Computational-experimental study of hydrogen ignition with distributed injection from pylons into a supersonic flow
Author:
Publisher
AIP Publishing
Link
http://aip.scitation.org/doi/pdf/10.1063/5.0052139
Reference8 articles.
1. Historical Survey on Enhanced Mixing in Scramjet Engines
2. E. T. Curran and S. N. B. Murthy, Scramjet Propulsion (American Institute of Astronautics and Aeronautics, Inc., Reston, VA, 2001).
3. Mixing and Combustion Studies Using Cavity-Based Flameholders in a Supersonic Flow
4. A. V. Starov and M. A. Goldfeld, “Hydrogen Injection Scheme Influence on Flow Structure in Supersonic Combustor of Constant Cross-Section” in XXV Conference on High-Energy Processes in Condensed Matter (HEPCM), AIP Conference Proceedings 1893, edited by V. M. Fomin (American Institute of Physics, Melville, NY, 2017), pp. 030157.
5. M. A. Goldfeld, A. A. Maslov, A. V. Starov, V. V. Shumskii and M. I. Yaroslavtsev, “IT-302M Hotshot Wind Tunnel as a Tool for the Development of Hypersonic Technologies,” in 18th International Conference on the Methods of Aerophysical Research, AIP Conference Proceedings 1770, edited by V. M. Fomin (American Institute of Physics, Melville, NY, 2016), pp. 030020.
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