Abstract
The paper considers the solution of the problem of determining the topology of the heated load-bearing structure and the size of the load-carrying elements that provide minimum compliance within a given mass using the criteria method of evolutionary optimization. The test cases are solved.
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Russian Text © The Author(s), 2019, published in Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2019, No. 4, pp. 27–35.
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Kretov, A.S., Shataev, P.A. Structural Optimization of Load-Bearing Heated Structures. Russ. Aeronaut. 62, 555–563 (2019). https://doi.org/10.3103/S1068799819040044
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DOI: https://doi.org/10.3103/S1068799819040044