Effect of the heat release on ejector-to-ramjet dynamic mode transition process in the rocket-based combined cycle engine

Yupeng Hu1, Yuan-Shu Liu2, Yijun Wang1, Ben-Quan Zhou1, Xing Zheng3, Rui Xue2
1Institute of systems Engineering, China Academy of Engineering Physics, Mianyang 621999, China
2State Key Laboratory for Strength and Vibration of Mechanical Structures, Shaanxi Engineering Laboratory for Vibration Control of Aerospace Structures, School of Aerospace, Xi'an Jiaotong University, 710049, Xi'an, China
3College of aircraft, Xi'an aeronautical institute, 710077 Xi'an, China

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Tài liệu tham khảo

Chojnacki, 1993, An assessment of the rocket-based combined cycle propulsion system for earth-to-orbit transportation

Siebenhaar, 1995, The Strutjet engine: The overlooked option for space launch

Bertin, 2003, Fifty years of hypersonics: where we’ve been, where we’re going, Prog. Aerosp. Sci., 39, 511, 10.1016/S0376-0421(03)00079-4

Fry, 2004, A century of ramjet propulsion technology evolution, J. Propuls. Power, 20, 27, 10.2514/1.9178

Klink, 2019, Investigation on the performance and feasibility of RBCC-based access-to space via multi-objective design optimization, Acta Astronaut., 157, 435, 10.1016/j.actaastro.2018.12.034

Bulman, 2011

Weir, 2022

Seddon, 1985

Tani, 2008, Ram and ejector–jet mode experiments of the combined cycle engine in Mach 4 flight conditions[C]

Zhang, 2018, Investigation of performance and mode transition in a variable divergence ratio dual-mode combustor, Aerosp. Sci. Technol., 80, 496, 10.1016/j.ast.2018.07.025

Hao, 2016, A model of mode transition logic in dual-mode scramjet engines, Aerosp. Sci. Technol., 49, 173, 10.1016/j.ast.2015.12.001

Yang, 2014, A mechanism of combustion mode transition for hydrogen fueled scramjet, Int. J. Hydrog. Energy, 39, 9791, 10.1016/j.ijhydene.2014.04.090

McConnaughey, 2012

Shi, 2020, Experimental study on ejector-to-ramjet mode transition in a divergent kerosene-fueled RBCC combustor with low total temperature inflow, Aerosp. Sci. Technol., 99, 105734, 10.1016/j.ast.2020.105734

Daines, 2022

Byrne, 2000, Analysis of transient thermal choking processes in a model scramjet engine, J. Propuls. Power, 16, 808, 10.2514/2.5645

Riggins, 2006, Thermodynamic analysis of dual-mode scramjet engine operation and performance, AIAA Pap., 2006

Huang, 2018, Supersonic mixing in airbreathing propulsion systems for hypersonic flights, Prog. Aerosp. Sci., 50, 593

Fallah, 2018, The influence of micro air jets on mixing augmentation of fuel in cavity flameholder at supersonic flow, Aerosp. Sci. Technol., 79, 187, 10.1016/j.ast.2018.01.021

Li, 2019, Experimental investigation on upstream fuel injection technique of RBCC scramjet mode, Appl. Therm. Eng., 154, 450, 10.1016/j.applthermaleng.2019.03.097

Chang, 2017, Recent research progress on unstart mechanism, detection and control of hypersonic inlet, Prog. Aerosp. Sci., 89, 1, 10.1016/j.paerosci.2016.12.001

Wang, 2015, Study of thermal throat of RBCC based on one-dimensional analysis, Acta Astronaut., 117, 130, 10.1016/j.actaastro.2015.07.034

D.K. Yan, X. Liu, Y.J. Wang, L. Shi, F. Qin, G.Q. He, R.J. Martinuzzi, Effect of area ratio and heat release method on the Ma∞ = 2-6 operation performance of rocket-based combined cycle engine, Aerosp. Sci. Technol.,Volume 126,2022,107617,ISSN 1270–9638.

Doster, 2008

Fluent Inc, 2010

Barik, 2015, Heat transfer enhancement from a small rectangular channel with different surface protrusions by a turbulent cross flow jet, Int. J. Therm. Sci., 98, 35, 10.1016/j.ijthermalsci.2015.07.003

Cai, 2016, Numerical and experimental analysis of heat transfer in injector plate of hydrogen peroxide hybrid rocket motor, Acta Astronaut., 128, 286, 10.1016/j.actaastro.2016.05.041

Westbrook, 1981, Simplified reaction mechanisms for the oxidation of hydrocarbon fuels in flames, Combust. Sci. Technol., 27, 31, 10.1080/00102208108946970

Lin, 2014

Wei, 2017, Research on shock wave characteristics in the isolator of central strut rocket-based combined cycle engine under Ma5.5, Acta Astronaut., 140, 284, 10.1016/j.actaastro.2017.08.013

Yan, 2018, Effect of the heat release on the component coordination in the rocket-based combined cycle engine, Acta Astronaut., 151, 942, 10.1016/j.actaastro.2018.04.051

Wang, 2017, Effect of thermal choking on ejection process in a rocket-based combined cycle engine, Appl. Therm. Eng., 116, 197, 10.1016/j.applthermaleng.2017.01.059