Effect of transverse fuel injection system on combustion efficiency in scramjet combustor
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DOI: 10.1016/j.energy.2020.119511
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- Li, Jianping & Liao, Zilong & Jiao, Guiqian & Song, Wenyan, 2019. "The mode transition characteristics in a dual-mode combustor at different total temperatures," Energy, Elsevier, vol. 188(C).
- Zhang, Duo & Yang, Shengbo & Zhang, Silong & Qin, Jiang & Bao, Wen, 2015. "Thermodynamic analysis on optimum performance of scramjet engine at high Mach numbers," Energy, Elsevier, vol. 90(P1), pages 1046-1054.
- Qin, Jiang & Cheng, Kunlin & Zhang, Silong & Zhang, Duo & Bao, Wen & Han, Jiecai, 2016. "Analysis of energy cascade utilization in a chemically recuperated scramjet with indirect combustion," Energy, Elsevier, vol. 114(C), pages 1100-1106.
- Yu, Xuanfei & Wang, Cong & Yu, Daren, 2019. "Thermodynamic assessment on performance extremes of the fuel indirect precooled cycle for hypersonic airbreathing propulsion," Energy, Elsevier, vol. 186(C).
- Li, Xiaojie & Huang, Xiaobin & Liu, Hong & Du, Jianke, 2020. "Fuel reactivity controlled self-starting and propulsion performance of a scramjet: A model investigation," Energy, Elsevier, vol. 195(C).
- Du, Zhao-bo & Huang, Wei & Yan, Li, 2019. "Parametric study on mixing augmentation mechanism induced by air injection in a shock-induced combustion ramjet engine," Energy, Elsevier, vol. 186(C).
- Yang, Qingchun & Chang, Juntao & Bao, Wen, 2014. "Thermodynamic analysis on specific thrust of the hydrocarbon fueled scramjet," Energy, Elsevier, vol. 76(C), pages 552-558.
- Zhang, Tiantian & Wang, Zhenguo & Huang, Wei & Ingham, Derek & Ma, Lin & Porkashanian, Mohamed, 2020. "An analysis tool of the rocket-based combined cycle engine and its application in the two-stage-to-orbit mission," Energy, Elsevier, vol. 193(C).
- Li, Jianping & Li, Jindong & Wang, Kai & Jiao, Guiqian & Liao, Zilong, 2020. "Study of low-temperature ignition characteristics in a supersonic combustor," Energy, Elsevier, vol. 195(C).
- Feng, Yu & Liu, Yuna & Cao, Yong & Gong, Keyu & Liu, Shuyuan & Qin, Jiang, 2020. "Thermal management evaluation for advanced aero-engines using catalytic steam reforming of hydrocarbon fuels," Energy, Elsevier, vol. 193(C).
- Xiong, Yuefei & Qin, Jiang & Cheng, Kunlin & Wang, Youyin, 2020. "Influence of water injection on performance of scramjet engine," Energy, Elsevier, vol. 201(C).
- Li, Zhixiong & Manh, Tran Dinh & Barzegar Gerdroodbary, Mostafa & Nam, Nguyen Dang & Moradi, R. & Babazadeh, Houman, 2020. "The effect of sinusoidal wall on hydrogen jet mixing rate considering supersonic flow," Energy, Elsevier, vol. 193(C).
- He, Yubao & Cao, Ruifeng & Huang, Hongyan & Qin, Jiang & Yu, Daren, 2017. "Overall performance assessment for scramjet with boundary-layer ejection control based on thermodynamics," Energy, Elsevier, vol. 121(C), pages 318-330.
- Amati, V. & Bruno, C. & Simone, D. & Sciubba, E., 2008. "Exergy analysis of hypersonic propulsion systems: Performance comparison of two different scramjet configurations at cruise conditions," Energy, Elsevier, vol. 33(2), pages 116-129.
- Yan, Li & Liao, Lei & Meng, Yu-shan & Li, Shi-bin & Huang, Wei, 2020. "Investigation on the mode transition of a typical three-dimensional scramjet combustor equipped with a strut," Energy, Elsevier, vol. 208(C).
- Peng, Yeping & Barzegar Gerdroodbary, M. & Sheikholeslami, M. & Shafee, Ahmad & Babazadeh, Houman & Moradi, R., 2020. "Mixing enhancement of the multi hydrogen fuel jets by the backward step," Energy, Elsevier, vol. 203(C).
- Seyedmatin, Pourya & Karimian, Saeed & Rostamzadeh, Hadi & Amidpour, Majid, 2020. "Electricity and hydrogen co-production via scramjet multi-expansion open cooling cycle coupled with a PEM electrolyzer," Energy, Elsevier, vol. 199(C).
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Cited by:
- Feng, Yanbin & Luo, Shibin & Song, Jiawen & Xu, Dequan, 2023. "Numerical investigation on flow and mixing characteristics of powder fuel under strong shear and shock wave interaction," Energy, Elsevier, vol. 263(PE).
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Keywords
Parallel injection; Transverse injection; Wedge shaped strut; Reacting flow; Hydrogen;All these keywords.
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