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

QR Code

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

In this paper, a new investigation of crack propagation on a commuter aircraft wing is discussed. The aircraft is a 19-seater multi-purpose commuter aircraft designed for a mission on the remote area. The dynamic load acting on the wing is assumed as harmonic load considering aerodynamic lift at...

Full description

Bibliographic Details
Main Authors:	Wirawan, Nanda, Abdullah, Nur Azam, Akbar, Mahesa, Curiel-Sosa, J.L.
Format:	Proceeding Paper
Language:	English English English
Published:	IOP Publishing Ltd 2018
Subjects:	TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/72822/ http://irep.iium.edu.my/72822/1/72822%20Analysis%20on%20Cracked%20Commuter.pdf http://irep.iium.edu.my/72822/2/72822%20Analysis%20on%20Cracked%20Commuter%20SCOPUS.pdf http://irep.iium.edu.my/72822/13/72822%20slides.pdf

Similar Items

Aerofracturelastic on wing box of multi-purpose commuter aircraft under gust lby means of XFEM
by: Abdullah, Nur Azam, et al.
Published: (2018)

Structural integrity assessment of cracked composite plate under aeroelastic loading by means of XFEM
by: Abdullah, Nur Azam, 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)

Modelling of transversal crack and delamination under traction with XFEM
by: Abdullah, Nur Azam, et al.
Published: (2017)

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)

Transversal crack and delamination of laminates using XFEM
by: Abdullah, Nur Azam, et al.
Published: (2017)

Aeroelastic assessment of cracked composite plate by means of fully coupled finite element and Doublet Lattice Method
by: Abdullah, Nur Azam, et al.
Published: (2018)

Effect of wing loading on gross takeoff mass of a hybrid buoyant aircraft
by: UlHaque, Anwar, et al.
Published: (2016)

Literature review : Biomimetic and conventional aircraft wing tips
by: Ahmed Siddiqui, Naseeb, et al.
Published: (2017)

Evaluation of aircraft wing-tip vortex using PIV
by: Elsayed, Omer Ali, et al.
Published: (2009)

Numerical inspection based on Quasi-Static Analysis using Rousselier Damage Model for aluminium wingbox aircraft structure
by: Ahmad, Meor iqram Meor, et al.
Published: (2018)

The development of a fixed wing aircraft analysis and design flight dynamic software
by: Ahmad Alaian, Ahmad Eshtiwey
Published: (2016)

Flutter analysis of supersonic wing with external stores
by: Abdullah, Nur Azam, et al.
Published: (2013)

Aeroelastic tailoring of oscillating supersonic wing with external stores
by: Abdullah, Nur Azam, et al.
Published: (2014)

Aeroelastic flutter analysis of supersonic wing with multiple external stores
by: Abdullah, Nur Azam, et al.
Published: (2014)

A matlab based educational software for the study on the effect of cut-out in aircraft wings
by: Mohammed Riyadh, Miah, et al.
Published: (2018)

Numerical investigation of the flow over delta wing and reverse delta wing
by: Ludin@Jamaluddin, Hani, et al.
Published: (2015)

Hybrid buoyant aircraft: future STOL aircraft for interconnectivity of the Malaysian islands
by: UlHaque, Anwar, et al.
Published: (2017)

Roll control reversal of variable swept wing in supersonic flow
by: Ibren, Mohamed, et al.
Published: (2019)

Numerical investigation of the vortical flow over delta wing and reverse delta wing
by: Omar, Ashraf Ali E., et al.
Published: (2012)

Aerodynamics of porous airfoils and wings
by: Mohammed Aldheeb, Mohammed Abdulmalek, et al.
Published: (2018)

Study of the reverse delta wing
by: Altaf, Afaq, et al.
Published: (2011)

Experimental investigation of wing tip vortex
by: Elsayed, Omer Ali, et al.
Published: (2009)

Aerodynamic performance of a naca 23012 half wing model with a reverse delta wing type add-on device
by: Asrar, Waqar, et al.
Published: (2015)

A review on aerodynamics of nonflapping bird wings
by: Mohammed Aldheeb, Mohammed Abdulmalek, et al.
Published: (2016)

Conceptual design of a winged hybrid airship
by: UlHaque, Anwar, et al.
Published: (2014)

Educational software for stress analysis of an aircraft fuselage
by: Mohamed Ali, Jaafar Syed, et al.
Published: (2010)

Flow visualization over a circular planform wing
by: Suliman , M. M. Ali, et al.
Published: (2013)

Experimental investigation of free wing IIUM-UAV configuration
by: Omar, Ashraf Ali, et al.
Published: (2010)

Adapting a propeller noise model for aircraft at cruising altitudes
by: Blunt, D., et al.
Published: (2014)

Crash analysis of an aircraft fuselage under belly landing
by: Syed Mohamed Ali, Jaffar, et al.
Published: (2017)

Framework of conceptual design methodology for hybrid buoyant aircraft
by: UlHaque, Anwar, et al.
Published: (2016)

Effect of a directionally porous wing tip on tip vortex
by: Mohammed Aldheeb, Mohammed Abdulmalek, et al.
Published: (2020)

Investigation of the vortical flow around a reverse delta wing
by: Altaf, Afaq, et al.
Published: (2011)

Induced rolling moment for NACA4412 plain and flapped wing
by: Elsayed, Omer Ali, et al.
Published: (2010)

Half model testing for canard of a hybrid buoyant aircraft
by: UlHaque, Anwar, et al.
Published: (2015)

Stability and takeoff ground roll issues of hybrid buoyant aircraft
by: UlHaque, Anwar, et al.
Published: (2014)

Design and fabrication of a winged hybrid airship model for IIUM-LSWT
by: UlHaque, Anwar, et al.
Published: (2015)

Development of IIUM Free Wing Unmanned Aerial Vehicle (IIUM-FWUAV)
by: Omar, Ashraf Ali, et al.
Published: (2010)

Aerostatic and aerodynamic modules of a hybrid buoyant aircraft: an analytical approach
by: UlHaque, Anwar, et al.
Published: (2015)