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Design of composite panels of minimum weight with several cases of loading

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Mechanics of Composite Materials Aims and scope

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Literature cited

  1. V. A. Komarov, “Structures with equal strength made of composite materials,” in: Optimal Design of Aircraft Structures, Issue 1, Kuibyshev (1973), pp. 86–100.

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  2. I. F. Obraztsov, V. V. Vasil'ev, and V. A. Bunakov, Optimum Reinforcement of Shells of Revolution Made of Composite Materials [in Russian], Moscow (1977).

  3. L. M. Vorob'ev and T. M. Vorob'eva, Nonlinear Transformations in Applied Variational Problems [in Russian], Moscow (1972).

  4. F. P. Vasil'ev, Numerical Methods of Solving Extremum Problems [in Russian], Moscow (1980).

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Authors and Affiliations

  1. K. E. Tsiolkovskii Moscow Institute of Aviation Technology, USSR

    A. A. Krikanov

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  1. A. A. Krikanov
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Translated from Mekhanika Kompozitnykh Materialov, No. 5, pp. 868–872, September–October, 1985.

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Krikanov, A.A. Design of composite panels of minimum weight with several cases of loading. Mech Compos Mater 21, 599–602 (1986). https://doi.org/10.1007/BF00610567

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  • DOI: https://doi.org/10.1007/BF00610567

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