Numerical simulation on thermal decomposition of n-dodecane using CFD with reaction model
Author:
Affiliation:
1. Research Unit IV, Japan Aerospace Exploration Agency
2. Department of Aerospace Engineering, Tohoku University
3. Research Unit III, Japan Aerospace Exploration Agency
Publisher
Japan Society of Mechanical Engineers
Link
https://www.jstage.jst.go.jp/article/jfst/19/4/19_2024jfst0032/_pdf
Reference29 articles.
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2. Combustion Research and Flow Technology, Inc., CRUNCH CFD MULTI PHYSICS: V3.3.0 USER GUIDE AND INPUT MANUAL (2019).
3. Coordinating Research Council, Handbook of aviation fuel properties (2004), CRC Report No .635.
4. Dahm, K.D., Virk, P.S., Bounaceur, R., Battin-Leclerc F., Marquaire, P.M., Fournet, R., Daniau, E. and Bouchez, M., Experimental and modelling investigation of the thermal decomposition of n-dodecane, Journal of Analytical and Applied Pyrolysis, Vol. 71, No. 2 (2004), pp. 865-881.
5. Edwards, T., DeWitt, M. J., Shafer, L., Brooks, D., Huang, H., Bagley, S. P., Oña, J. O. and Wornet, M., J., Fuel Composition Influence on Deposition in Endothermic Fuels, 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference (2006), DOI: 10.2514/6.2006-7973.
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