IIUM Repository

Dr. Nur Azam Abdullah

Assistant Professor

Mechanical Enginering

International Islamic University Malaysia

Aeroelasticity, Fracture Mechanics, Finite Element Analysis, Fluid-structure Interaction, Unsteady Aerodynamics, Composite Structure, Aircraft Design

Ph.D. in Mechanical Engineering, The University of Sheffield (TUoS), United Kingdom (2018). M.Sc in Mechanical Engineering (Research), International Islamic University Malaysia (IIUM), Malaysia. (2014). B.Eng (Hons) in Aerospace Engineering, Islamic University Malaysia (IIUM), Malaysia, (2012).

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Latest Additions

  1. Abdullah, Nur Azam and Wirawan, Nanda and Curiel-Sosa, J.L. and Akbar, Mahesa (2018) Aerofracturelastic on wing box of multi-purpose commuter aircraft under gust lby means of XFEM. In: 6th International Conference Integrity-Reliability-Failure, 22-26 Jul 2018, Lisbon, Portugal.
  2. Abdullah, Nur Azam and Curiel-Sosa, J.L. and Wirawan, Nanda and Akbar, Mahesa (2018) Structural integrity assessment of cracked composite plate under aeroelastic loading by means of XFEM. In: 6th International Conference Integrity-Reliability-Failure, 22-26 Jul 2018, Lisbon, Portugal.
  3. Abdullah, Nur Azam and Curiel-Sosa, Jose Luis and Akbar, Mahesa (2017) Flutter assessment on composite plate with crack by means of fully coupled Finite Element and Doublet Lattice Method. In: 3rd International Conference on Mechanics of Composites (MechComp 2017), 4th-7th July 2017, Bologna, Italy. (Unpublished)
  4. Abdullah, Nur Azam and Curiel-Sosa, J.L. and Taylor, Zeike A. and Tafazzolimoghaddam, Behrooz and Vicente, J.L Martinez (2017) Modelling of transversal crack and delamination under traction with XFEM. In: 3rd International Conference on Mechanics of Composites (MechComp 2017), 4th-7th July 2017, Bologna, Italy. (Unpublished)
  5. Abdullah, Nur Azam and Akbar, Mahesa and Wirawan, Nanda and Curiel-Sosa, Jose Luis (2019) Structural integrity assessment on cracked composites interaction with aeroelastic constraint by means of XFEM. Composite Structures. ISSN 0263-8223
  6. Ahmad, M.I.M. and Curiel-Sosa, J.L. and Akbar, M. and Abdullah, Nur Azam (2018) Numerical inspection based on Quasi-Static Analysis using Rousselier Damage Model for aluminium wingbox aircraft structure. Journal of Physics: Conference Series, 1106. pp. 1-12. ISSN 1742-6588 E-ISSN 1742-6596
  7. Abdullah, Nur Azam and Curiel-Sosa, Jose Luis and Akbar, Mahesa (2018) Aeroelastic assessment of cracked composite plate by means of fully coupled finite element and Doublet Lattice Method. Composite Structures, 202 (SI:Ian Marshall). pp. 151-161. ISSN 0263-8223
  8. Abdullah, Nur Azam and Curiel-Sosa, Jose Luis and Taylor, Zeike A. and Tafazzolimoghaddam, Behrooz and Martinez Vicente, J.L. and Zhang, Chao (2017) Transversal crack and delamination of laminates using XFEM. Composite Structures, 173. pp. 78-85. ISSN 0263-8223
  9. Wirawan, Nanda and Abdullah, Nur Azam and Akbar, Mahesa and Curiel-Sosa, J.L. (2018) Analysis on cracked commuter aircraft wing under dynamic cruise load by means of XFEM. Journal of Physics: Conference Series, 1106. pp. 1-7. ISSN 1742-6588 E-ISSN 1742-6596