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Fatigue Crack Growth Rate Under Irregular Fatigue Loading
2003An 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
Review on uncertainties in fatigue loads and fatigue life of ships and offshore structures
Ocean Engineering, 2022Carlos Guedes Soares
exaly
Mechanistic-empirical analysis of asphalt pavement fatigue cracking under vehicular dynamic loads
Construction and Building Materials, 2021Jingnan Zhao, Hao Wang
exaly
Comprehensive Optimization for Fatigue Loads of Wind Turbines in Complex-Terrain Wind Farms
IEEE Transactions on Sustainable Energy, 2021Lang Li, Songyue Zheng, Dongran R Song
exaly

