An analytical model based on cumulative damage has been used for predicting the damage evolution in composite materials. The model is verified with experimental data from a carbon/epoxy composite fatigued under tension-tension load. Fatigue tests of specimens have been monitored with an infra-red th
Damage evolution and fatigue debonding of diamond films under repeated loading
β Scribed by Shoji Kamiya; Hitoshi Sekino; Hiroyuki Hanyu; Joana C. Madaleno; Jose Gracio
- Publisher
- Elsevier Science
- Year
- 2008
- Tongue
- English
- Weight
- 689 KB
- Volume
- 203
- Category
- Article
- ISSN
- 0257-8972
No coin nor oath required. For personal study only.
β¦ Synopsis
It was aimed in this study to investigate the fundamental fatigue damage of CVD diamond films deposited on silicon substrate. In order to eliminate complicated dynamic surface interaction, fatigue experiment was performed with a quasi static cyclic load applied by spherical indenters at 10 Hz. The initial fatigue damage appeared on the substrate surface under the diamond film as small cracks, followed by partial debonding of the diamond film. This also meant that silicon was susceptible to fatigue even under the environment hermetically sealed with surface coating. Fatigue lifetime before debonding was successfully characterized as stress-number of cycles (S-N) diagram.
π SIMILAR VOLUMES
An experimental investigation of adhesively bonded composite joint was conducted to characterize the debond growth mechanism under mode II static and fatigue loadings. For this purpose, end-notched flexure specimens of graphite/epoxy (T300/5208) adherends bonded with EC 3445 adhesive were tested. In
A consolidation of powders using the KOBO method at elevated temperature was elaborated for production of Al/SiC metal matrix composite (MMC). The observations of the mean strain and inelastic strain range during the force controlled high cycle fatigue (HCF) tests identified the ratcheting mechanism
## a b s t r a c t Based on the critical plane approach, a new damage parameter for multiaxial fatigue damage is presented. Both components of strain and stress are considered in this parameter. Thus, a new multiaxial fatigue damage model is given based on the critical plane approach. The capabili