Structural integrity assessment of cracked composite plate under aeroelastic loading by means of XFEM

by Abdullah, Nur Azam, Curiel-Sosa, J.L., Wirawan, Nanda, Akbar, Mahesa
Published 2018

Aerofracturelastic on wing box of multi-purpose commuter aircraft under gust lby means of XFEM

by Abdullah, Nur Azam, Wirawan, Nanda, Curiel-Sosa, J.L., Akbar, Mahesa
Published 2018

Analysis on cracked commuter aircraft wing under dynamic cruise load by means of XFEM

by Wirawan, Nanda, Abdullah, Nur Azam, Akbar, Mahesa, Curiel-Sosa, J.L.
Published 2018

Numerical inspection based on Quasi-Static Analysis using Rousselier Damage Model for aluminium wingbox aircraft structure

by Ahmad, M.I.M., Curiel-Sosa, J.L., Akbar, M., Abdullah, Nur Azam
Published 2018

Modelling of transversal crack and delamination under traction with XFEM

by Abdullah, Nur Azam, Curiel-Sosa, J.L., Taylor, Zeike A., Tafazzolimoghaddam, Behrooz, Vicente, J.L Martinez
Published 2017