heterogeneous over their thickness. A modified intermittently active procedure based on the successive compliance principle was used for optimization.
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N. F. Mormul' and Yu. M. Pochtman, "Multicriterion optimization of strengthened composite panels upon combined loading," Mekh. Kompozitn. Mater., 29, No. 6, 823–830 (1993).
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Yu. M. Pochtman, L. V. Derevyanko, and N. F. Mormul', "Multicriterion optimization of hybrid composite cylindrical shells upon the action of stochastic combined loading," Mekh. Kompozitn. Mater., No. 6, 1094–1100 (1990).
N. F. Mormul', Multicriterion Optimization of Composite Panels and Cylindrical Shells Using Intermittently Active Procedures [in Russian], Technological Sciences Candidate's Dissertation, Dnepropetrovsk (1990).
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Translated from Mekhanika Kompozitnykh Materialov, Vol. 31, No. 3, pp. 370–377, May–June, 1995.
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Mormul', N.F., Pochtman, Y.M. Multicriterion optimization of strengthened hybrid composite panels. Mech Compos Mater 31, 271–276 (1995). https://doi.org/10.1007/BF00615641
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DOI: https://doi.org/10.1007/BF00615641