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Design and Optimization of Defense Hole System for Shear Loaded Laminates
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Author(s): Mohammad Al-Husban (Civil Aviation Regulatory Commission, Jordan), Salih N. Akour (Sultan Qaboos University, Oman)and Jamal F. Nayfeh (Prince Mohammad Bin Fahd University, Kingdom of Saudi Arabia)
Copyright: 2012
Pages: 10
Source title:
Technology Engineering and Management in Aviation: Advancements and Discoveries
Source Author(s)/Editor(s): Evon Abu-Taieh (Arab International University, Republic of Syria), Asim El Sheikh (Arab Academy for Banking and Financial Sciences, UAE)and Mostafa Jafari (Research Institute of Forests and Rangelands, Iran)
DOI: 10.4018/978-1-60960-887-3.ch008
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Abstract
Stress concentrations associated with circular holes in pure biaxial shear-loaded laminates can be reduced by up to 20.56%. This significant reduction is made possible by introducing elliptical auxiliary holes along the principal stress direction. The effect of the stacking sequence, the fiber orientation, and the stiffness of both the fiber and the matrix are investigated.
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