The crack propagation velocity in corroGon fatigue (du/dN), were measured on the Ni-Cr-Mo steel quenched and tempered at 473 or 773 K. The steel with high sensitivity to delayed failure reveals the largest (du/dN), under square load and the smaller (da/dN), under positive saw tooth load. The frequen
Crack nucleation and propagation of corrosion fatigue in high-strength steel
โ Scribed by Y Hirose; T Mura
- Publisher
- Elsevier Science
- Year
- 1985
- Tongue
- English
- Weight
- 851 KB
- Volume
- 22
- Category
- Article
- ISSN
- 0013-7944
No coin nor oath required. For personal study only.
โฆ Synopsis
Crack nucleation and growth behavior of corrosion fatigue are investigated experimentally and theoretically for 200ยฐC tempered AISI 4340 steel in 35% NaCl solution. The crack nucleation at notch roots is determined by the electrical potential method. The cycle for crack nucleation, N,, increases with the notch radius p and decreases with the apparent stress intensity factor AK,. A linear relation between N, and parameter {?AK,l(np)"' -(?AK,/(np)"'),,,} is observed m a semilog diagram, where 2(2AK,/(npl""),t, is almost equal to the yield shear strength. The influence of stress ratio. R, and cycle frequency. f. on the crack growth rate, 15, is clearly observed. The 18 increases with decreasing f, and the threshold stress intensity factor, AIYFsfC, decreases with decreasing R. In order to explain these experimental results. a new dislocation dipole model is proposed. A model of dislocation dipoles is considered at a notchtip, and diffusion of hydrogen atoms along the line of the pile-up of dislocation dipoles is solved. A certain accumulation of hydrogen atoms at the leading edge of pile-up of dislocation dipoles leads to the crack initiation. A detached crack initiates and grows to the tip of the already existing crack. When the detached crack extends to the tip of the main crack. the process of crack initiation repeats at the tip of a new existing crack. The theory agrees with all the experimental observations.
๐ SIMILAR VOLUMES
In support of Douglas Aircraft Co. structural damage tolerance analysis, crack propagation rates were measured in humid air from lo-\* to 10m3 mm/cycle of several high strength martensitic steels at stress ratios of R = 0.1 and R = 0.5. Increasing the stress ratio was found to decrease the threshold
The criteria for stress corrosion crack branching in high-strength steels are shown to be (1) a constant crack velocity and (2) attainment of a critical stress intensity Klb. For the steels investigated, values of K,b I K,,,, range from 2 to 4. This indicates that when K,, /K,, exceeds 0.5, rapid br
The micromechanics of crack initiation and early growth in 4340 steel is studied using the SEM, and it is found that growth is discontinuous and transgranular, with the distance between growth steps corresponding to the prior austenite grain size spread. The lowest observed growth rate is approximat
Abbxt-Fracture toughness under tensile test and fatigue test on high strength steel at teqrature ranging from room temperature to -180ยฐC were experimentilly studied. The value of fracture toughness under fatigue test is considerably lower than that obtained under tensile test. Within the range from