The propagation behavior of small fatigue cracks in smooth specimens of an aluminum alloy (2024-T6) reinforced with 20% volume of SiC particles was studied under load-and displacement-controlled cyclic conditions. The development of crack closure with crack extension was measured through the complia
The role of fracture toughness in low-cycle fatigue crack propagation for high-strength alloys
โ Scribed by Thomas W. Crooker
- Publisher
- Elsevier Science
- Year
- 1973
- Tongue
- English
- Weight
- 730 KB
- Volume
- 5
- Category
- Article
- ISSN
- 0013-7944
No coin nor oath required. For personal study only.
โฆ Synopsis
Ahabnet-The trend toward broader application of high-strength structural alloys has increased the potential for failure by low-cycle fatigue crack propagation. There is a signiBcant probability that complex structures will contain undetected cracks remaining from fabrication or that cracks will readily initiate from less severe fabrication defects. Under the repeated application of high stresses. imposed on hi-strength alloys, such cracks will rapidly grow in low-cycle fatigue. To guard against disastrous failures caused by cracks propagating to terminal fracture, high-strength structural alloys which also possess high levels of fracture resistance have been developed in recent years. This paper describes the principal fatigue crack propagation characteristics which are derived from high fracture toughness and discusses the potential benefits available through the use of high-toughness alloys in cyclically-loaded structures.
๐ SIMILAR VOLUMES
Experiments have been made to investigate the effect of mean stress on fatigue crack propagation in +in. (12.7mm) thick specimens of six aluminium alloys of high and low fracture toughness. The resuits are presented in terms of the stress intensity factor range, AK and the R value where R is the rat
Centrally cracked specimens of JIS SM58Q and I-IT80 steels were fatigued. The fatigue crack growth rates, da/dn, and the stress intensity threshold levels, AK,, were measured over the range of stress ratio, R, from -1 to 0.8 by the use of an automatic method of continuously decreasing stress intensi