A cumulative model of fatigue crack growth Export

@article{glinka82, abstract = {A model of fatigue crack growth based on an analysis of elastic/plastic stress and strain at the crack tip is presented. It is shown that the fatigue crack growth rate can be calculated by means of the local stress/strain at the crack tip. The local stress and strain calculations are based on the general solutions given by Hutchinson, Rice and Rosengren. It is assumed that a small highly strained area existing at the crack tip is responsible for the fatigue crack growth. It is also assumed that the fatigue crack growth rate depends mainly on the width, x*, of the highly strained zone and on the strain range, [Delta][epsilon]*, within the zone. A relationship between stress intensity factor K and the local strain and stress has been developed. It is possible to calculate the local strain for a variety of crack problems. Then, the number of cycles N* required for material failure inside the highly strained zone is calculated. The fatigue crack growth rate is calculated as the ratio x*/N*.The calculated fatigue crack growth rates were compared to the experimental ones. Two alloys steels and two aluminium alloys were analyzed. Good agreement between experimental and theoretical results is obtained.}, author = {Glinka, G.}, citeulike-article-id = {449677}, citeulike-linkout-0 = {http://www.sciencedirect.com/science/article/B6V35-481F1DM-1/2/461cd09b1b1cbec374779f41c97665aa}, journal = {International Journal of Fatigue}, keywords = {2219, 7075, bibtex-import, crack, growth, imporant, notch, theoretical, vs}, month = {April}, number = {2}, pages = {59--67}, pdf = {glinka82.pdf}, posted-at = {2005-12-25 12:44:50}, priority = {2}, title = {A cumulative model of fatigue crack growth}, url = {http://www.sciencedirect.com/science/article/B6V35-481F1DM-1/2/461cd09b1b1cbec374779f41c97665aa}, volume = {4}, year = {1982} }

TY - JOUR ID - glinka82 L3 - citeulike-article-id:449677 N2 - A model of fatigue crack growth based on an analysis of elastic/plastic stress and strain at the crack tip is presented. It is shown that the fatigue crack growth rate can be calculated by means of the local stress/strain at the crack tip. The local stress and strain calculations are based on the general solutions given by Hutchinson, Rice and Rosengren. It is assumed that a small highly strained area existing at the crack tip is responsible for the fatigue crack growth. It is also assumed that the fatigue crack growth rate depends mainly on the width, x*, of the highly strained zone and on the strain range, [Delta][epsilon]*, within the zone. A relationship between stress intensity factor K and the local strain and stress has been developed. It is possible to calculate the local strain for a variety of crack problems. Then, the number of cycles N* required for material failure inside the highly strained zone is calculated. The fatigue crack growth rate is calculated as the ratio x*/N*.The calculated fatigue crack growth rates were compared to the experimental ones. Two alloys steels and two aluminium alloys were analyzed. Good agreement between experimental and theoretical results is obtained. IS - 2 JF - International Journal of Fatigue EP - 67 TI - A cumulative model of fatigue crack growth VL - 4 SP - 59 KW - 2219 KW - 7075 KW - bibtex-import KW - crack KW - growth KW - imporant KW - notch KW - theoretical KW - vs AU - Glinka, G PY - 1982/April// UR - http://www.sciencedirect.com/science/article/B6V35-481F1DM-1/2/461cd09b1b1cbec374779f41c97665aa ER -