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Aircraft Engineering and Aerospace Technology, 1962
This preliminary investigation has shown that the programme load method of testing provides more useful information than single load level tests enabling a more reliable estimate of a structural joint fatigue life to be obtained.
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This preliminary investigation has shown that the programme load method of testing provides more useful information than single load level tests enabling a more reliable estimate of a structural joint fatigue life to be obtained.
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Stahlbau, 2014
AbstractOffshore wind turbines are subject to dynamic excitation from wave loads. Especially when monopile substructures are used, significant fatigue loads can be induced by waves, which are then governing the design. Calculations in the frequency domain are very efficient to compute such wave induced loads and by applying some simplifications, very ...
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AbstractOffshore wind turbines are subject to dynamic excitation from wave loads. Especially when monopile substructures are used, significant fatigue loads can be induced by waves, which are then governing the design. Calculations in the frequency domain are very efficient to compute such wave induced loads and by applying some simplifications, very ...
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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
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