Abstract
An approach intended for the evaluation of total energy released in multi-component defects subjected to ultrasonic stimulation is described. Experimental research was conducted on carbon/carbon composite containing a 25 J impact damage defect. The test sample was ultrasonically stimulated at the frequency of 22 kHz by using a magnetostrictive device. The impact damage was modelled as a pyramid-like set of six single delaminations, and each of them represented an independent heat source. The calculated temperature response was matched to the experimental temperature profile by shape and amplitude thus allowing the evaluation of energy release within the defect.
| Original language | English |
|---|---|
| Pages (from-to) | 167-173 |
| Number of pages | 7 |
| Journal | Composites Part B: Engineering |
| Volume | 165 |
| DOIs | |
| Publication status | Published - 15 May 2019 |
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Keywords
- Carbon/carbon composite
- Energy release
- Impact damage
- Ultrasonic infrared thermography
ASJC Scopus subject areas
- Ceramics and Composites
- Mechanics of Materials
- Mechanical Engineering
- Industrial and Manufacturing Engineering
Cite this
Quantitative study of local heat sources by Ultrasonic Infrared Thermography : An approach for estimating total energy released by low energy impact damage in C/C composite. / Umar, M. Z.; Vavilov, V.; Abdullah, H.; Ariffin, A. K.
In: Composites Part B: Engineering, Vol. 165, 15.05.2019, p. 167-173.Research output: Contribution to journal › Article
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TY - JOUR
T1 - Quantitative study of local heat sources by Ultrasonic Infrared Thermography
T2 - An approach for estimating total energy released by low energy impact damage in C/C composite
AU - Umar, M. Z.
AU - Vavilov, V.
AU - Abdullah, H.
AU - Ariffin, A. K.
PY - 2019/5/15
Y1 - 2019/5/15
N2 - An approach intended for the evaluation of total energy released in multi-component defects subjected to ultrasonic stimulation is described. Experimental research was conducted on carbon/carbon composite containing a 25 J impact damage defect. The test sample was ultrasonically stimulated at the frequency of 22 kHz by using a magnetostrictive device. The impact damage was modelled as a pyramid-like set of six single delaminations, and each of them represented an independent heat source. The calculated temperature response was matched to the experimental temperature profile by shape and amplitude thus allowing the evaluation of energy release within the defect.
AB - An approach intended for the evaluation of total energy released in multi-component defects subjected to ultrasonic stimulation is described. Experimental research was conducted on carbon/carbon composite containing a 25 J impact damage defect. The test sample was ultrasonically stimulated at the frequency of 22 kHz by using a magnetostrictive device. The impact damage was modelled as a pyramid-like set of six single delaminations, and each of them represented an independent heat source. The calculated temperature response was matched to the experimental temperature profile by shape and amplitude thus allowing the evaluation of energy release within the defect.
KW - Carbon/carbon composite
KW - Energy release
KW - Impact damage
KW - Ultrasonic infrared thermography
UR - http://www.scopus.com/inward/record.url?scp=85057384757&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=85057384757&partnerID=8YFLogxK
U2 - 10.1016/j.compositesb.2018.11.124
DO - 10.1016/j.compositesb.2018.11.124
M3 - Article
AN - SCOPUS:85057384757
VL - 165
SP - 167
EP - 173
JO - Composites Part B: Engineering
JF - Composites Part B: Engineering
SN - 1359-8368
ER -