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- [4] Link-up strength of 2524-T3 and 2024-T3 aluminum panels with multiple site damage JOURNAL OF AIRCRAFT, 2005, 42 (02): : 535 - 541
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- [6] Residual strength of stiffened panels with multiple site damage FATIGUE '99: PROCEEDINGS OF THE SEVENTH INTERNATIONAL FATIGUE CONGRESS, VOLS 1-4, 1999, : 2515 - 2520
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- [10] Test research of residual strength on aluminum panels with multiple site damage Hangkong Cailiao Xuebao/Journal of Aeronautical Materials, 2007, 27 (02): : 13 - 17