Evaluation of Calendar Damage of Aircraft Structures Using Acoustic Emission


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Key Engineering Materials (Volumes 270-273)

Edited by:

Seung-Seok Lee, Dong-Jin Yoon, Joon-Hyun Lee and Sekyung Lee




R. S. Geng "Evaluation of Calendar Damage of Aircraft Structures Using Acoustic Emission", Key Engineering Materials, Vols. 270-273, pp. 503-509, 2004

Online since:

August 2004





[1] Geng R S. Acoustic Emission Evaluation of the Initiation and Growth of Fatigue Cracks in Aircraft Main Structures[J], Non-Destructive Testing (in Chinese), 1999, 21(4).

[2] Geng R S, Fu G X, Source Mechanism of Acoustic Emission Produced by Pitting Corrosion, Acta Acustica[J], 2002, 27(4), 369-372.

[3] Geng R S, Shen G T, An Overview of the Development of Acoustic Emission Signal Processing and Analysis Technique[J], Non-Destructive Testing (in Chinese), 2002, 24(1): 23-28.

[4] Shen G T, Geng R S, Parameter Analysis of Acoustic Emission Signals[J], Non-Destructive Testing (in Chinese), 2002, 24(2): 72-77.

[5] Ландау Л Д, Лифшиц E.M. Механика сплошных сред, Гостехиздат, (1962).

[6] Gorman MR, Plate wave acoustic emission[J], JASA, 1991, 90(1): 358-364.

[7] Dunegan H L, Modal Analysis of Acoustic Emission Signals[J], Journal of Acoustic Emission, 1998(15), 1-4 Zhang D, Equivalent Environmental Spectrum of Determining Aircraft Calendar Life[J], Acta Aeronautica et Astronautica Sinica, 2000, 21(3) : 128-133.

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