The Thickness of an Aircraft Wing Skins Optimization Based on ABAQUS

Zheng Ran Yang; Yi Jiang; Cong Huang

doi:10.4028/www.scientific.net/AMM.716-717.679

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 716-717The Thickness of an Aircraft Wing Skins...

The Thickness of an Aircraft Wing Skins Optimization Based on ABAQUS

Abstract:

Wing skins play a vital role on the wing structure as well as the inherent characteristics of the wing. The thickness of the wing skins affects many of the key parameters of the wing. To study the impact of the thickness of the wing skins on the modal characteristics of the wing, and to preferable for the thickness of the wing skins, a certain type of aircraft wing model as an example, we carried out on the wing modal analysis and preferable the thickness of the wing skins based on Abaqus. The calculations show that the thickness of the wing skins are all affected on each wing modal frequencies, modal size of displacement and stress.

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Periodical:

Applied Mechanics and Materials (Volumes 716-717)

Pages:

679-681

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.716-717.679

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Cite this paper

Online since:

December 2014

Authors:

Zheng Ran Yang*, Yi Jiang, Cong Huang

Keywords:

ABAQUS, Finite Element Analysis (FEA), Optimization of Skin Thickness

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* - Corresponding Author

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