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.
Structural Optimization of Load-Bearing Heated Structures
Russ. Aeronaut.
Russian Aeronautics ; 62 , 4 ; 555-563
2019-10-01
9 pages
Article (Journal)
Electronic Resource
English