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Fatigue crack growth life prediction for a notched beam based on modal frequency |
LIU Wenguang, WANG Yaobin |
School of Aeronautic Manufacturing Engineering, Nanchang Hangkong University, Nanchang 330063, China |
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Abstract Starting from tests of notched beams, fatigue crack growth characteristics and change law of modal frequencies for a V shape-notched cantilever beam under cyclic loads were studied to analyze the relation between modal frequencies and crack growth increment. Crack growth increment was taken as damage parameter to establish the relation between the decline rate of the first order modal frequency and damage parameter. Then, an evolution model for crack damage versus cyclic loading number was set up based on the damage mechanics. A prediction method of fatigue crack growth life was proposed for a cantilever notched beam based on the decline rate of modal frequency using the relation between modal frequency decline rate and crack damage parameter to realize predicting residual fatigue crack growth life of a cantilever beam based on the current crack damage and the corresponding loading cycle number. Results showed that the modal frequency decline rate is sensitive to the fatigue crack growth life of a notched beam; the fatigue crack growth life predicted using the proposed method is basically consistent to the measured one.
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Received: 19 July 2018
Published: 28 December 2019
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