Combustion Behavior of Thermally Cracked Components of n-Dodecane in a Scramjet Model Combustor

Author:

NAKAYA Shinji,NOMURA Toshiki,HIKICHI Yuta,TANAKA Shintaro,CHOI Minho,IMAMURA Osamu,TSUE Mitsuhiro,TOMIOKA Sadatake

Publisher

Japan Society for Aeronautical and Space Sciences

Reference38 articles.

1. 1) Cheng, S.: Hypersonic Propulsion, Progr. Energy Combust. Sci., 15 (1989), pp. 181-202.

2. 2) Ju, Y. and Bioka, T.: Ignition Simulation of Methane/ Hydrogen Mixtures in a Supersonic Mixing Layer, Combust. Flame, 102, 4 (1995), pp.462-470.

3. 3) Ryan, M., Gruber, M., Carter, C. and Mathur, T.: Planar Laser-Induced Fluorescence Imaging of OH in a Supersonic Combustor Fueled with Ethylene and Methane, Proc. Combust. Inst., 32 (2009), pp. 2429-2436.

4. 4) Rasmussen, C. C., Driscoll, J. F., Hsu, K.-Yu, Donbar, J. M., Gruber, M. R. and Carter, C. D.: Stability Limits of Cavity-Stabilized Flames in Supersonic Flow, Proc. Combust. Inst., 30 (2005), pp. 2825-2833.

5. 5) Micka, D. J. and Driscoll, J. F.: Combustion Characteristics of a Dual-Mode Scramjet Combustor with Cavity Flameholder, Proc. Combust. Inst., 32 (2009), pp. 2397-2404.

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