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Fatigue Crack Growth Rate Under Irregular Fatigue Loading

2003
An aircraft cracked component can be approximated as a wide plate with a centre-crack. The component is subjected to the following repeated load sequence: 5, 120, 15, 91, 18, 75, 40, 80, 10, 110 MPa. A crack of length 20 mm has been detected in the component.
Sp. Pantelakis, P. Papanikos
openaire   +1 more source

Fatigue Loading

2003
WATANABE I.   +6 more
  +6 more sources

Mechanistic-empirical analysis of asphalt pavement fatigue cracking under vehicular dynamic loads

Construction and Building Materials, 2021
Jingnan Zhao, Hao Wang
exaly  

Comprehensive Optimization for Fatigue Loads of Wind Turbines in Complex-Terrain Wind Farms

IEEE Transactions on Sustainable Energy, 2021
Lang Li, Songyue Zheng, Dongran R Song
exaly  

Data‐driven prediction and interpretation of fatigue damage in a road‐rail suspension bridge considering multiple loads

Structural Control and Health Monitoring, 2022
Zhen Sun, JoÃo Santos, Elsa Caetano
exaly  

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