RT Journal Article
T1 Development of fatigue cracks from mechanically machined scratches on 2024-T351 aluminium alloy - part I: experimentation and fractographic analysis
A1 Cini, Andrea
A1 P.E., Irving
AB Clad and unclad 2024-T351 alumini um alloy sheets, weakened by mechanically machined scratches, were fatigued to investigate the effect of small surface damage, like scribe marks, on aircraft fuselage joints. The role of scratch cross section geometry on fatigue life of scribed components was analysed. Scratches between 25 and 185 mum deep, with 5, 25 and 50 mum root radii, were cut on sample surface by using diamond-tipped tools. After testing, fracture surfaces were examined using a scanning electron microscope, and crack growth rates were measured by striation counting. Scratches reduced aluminium fatigue life under tensile and bending load up to 97.8% due to multiple crack nucleation at their roots. Short cracks nucleated from sharp scratches coalesced to formunique elongated cracks growing through sample thickness. Cracks initiated fromscratches were typical short cracks, growing faster than conventional long cracks. Despite the different scribing process, fatigue data of regular diamond tool cut scribes can be used to conservatively predict life reduction owing to ploughed in-service scribe marks on fuselage joints. Finite element analyses on scribed samples and the fatigue life prediction models are described in Part II of this paper.
PB Wiley
SN 8756758X (ISSN)
YR 2017
FD 2017-05-01
LK https://hdl.handle.net/10016/39951
UL https://hdl.handle.net/10016/39951
LA eng
NO This research activity was funded by Airbus. The support of Dr Domenico Furfari from Airbus in providing the research group with samples as well of Mr Ben Hopper from Cranfield University in scribing specimens is gratefully acknowledged.
DS e-Archivo
RD 18 jul. 2024