کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
7153701 1462488 2018 9 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Prediction of fatigue crack growth rate for small-sized CIET specimens based on low cycle fatigue properties
ترجمه فارسی عنوان
پیش بینی سرعت رشد ترک خستگی برای نمونه های کوچک و کوچک بر اساس ویژگی های خستگی چرخه کم
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی هوافضا
چکیده انگلیسی
Based on experiments of low cycle fatigue for 5083-H112 aluminum alloy, two energy-based predictive models have been introduced to predict the fatigue crack growth behaviors of traditional Compact Tension (CT) and small-sized C-shaped Inside Edge-notched Tension (CIET) specimens with different thicknesses and load ratios. Different values of the effective stress ratio U are employed in the theoretical fatigue crack growth models to correct the effect of crack closure. Results indicate that the two predictive models show different capacities of predicting the fatigue crack growth behaviors of CIET and CT specimens with different thicknesses and load ratios. The accuracy of predicted results of the two models is strongly affected by the method for determination of the effective stress ratio U. Finally, the energy-based Shi&Cai model with crack closure correction by means of Newman's method is highly recommended in prediction of fatigue crack growth of CIET specimens via low cycle fatigue properties.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Chinese Journal of Aeronautics - Volume 31, Issue 4, April 2018, Pages 740-748
نویسندگان
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