Method Studied on the Tensile and Compression Strength Prediction of Friction Stir Welding Aircraft Panel

Zhen Dong Hu; Yang Liu Chen; Xin Song

doi:10.4028/www.scientific.net/KEM.723.142

Paper Titles

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Neutron Spectrometer Used for Nondestructive Detection of Materials Deep Stress: Status of the Project
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Research on Torsion Beam with High Strength Steel Materials Forming
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Method Studied on the Tensile and Compression Strength Prediction of Friction Stir Welding Aircraft Panel
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Friction Stir Forming of A5083 Aluminum Alloy Gear-Racks with WC Particles Embedded in Tooth Surface
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Measurement of Complex Permittivity of Materials Using a Double-Ridge Waveguide Resonator
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Material Testing Based on Cylindrical Cavity
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HomeKey Engineering MaterialsKey Engineering Materials Vol. 723Method Studied on the Tensile and Compression...

Method Studied on the Tensile and Compression Strength Prediction of Friction Stir Welding Aircraft Panel

Abstract:

The tensile and compression strength of the Z shaped stiffened-welded plate is studied in this paper. Through the analysis of the main influential factors of the panel strength, the theoretical calculation formula of the tensile and compression strength of the panel plate which are verified by the experimental values is established in this paper,. And the tensile strength prediction value is 8.4% larger than the experimental value while the compression strength prediction value is 4.36% smaller than the experimental value. This method can provide reference for the selection of welding structure.

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Proceedings of International Conference on Material Science and Engineering 2016

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Periodical:

Key Engineering Materials (Volume 723)

Pages:

142-147

DOI:

https://doi.org/10.4028/www.scientific.net/KEM.723.142

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Online since:

December 2016

Authors:

Zhen Dong Hu*, Yang Liu Chen, Xin Song

Keywords:

Friction Stir Welding, Strength Estimation, Structural Strength, Welded Panels

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