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Received December 24, 2011
Accepted March 10, 2012
- This is an Open-Access article distributed under the terms of the Creative Commons Attribution Non-Commercial License (http://creativecommons.org/licenses/bync/3.0) which permits unrestricted non-commercial use, distribution, and reproduction in any medium, provided the original work is properly cited.
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Surface recession mechanism of carbon fiber reinforced plastic layer by thermal decomposition
1Safety Research Division, Institute of Gas Safety R&D, Gyeonggi-do 429-712, Korea 2Department of Chemical Engineering, The University of Seoul, Seoul 130-743, Korea 3Korea Institute of Science and Technology (KIST), Seoul 136-791, Korea
hkim@uos.ac.kr
Korean Journal of Chemical Engineering, November 2012, 29(11), 1508-1515(8), 10.1007/s11814-012-0036-x
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Abstract
We tested the thermal resistance of a carbon-fiber-reinforced fuel storage tank by using the simulations and the experiments. A model describing the one-dimensional heat transfer in a composite wall exposed to a flame was developed. As a moving boundary condition, the thickness recession is expressed by the one-step Arrhenius-type decomposition kinetics. The differential equations are solved by the Crank-Nicolson method, the algorithm of which is developed by us. For the experimental verification of the simulation, the well-controlled heat is added to one side of the square specimen taken from a carbon-fiber-wounded epoxy cylinder and the change in mass of the specimen is recorded as time passes. From the comparison of the results of two methodologies, it is hypothesized that the normalized thickness by the initial value should be always equal to the normalized mass by the initial value at a certain time. As a result, the surface recession data obtained by the simulations provide good predictions for those by the experiments.
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References
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Dodds N, Gibson AG, Dewhurst D, Davis JM, Compo.: Part A., 31, 689 (2000)
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Trelles J, Lattimer BY, Fire Mater., 31, 147 (2007)
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Sohn Y, Baek SW, Kashiwagi T, Combust. Sci. Technol., 145(1-6), 83 (1999)
Mouritz AP, Mathys Z, Compo. Sci. Technol., 61, 475 (2001)
Gibson AG, Wright PNH, Wu YS, Mouritz AP, Mathys Z, Gardiner CP, Plastics, Rubber and Compo., 32, 81 (2003)
Gardiner CP, Mathys Z, Mouritz AP, Marin Struct., 17, 53 (2004)
Burchill PJ, Mathys Z, Gardiner CP, Fire Mater., 29, 249 (2005)
Griffis CA, Masumura RA, Chang CI, J. Comp. Mater., 15, 427 (1981)
Kindelan M, Linan A, Acta Astronaut., 5, 1199 (1978)
Keller T, Tracy C, Zhou A, Compo.: Part A., 37, 1286 (2006)
Staggs JEJ, Polym. Degrad. Stabil., 82, 297 (2003)
Lyon RE, Quintiere JG, Combust. Flame, 151(4), 551 (2007)
ISO 5660-1 (2002)
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JIa F, Galea ER, Patel MK, Fire Mater., 23, 71 (1999)