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Effects of Fatigue Damage on the Microscopic Modulus of Cortical Bone Using Nanoindentation
- Source :
- Materials, Materials, Vol 14, Iss 3252, p 3252 (2021), Volume 14, Issue 12
- Publication Year :
- 2021
- Publisher :
- MDPI, 2021.
-
Abstract
- Alterations to the bone structure from cycle loadings can undermine its damage resistance at multiple scales. The accumulation of fatigue damage in a bone is commonly characterized by the reduction in the elastic modulus. In this study, nano-indentation was used for investigating microscopic damage evolution of bovine tibia samples subjected to fatigue loading. Indentation tests were conducted in the same 60 μm × 120 μm area with different degrees of damage, including fracture, and the evolution of reduced modulus was observed. The results showed that bone’s reduced modulus decreased significantly during the initial 40% of the life fraction, whereas it proceeded slowly during the remaining period. As the size of the residual indentations was about 4 μm in length, the degradation of bone’s reduced modulus reflected the accumulation of fatigue damage at smaller scales.
- Subjects :
- Technology
Materials science
nanoindentation
medicine.medical_treatment
Modulus
030209 endocrinology & metabolism
02 engineering and technology
Article
03 medical and health sciences
0302 clinical medicine
Indentation
reduced modulus
medicine
General Materials Science
Tibia
bone fatigue damage
Composite material
Elastic modulus
Reduction (orthopedic surgery)
Microscopy
QC120-168.85
QH201-278.5
Nanoindentation
Engineering (General). Civil engineering (General)
021001 nanoscience & nanotechnology
TK1-9971
medicine.anatomical_structure
Descriptive and experimental mechanics
hierarchical structure
Fracture (geology)
Cortical bone
Electrical engineering. Electronics. Nuclear engineering
TA1-2040
0210 nano-technology
fatigue test methods
Subjects
Details
- Language :
- English
- ISSN :
- 19961944
- Volume :
- 14
- Issue :
- 12
- Database :
- OpenAIRE
- Journal :
- Materials
- Accession number :
- edsair.doi.dedup.....fb90e5bc6d851a639ccf617cb4a78279