Aerofracturelastic on wing box of multi-purpose commuter aircraft under gust lby means of XFEM
In this paper, crack behavior of an aluminum wing box under gust load is presented. The investigated wing box is based on one of the design prototypes of a multi-purpose commuter aircraft. The wing box has been tested experimentally for the vibration test and flutter test. The results of both tests...
Main Authors: | Abdullah, Nur Azam, Wirawan, Nanda, Curiel-Sosa, J.L., Akbar, Mahesa |
---|---|
Format: | Conference or Workshop Item |
Language: | English |
Published: |
2018
|
Subjects: | |
Online Access: | http://irep.iium.edu.my/74974/ http://irep.iium.edu.my/74974/1/7208.pdf |
Similar Items
-
Structural integrity assessment of cracked composite plate under aeroelastic loading by means of XFEM
by: Abdullah, Nur Azam, et al.
Published: (2018) -
Modelling of transversal crack and delamination under traction with XFEM
by: Abdullah, Nur Azam, et al.
Published: (2017) -
Analysis on cracked commuter aircraft wing under dynamic cruise load by means of XFEM
by: Wirawan, Nanda, et al.
Published: (2018) -
Structural integrity assessment on cracked composites interaction with aeroelastic constraint by means of XFEM
by: Abdullah, Nur Azam, et al.
Published: (2019) -
Flutter assessment on composite plate with crack by means of fully coupled Finite Element and Doublet Lattice Method
by: Abdullah, Nur Azam, et al.
Published: (2017)