Influence of Composite Skin on the Energy Absorption Characteristics of an Aircraft Fuselage
In aviation history, accidents during landing are more frequent compared to other phases of flight and in most cases the aircraft is forced to make an emergency belly landing when landing gear malfunctions. This study aims to analyse the energy absorption of a typical composite aircraft fuselage se...
Main Authors: | Sharifah Nadhirah S. A. R., Jaffar Syed Mohammed Ali, Shaik Dawood M. S. I., Adib Hamdani R. |
---|---|
Format: | Article |
Language: | English |
Published: |
Deer Hill Publications
2023-01-01
|
Series: | International Journal of Engineering Materials and Manufacture |
Online Access: | http://deerhillpublishing.com/index.php/ijemm/article/view/247 |
Similar Items
-
Educational software for stress analysis of an aircraft fuselage
by: Mohamed Ali, Jaafar Syed, et al.
Published: (2010) -
Fuselage structures design of an amphibian aircraft /
by: 274441 Norfadzli Abdul Mohamed, et al.
Published: (2008) -
Aircraft Fuselage Corrosion Detection Using Artificial Intelligence
by: Bruno Brandoli, et al.
Published: (2021-06-01) -
EXPERIMENT AND SIMULATION RESEARCH ON UNIFORM SUPERCHARGED FATIGUE CRACK INITIATION OF AIRCRAFT FUSELAGE SKIN
by: LIU LiPing, et al.
Published: (2020-01-01) -
Calculation of longitudinal forces acting on aircraft fuselage /
by: 430131 Phoon, Kin Wah
Published: (1993)