Fatigue crack growth from corrosion damage in 7075-T6511 aluminium alloy under aircraft loading

DuQuesnay, D. L. / Underhill, P. R. / Britt, H. J. | British Library Online Contents | 2003

Thermal Ageing Effects on the Residual Fatigue Strength of AA2618-T6511 Aluminium Alloy

Molari, P. G. / Morelli, P. / Maldotti, S. et al. | British Library Online Contents | 2006

Fracture mechanics modelling of constant and variable amplitude fatigue behaviour of field corroded 7075‐t6511 aluminium

McMurtrey, M.D. / Bae, D. / Burns, J.T. | British Library Online Contents | 2017

Mesh-less simulation of the penetration of 6061-T6511 aluminum alloy target by a semi-spherical rigid projectile

Zaidi, A. M. A. / Li, Q. M. | British Library Conference Proceedings | 2005

Microstructure characterization of 7055-T6, 6061-T6511 and 7A52-T6 Al alloys subjected to ballistic impact against heavy tungsten alloy projectile

Khan, M. A. / Wang, Y. / Malik, A. et al. | Springer Verlag | 2019