Effect of Detail Design on Fatigue Performance of Aircraft Door Frame
Joint Authors
Fusheng, Wang
Zhufeng, Yue
Hangshan, Gao
Jianxiong, Kang
Source
Advances in Mechanical Engineering
Issue
Vol. 2013, Issue 2013 (31 Dec. 2013), pp.1-7, 7 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2013-11-24
Country of Publication
Egypt
No. of Pages
7
Main Subjects
Abstract EN
The fatigue tests were carried out on door frame containing single-side design and double-side design to assess the effect of different designs on fatigue life.
By contrast, the finite element method (FEM) was also used to analyze the stress distribution of the two frames.
At last, the fracture morphologies of the specimens after fatigue test were examined by scanning electron microscopy.
The results revealed that the double-side design could elevate about 18~21 times of fatigue life.
The direction of crack propagation is transverse in single-side frame, while it is longitudinal in double-side frame.
American Psychological Association (APA)
Jianxiong, Kang& Hangshan, Gao& Fusheng, Wang& Zhufeng, Yue. 2013. Effect of Detail Design on Fatigue Performance of Aircraft Door Frame. Advances in Mechanical Engineering،Vol. 2013, no. 2013, pp.1-7.
https://search.emarefa.net/detail/BIM-464049
Modern Language Association (MLA)
Jianxiong, Kang…[et al.]. Effect of Detail Design on Fatigue Performance of Aircraft Door Frame. Advances in Mechanical Engineering No. 2013 (2013), pp.1-7.
https://search.emarefa.net/detail/BIM-464049
American Medical Association (AMA)
Jianxiong, Kang& Hangshan, Gao& Fusheng, Wang& Zhufeng, Yue. Effect of Detail Design on Fatigue Performance of Aircraft Door Frame. Advances in Mechanical Engineering. 2013. Vol. 2013, no. 2013, pp.1-7.
https://search.emarefa.net/detail/BIM-464049
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-464049
