Affiliation:
1. Siberian Aeronautical Research Institute named after S.A. Chaplygin
2. Chaplygin Siberian Scientific Research Institute of Aviation
Abstract
The topological optimization method was used to synthesize bionic structures for the promising small aircraft compartment made of aluminum alloy. Topological optimization was performed on the basis of the ESO-SIMP method using the ANSYS Workbench software tools. Influence of the design parameters, in particular, of the shell thickness, on the strength and weight characteristics of the compartment bionic structures after topological optimization was studied under the external loads action.
Publisher
Bauman Moscow State Technical University
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