Influence of Incident Shocks on Flame Characteristics in the Strut-Equipped Supersonic Combustor
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Junlong Zhang | Libo Lin | W. Bao | Kai Yong
[1] Zhao-bo Du,et al. Hydrogen mixing augmentation mechanism induced by the vortex generator and oblique shock wave in a scramjet engine , 2022, International journal of hydrogen energy.
[2] Y. Egami,et al. Mechanism of supersonic mixing enhancement by a wall-mounted three-dimensional cavity , 2021 .
[3] Nan Li. Response of shock train to fluctuating angle of attack in a scramjet inlet-isolator , 2021, Acta Astronautica.
[4] R. Moradi,et al. Influence of backward-facing step on the mixing efficiency of multi microjets at supersonic flow , 2020 .
[5] Qiang Li,et al. Numerical and experimental investigation of the geometrical scale effect on a confined subsonic-supersonic shear layer , 2020 .
[6] K. Pandey,et al. Numerical investigation on implication of strut profile on combustion characteristics in a cavity based scramjet combustor , 2020 .
[7] Z. Xia,et al. Experimental and numerical study of solid rocket scramjet combustor equipped with combined cavity and strut device , 2019, Acta Astronautica.
[8] Wei Huang,et al. Supersonic mixing in airbreathing propulsion systems for hypersonic flights , 2019, Progress in Aerospace Sciences.
[9] Daren Yu,et al. Closed-loop control of shock train in inlet-isolator with incident shocks , 2019, Experimental Thermal and Fluid Science.
[10] Daren Yu,et al. Research progress on strut-equipped supersonic combustors for scramjet application , 2018, Progress in Aerospace Sciences.
[11] Zhenguo Wang,et al. Flame stabilization with a rear-wall-expansion cavity in a supersonic combustor , 2018, Acta Astronautica.
[12] Li Yan,et al. Flame propagation and stabilization in dual-mode scramjet combustors: A survey , 2018, Progress in Aerospace Sciences.
[13] Jun Li,et al. Experimental investigation on gliding arc discharge plasma ignition and flame stabilization in scramjet combustor , 2018, Aerospace Science and Technology.
[14] H. Ogawa,et al. Numerical analysis and design optimization of supersonic after-burning with strut fuel injectors for scramjet engines , 2018, Acta Astronautica.
[15] Jialing Le,et al. Study on the effects of thermal throat on flame stabilization in a kerosene fueled supersonic combustor , 2018, Energy Conversion and Management.
[16] Wei Huang,et al. Nonlinear process in the mode transition in typical strut-based and cavity-strut based scramjet combustors , 2018 .
[17] Daren Yu,et al. Periodic forcing of a shock train in a scramjet inlet-isolator at overspeed condition , 2018 .
[18] Wenya Song,et al. Experimental study of cone-struts and cavity flameholders in a kerosene-fueled round scramjet combustor , 2017 .
[19] Jialing Le,et al. Investigation of combustion process of a kerosene fueled combustor with air throttling , 2017 .
[20] Guangming Guo,et al. Numerical study of active flow control over a hypersonic backward-facing step using supersonic jet in near space , 2017 .
[21] Jialing Le,et al. Investigation of combustion and flame stabilization modes in a hydrogen fueled scramjet combustor , 2016 .
[22] Li Yan,et al. Numerical investigation on the ram–scram transition mechanism in a strut-based dual-mode scramjet combustor , 2016 .
[23] Jianwen Xing,et al. Experimental and computational study on combustion performance of a kerosene fueled dual-mode scramjet engine , 2015 .
[24] Daren Yu,et al. Switching control of thrust regulation and inlet unstart protection for scramjet engine based on Min strategy , 2015 .
[25] Li Yan,et al. Survey on the mode transition technique in combined cycle propulsion systems , 2014 .
[26] He-xia Huang,et al. Behavior of shock trains in a hypersonic inlet/isolator model with complex background waves , 2012 .
[27] Wright-Patterson Afb,et al. Shock Train Position Control in an Axisymmetric Scramjet Combustor Flowpath , 2012 .
[28] Jing Lei,et al. Numerical investigation on the shock wave transition in a three-dimensional scramjet isolator , 2011 .
[29] Srikant Srinivasan,et al. Large Eddy Simulation of Supersonic Combustion in a Cavity-Strut Flameholder , 2011 .
[30] Jian Li,et al. IGNITION TRANSIENT IN AN ETHYLENE FUELED SCRAMJET ENGINE WITH AIR THROTTLING , 2010 .
[31] R. A. Baurle,et al. The Art of Extracting One-Dimensional Flow Properties from Multi-Dimensional Data Sets , 2007 .
[32] E. R. V. Driest,et al. Turbulent Boundary Layer in Compressible Fluids , 2003 .
[33] E. T. Curran,et al. Scramjet Engines: The First Forty Years , 2001 .