Author:
Cheung Chi Ho Eric,Gray Phillip,Lin Kuen Yuan
Publisher
American Institute of Aeronautics and Astronautics
Reference9 articles.
1. 1Cheung,C.H.E.,andLin,K.Y."ReliabilityofDamageToleranceCompositeStructureUsingFastenersasDisbondArrest Mechanism,"AIAA-2009-2242, 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, PalmSprings, California, May2009.
2. 2Cheung, C. H. E., Gray, M. G., Mabson, G. E., and Lin, K. Y. "Analysis of Fastener as Disbond Arrest Mechanism for Laminated Composite Structures,"AIAA-2010-3024, 51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Orlando, Florida,Apr. 2010.
3. Influence of Fastener Flexibility on the Prediction of Load Transfer and Fatigue Life for Multiple-Row Joints
4. 5Reeder, J., Kyongchan S., Chunchu, P. B., and Ambur, D. R. "Postbuckling and Growth of Delaminations in Composite Plates Subjected to Axial Compression,"43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Denver, Colorado,Apr.2002.
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