𝔖 Bobbio Scriptorium
✦   LIBER   ✦

Mode III fatigue crack propagation rates in 6061-T6 aluminium

✍ Scribed by R.P. Wright; R.A. Queeney

Publisher
Elsevier Science
Year
1982
Tongue
English
Weight
333 KB
Volume
4
Category
Article
ISSN
0142-1123

No coin nor oath required. For personal study only.

πŸ“œ SIMILAR VOLUMES

Short fatigue crack growth in aluminium
Short fatigue crack growth in aluminium alloy 6082-T6
✍ T. Mann; G. HΓ€rkegΓ₯rd; K. StΓ€rk πŸ“‚ Article πŸ“… 2007 πŸ› Elsevier Science 🌐 English βš– 360 KB

Fatigue crack growth tests on 6082-T6 aluminium specimens have been carried out. The single edge notched tension specimens had a spark eroded 0.2 mm deep starter notch. In order to measure the crack growth, a special direct current potential drop method was used. The experiments were carried out at

Comparison of the simulation and experim
Comparison of the simulation and experimental fatigue crack behaviors in the aluminum alloy HS6061-T6
✍ S.K. Lu; X.H. Yi; L.Yu; Y.L Jiang; W.R. Wei πŸ“‚ Article πŸ“… 2011 πŸ› Elsevier 🌐 English βš– 625 KB

This work deals with rotating bending fatigue tests on aluminum alloy HS6061-T6. Results have been obtained for two sizes of narrow section diameter for specimens with one hole. Results show that fatigue endurance is reduced in the case of the hole. In order to explain this behavior, numerical analy

Fatigue crack propagation rate at low Ξ”K
Fatigue crack propagation rate at low Ξ”K of two aluminum sheet alloys, 2024-T3 and 7075-T6
✍ T.L. Mackay πŸ“‚ Article πŸ“… 1979 πŸ› Elsevier Science 🌐 English βš– 434 KB

For transport aircraft with long lifetimes, crack growth data to implement the durability life requirements in the low AK range are needed. This is the region comprising most of the lifetime for the cracks of interest, and it is also the region where there is little data available. Crack growth data