Effect of the amplitude loading on fatigue crack growth
作者： M. Benachour , A. Hadjoui , M. Benguediab , N. Benachour
DOI: 10.1016/J.PROENG.2010.03.013
关键词:
摘要: The paper presents an experimental work of fatigue crack growth for aerospace 2024 T351 aluminum alloy under constant amplitude loading. At 10 Hz frequency, the effect various amplitudes loading is examined bending V-Charpy specimen. results tests conducted at R=0.1, show on life and rate. fractography examinations were carried out scanning electron microscopic SEM presence striations in Paris region.
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