Experimental Study on Fatigue Life of Four Typical Aircraft Connectors

Author:

Qiao Hongwei,Ren Yunyan,Zhang Hui

Publisher

Springer Nature Singapore

Reference11 articles.

1. Ireman T, Ranvik T, Eriksson I (2000) On damage development in mechanically fastened composite laminates. Compos Struct 49(2):151–171

2. Xiaofei X, Weixing Y (1998) Research on detail design of anti-fatigue of machine structure. Mech Strength 20(1):70–73

3. Liu J, Xu HL, Zhai HB et al (2010) Effect of detail design on fatigue performance of fastener hole. Mater Des 31(2):976–980

4. Qiqing H, Caifeng Z, Zhiping Y (2005) Study on the stress intensity factor of multi-crack crack tip in porous connection structure with contact problem. Mech Strength 27(5):661–665

5. Urban MR (2003) Analysis of the fatigue life of riveted sheet metal helicopter airframe joints. Int J Fatigue 25(9–11):1013–1026

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