Optimization of composite patch repair for center-cracked rectangular plate using design of experiments method

• المؤلفون الرئيسيون: Aabid, Abdul, Hrairi, Meftah, Mohamed Ali, Jaffar Syed
• التنسيق: Conference or Workshop Item
• اللغة: English; English; English
• منشور في: Elsevier Ltd 2020
• الموضوعات: TL500 Aeronautics; TS200 Metal manufactures. Metalworking
• الوصول للمادة أونلاين: http://irep.iium.edu.my/81790/13/81790_Optimization%20of%20composite%20patch%20repair%20for%20center-cracked.pdf; http://irep.iium.edu.my/81790/7/81790_Optimization%20of%20composite%20patch%20repair%20for%20center-cracked_SCOPUS.pdf; http://irep.iium.edu.my/81790/14/81790_Optimization%20of%20composite%20patch%20repair%20for%20center-cracked_WOS.pdf; http://irep.iium.edu.my/81790/; https://www.sciencedirect.com/science/article/pii/S2214785320324214

The repair of aircraft structures using composite material patches are well known in aerospace industries. In the present work composite patch bonded with a superglue over a cracked rectangular plate under uniform uniaxial tensile stress is considered. A three-dimensional finite element method was u...