首页 | 本学科首页   官方微博 | 高级检索  
     


The effect of notch geometry on critical distance high cycle fatigue predictions
Authors:David B Lanning  Theodore Nicholas  Anthony Palazotto
Affiliation:aCollege of Engineering, Embry-Riddle Aeronautical University, 3700 Willow Creek Road, Prescott, AZ 86301-3720, USA;bAir Force Institute of Technology, 2950 Hobson Way, Building 640, Wright-Patterson AFB, OH 45433-7765, USA
Abstract:A critical distance method for predicting the fatigue limit stresses of notched specimens was implemented for notched specimens with a wide range of notch dimensions. Circumferentially notched cylindrical specimens (kt=1.97–4.07) taken from Ti–6Al–4V forged plate were cycled to failure (R=0.1 and 0.5) using a step loading method for estimating the 106 cycle fatigue limit stresses. These experimental data were used in combination with finite element solutions for all specimen geometries to determine a ‘critical distance’, a quantity or parameter determined from the stress distribution surrounding the notch in combination with fatigue limit stress data from unnotched specimens. A unique parameter was not found for all of the specimen geometries. However, predictions for the fatigue limit stresses of the larger notch geometries may be made with some amount of accuracy using a single value of the critical distance parameter, while reasonable predictions for the specimens with the smallest notch dimensions may be made upon the recognition of an apparent size effect.
Keywords:High cycle fatigue  Notches  Critical distance  Ti–  6Al–  4V
本文献已被 ScienceDirect 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号