Effects of Additional Cavity Floor Injection on the Ignition and Combustion Processes in a Mach 2 Supersonic Flow
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- Tao Cui & Yang Ou, 2019. "Modeling of Scramjet Combustors Based on Model Migration and Process Similarity," Energies, MDPI, vol. 12(13), pages 1-12, June.
- Stephen M. Neill & Apostolos Pesyridis, 2017. "Modeling of Supersonic Combustion Systems for Sustained Hypersonic Flight," Energies, MDPI, vol. 10(11), pages 1-22, November.
- Chae-Hyoung Kim & In-Seuck Jeung, 2019. "Forced Combustion Characteristics Related to Different Injection Locations in Unheated Supersonic Flow," Energies, MDPI, vol. 12(9), pages 1-13, May.
- Devendra Sen & Apostolos Pesyridis & Andrew Lenton, 2018. "A Scramjet Compression System for Hypersonic Air Transportation Vehicle Combined Cycle Engines," Energies, MDPI, vol. 11(6), pages 1-32, June.
- Chaolong Li & Zhixun Xia & Likun Ma & Xiang Zhao & Binbin Chen, 2019. "Numerical Study on the Solid Fuel Rocket Scramjet Combustor with Cavity," Energies, MDPI, vol. 12(7), pages 1-17, March.
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Cited by:
- Byeong-Jo Hwang & Seongki Min, 2023. "Numerical Investigation of the Effect of Supersonic Air Temperature on the Mixing Characteristics of Liquid Fuel," Energies, MDPI, vol. 16(1), pages 1-17, January.
- Wenxiong Xi & Mengyao Xu & Chaoyang Liu & Jian Liu & Bengt Sunden, 2022. "Generation and Propagation Characteristics of an Auto-Ignition Flame Kernel Caused by the Oblique Shock in a Supersonic Flow Regime," Energies, MDPI, vol. 15(9), pages 1-14, May.
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Keywords
injection scheme; cavity floor injection; ignition; flame stabilization;All these keywords.
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