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...
محفوظ في:
المؤلفون الرئيسيون: | Wirawan, Nanda, Abdullah, Nur Azam, Akbar, Mahesa, Curiel-Sosa, J.L. |
---|---|
التنسيق: | Conference or Workshop Item |
اللغة: | English English English |
منشور في: |
IOP Publishing Ltd
2018
|
الموضوعات: | |
الوصول للمادة أونلاين: | 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 http://irep.iium.edu.my/72822/ https://iopscience.iop.org/article/10.1088/1742-6596/1106/1/012014/pdf |
الوسوم: |
إضافة وسم
لا توجد وسوم, كن أول من يضع وسما على هذه التسجيلة!
|
مواد مشابهة
-
Aerofracturelastic on wing box of multi-purpose commuter aircraft under gust lby means of XFEM
بواسطة: Abdullah, Nur Azam, وآخرون
منشور في: (2018) -
Structural integrity assessment of cracked composite plate under aeroelastic loading by means of XFEM
بواسطة: Abdullah, Nur Azam, وآخرون
منشور في: (2018) -
Structural integrity assessment on cracked composites interaction with aeroelastic constraint by means of XFEM
بواسطة: Abdullah, Nur Azam, وآخرون
منشور في: (2019) -
Modelling of transversal crack and delamination under traction with XFEM
بواسطة: Abdullah, Nur Azam, وآخرون
منشور في: (2017) -
Flutter assessment on composite plate with crack by means of fully coupled Finite Element and Doublet Lattice Method
بواسطة: Abdullah, Nur Azam, وآخرون
منشور في: (2017)