Study of Aging Technology in Aeronautical Aluminum Alloy Plate Vibration Base on Finite Element Numerical Simulation

Yong Guo

doi:10.4028/www.scientific.net/AMM.644-650.85

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 644-650Study of Aging Technology in Aeronautical Aluminum...

Study of Aging Technology in Aeronautical Aluminum Alloy Plate Vibration Base on Finite Element Numerical Simulation

Abstract:

The vibration aging is an important means to eliminate the residual stress exiting in the structural parts. We establish a typical aluminum alloy plate finite element numerical model with the finite element method and acquire the natural frequencies and the corresponding vibration modes through the modal analysis. At the same time, make use of the numerical simulation of vibration aging process of aluminum alloy plate to study vibration aging effect in different vibration frequencies.

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Periodical:

Applied Mechanics and Materials (Volumes 644-650)

Pages:

85-89

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.644-650.85

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Online since:

September 2014

Authors:

Yong Guo*

Keywords:

Aluminum Alloy Plate, Finite Element Analysis (FEA), Modal, Vibration Aging

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* - Corresponding Author

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