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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Veröffentlicht in:	2022 4th International Conference on Artificial Intelligence and Advanced Manufacturing (AIAM) S. 857 - 864
1. Verfasser:	Chen, Bowei
Format:	Tagungsbericht
Sprache:	Englisch
Veröffentlicht:	IEEE 01.10.2022
Schlagworte:	Aerofoil Atmospheric modeling Finite element analysis Force Geometry Linear programming Loading Non-linear programming method Programming Software Truss structure
Online-Zugang:	Volltext
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