Optimization Design and Finite Element Analysis of an Aerofoil's Dominant Truss Structure

In order to further optimize the dominant truss structure inside the aerofoil of a certain aircraft type, an optimization model for the structure is proposed. Firstly, a traditional optimization model is established based on the nonlinear programming method, which regards the deflection of the aerof...

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Bibliographic Details

Published in:	2022 4th International Conference on Artificial Intelligence and Advanced Manufacturing (AIAM) pp. 857 - 864
Main Author:	Chen, Bowei
Format:	Conference Proceeding
Language:	English
Published:	IEEE 01.10.2022
Subjects:	Aerofoil Atmospheric modeling Finite element analysis Force Geometry Linear programming Loading Non-linear programming method Programming Software Truss structure
Online Access:	Get full text
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