Structural integrity assessment on cracked composites interaction with aeroelastic constraint by means of XFEM

Author:

Abdullah Nur Azam,Akbar Mahesa,Wirawan Nanda,Curiel-Sosa Jose Luis

Funder

Ministry of Higher Education, Malaysia

International Islamic University Malaysia

Indonesia Endowment Fund for Education

National Institute of Aeronautics & Space of Indonesia

Indonesian Aerospace

Agency for Assessment & Application of Technology of Indonesia

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference23 articles.

1. Flight test of GL-1 glider half scale prototype;Zulkarnain;J Phys: Conf Ser,2018

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4. Crack-induced changes in divergence and flutter of cantilevered composite panels;Wang;Struct Health Monit,2005

5. Effect of load sequences on crack propagation under random and program loading;Schijve;Eng Fract Mech,1973

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