Study on the Ignition Method for n-Octane Pyrolysis Fuel in a Scramjet Engine
Author:
Affiliation:
1. Department of Aerospace Engineering, Tohoku University
2. Kakuda Space Center, Japan Aerospace Exploration Agency
Publisher
Japan Society for Aeronautical and Space Sciences
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://www.jstage.jst.go.jp/article/tjsass/65/1/65_T-20-68/_pdf
Reference44 articles.
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2. 2) Hank, J. M., Murphy, J. S., and Mutzman, R. C.: The X-51A Scramjet Engine Flight Demonstration Program, AIAA Paper 2008-2540, 2008.
3. 3) Tani, K., Onodera, T., Kato, K., and Takegoshi, M.: Flight Experiment for the Validation of New Methodology to Compensate the Wind Tunnel Contamination Problem, Proceedings of 32nd International Symposium on Space Technology and Science, 2019-m-11, June 2019.
4. 4) Powell, O. A., Edwards, J. T., Norris, R. B., Numbers, K. E., and Pearce, J. A.: Development of Hydrocarbon-Fueled Scramjet Engines: The Hypersonic Technology (HyTech) Program, J. Propul. Power, 17 (2001), pp. 1170–1176.
5. 5) Tomioka, S., Hiraiwa, T., Saito, T., Kato, K., Kodera, M., and Tani, K.: System Analysis of a Hydrocarbon-Fueled RBCC Engine Applied to a TSTO Launch Vehicle, Trans. JSASS Aerospace Technology Japan, 12 (2014), pp. Pa_91–Pa_99.
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1. Effects of Thermal/Chemical Nonequilibrium on a High-Mach Ethylene-Fueled Scramjet;Journal of Propulsion and Power;2023-07
2. Dynamic Mode Decomposition of the Combustion Flow Field in a Scramjet Combustor with a Cavity Flameholder;AIAA AVIATION 2023 Forum;2023-06-08
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