Effect of Detail Design on Fatigue Performance of Aircraft Door Frame

المؤلفون المشاركون

Fusheng, Wang
Zhufeng, Yue
Hangshan, Gao
Jianxiong, Kang

المصدر

Advances in Mechanical Engineering

العدد

المجلد 2013، العدد 2013 (31 ديسمبر/كانون الأول 2013)، ص ص. 1-7، 7ص.

الناشر

Hindawi Publishing Corporation

تاريخ النشر

2013-11-24

دولة النشر

مصر

عدد الصفحات

7

التخصصات الرئيسية

هندسة ميكانيكية

الملخص 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.

نمط استشهاد جمعية علماء النفس الأمريكية (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

نمط استشهاد الجمعية الأمريكية للغات الحديثة (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

نمط استشهاد الجمعية الطبية الأمريكية (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

نوع البيانات

مقالات

لغة النص

الإنجليزية

الملاحظات

Includes bibliographical references

رقم السجل

BIM-464049