An analysis tool of the rocket-based combined cycle engine and its application in the two-stage-to-orbit mission
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Tiantian Zhang | Zhenguo Wang | Lin Ma | Huang Wei | Derek B. Ingham | Mohamed Porkashanian | Huang Wei | Zhenguo Wang | D. Ingham | Lin Ma | Tian-tian Zhang | Mohamed Porkashanian
[1] Martin Sippel,et al. Evolution of the SpaceLiner towards a Reusable TSTO-Launcher , 2016 .
[2] Zhenguo Wang,et al. Thermodynamic efficiency analysis and cycle optimization of deeply precooled combined cycle engine in the air-breathing mode , 2017 .
[3] William J. D. Escher,et al. A retrospective on early cryogenic primary rocket subsystem designs as integrated into rocket-based combined-cycle (RBCC) engines , 1993 .
[4] John Edward Bradford,et al. SCCREAM v.5: A Web-Based Airbreathing Propulsion Analysis Tool , 1999 .
[5] Kouichiro Tani,et al. Conceptual Study of a Rocket-Ramjet Combined-Cycle Engine for an Aerospace Plane , 2007 .
[6] Richard E. Brown,et al. Hybrid propulsion parametric and modular model : a novel engine analysis tool conceived for design optimization , 2014 .
[7] Hideo Ikawa,et al. Rapid methodology for design and performance prediction of integrated supersonic combustion ramjet engine , 1991 .
[8] Daren Yu,et al. Investigation of performance and mode transition in a variable divergence ratio dual-mode combustor , 2018, Aerospace Science and Technology.
[9] Wen Bao,et al. Maximum thrust for the rocket-ejector mode of the hydrogen fueled rocket-based combined cycle engine , 2015 .
[10] John Edward Bradford,et al. SCCREAM (Simulated Combined-Cycle Rocket Engine Analysis Module): A Conceptual RBCC Engine Design Tool , 1997 .
[11] Wei Huang,et al. The overall layout of rocket-based combined-cycle engines: a review , 2019, Journal of Zhejiang University-SCIENCE A.
[12] Jiang Qin,et al. Thermodynamic analysis on optimum performance of scramjet engine at high Mach numbers , 2015 .
[13] Zhiwen Wu,et al. Numerical and Experimental Study on the Solid-Fuel Scramjet Combustor , 2015 .
[14] Wenya Song,et al. Effect of Truncation on the Performance of Busemann Inlet , 2009 .
[15] Qingjun Zhao,et al. Performance analysis of a pre-cooled and fuel-rich pre-burned mixed-flow turbofan cycle for high speed vehicles , 2018, Energy.
[16] E. T. Curran,et al. Scramjet Engines: The First Forty Years , 2001 .
[17] Enrico Sciubba,et al. Exergy analysis of hypersonic propulsion systems: Performance comparison of two different scramjet configurations at cruise conditions , 2008 .
[18] Zun Cai,et al. Survey on key techniques of rocket-based combined-cycle engine in ejector mode , 2019, Acta Astronautica.
[19] Wang Yajun,et al. Study of thermal throat of RBCC combustor based on one-dimensional analysis , 2015 .
[20] Jie Liu,et al. A rocket-based combined-cycle engine prototype demonstrating comprehensive component compatibility and effective mode transition , 2016 .
[21] Li Yan,et al. Flame propagation and stabilization in dual-mode scramjet combustors: A survey , 2018, Progress in Aerospace Sciences.
[22] Hosung Lee,et al. Application of a New Economic Analysis Tool to a Two-Stage-to-Orbit RBCC Launch Vehicle Design , 1996 .
[23] Takeshi Kanda,et al. Experimental Study of a Combined-Cycle Engine Combustor in Ejector-Jet Mode , 2007 .
[24] Alessandro Mogavero. Toward automated design of Combined Cycle Propulsion , 2016 .
[25] Sadatake Tomioka,et al. Design of Sub-Scale Rocket-Ramjet Combined Cycle Engine Model , 2005 .
[26] Fei Qin,et al. Research progress on ejector mode of rocket-based combined-cycle engines , 2019, Progress in Aerospace Sciences.
[28] George Culver,et al. Performance Comparison of RBCC- and TBCC-based Reusable Launch Vehicles with Enhancing Technologies , 2003 .
[29] Anthony Castrogiovanni,et al. X-43A Vehicle Design and Manufacture , 2005 .
[30] Kenji Kudo,et al. A Conceptual Study of a Combined Cycle Engine for an Aerospace Plane , 2002 .
[31] David B. Doman,et al. Nonlinear Longitudinal Dynamical Model of an Air-Breathing Hypersonic Vehicle , 2007 .
[32] Johan Steelant,et al. Hexafly-INT Experimental Flight Test Vehicle (EFTV) Aero-Thermal Design , 2017 .
[33] Fei Qin,et al. Effects of Fuel-lean Primary Rocket on Bypass Ratio in RBCC Ejector Mode , 2014 .
[34] Xu Xu,et al. Effect of thermal choking on ejection process in a rocket-based combined cycle engine , 2017 .
[35] Daren Yu,et al. Thermodynamic assessment on performance extremes of the fuel indirect precooled cycle for hypersonic airbreathing propulsion , 2019, Energy.
[36] Ye Wei,et al. Climbing performance analysis of rocket-based combined cycle engine powered aircraft , 2019, Acta Astronautica.
[37] Sam Han,et al. Ejector Primary Flow Molecular Weight Effects in an Ejector -Ram Rocket Engine , 2002 .
[38] Guoqiang He,et al. Effect of the heat release on the component coordination in the rocket-based combined cycle engine , 2018, Acta Astronautica.
[39] Xianggeng Wei,et al. Experimental study on combustion modes of a liquid kerosene fueled RBCC combustor , 2017 .
[40] Takeshi Tsuchiya,et al. Multi-Objective, Multidisciplinary Design Optimization of TSTO Space Planes with RBCC Engines , 2015 .
[41] E. T. Curran,et al. Low-Speed Operation Of An Integrated Rocket-Ram-Scramjet For A Transatmospheric Accelerator , 1996 .
[42] John R. Olds,et al. Improvements and Enhancements to SCCREAM, A Conceptual RBCC Engine Analysis Tool , 1998 .
[44] Catherine Bahm,et al. Overview With Results and Lessons Learned of the X-43A Mach 10 Flight , 2005 .
[45] Sadatake Tomioka,et al. Multi-objective design and trajectory optimization of space transport systems with RBCC propulsion via evolutionary algorithms and pseudospectral methods , 2014 .
[46] Lei Shi,et al. Rocket-Based Combined-Cycle Inlet Researches in Northwestern Polytechnical University , 2018, 2018 9th International Conference on Mechanical and Aerospace Engineering (ICMAE).
[47] Sejong Oh,et al. Quasi-1D analysis and performance estimation of a sub-scale RBCC engine with chemical equilibrium , 2017 .
[48] Richard Foster. Optimization of the rocket mode trajectory in a rocket based combined cycle (RBCC) engine powered SSTO vehicle , 1989 .
[49] Marc A. Brock. Performance Study of Two-Stage-to-Orbit Reusable Launch Vehicle Propulsion Alternatives , 2012 .
[50] Sejong Oh,et al. A Preliminary Design of Flight Test Conditions for a Sub-scale RBCC Engine using a Sounding Rocket , 2015 .
[51] J. Anderson,et al. Fundamentals of Aerodynamics , 1984 .
[52] Li Yan,et al. Survey on the mode transition technique in combined cycle propulsion systems , 2014 .
[53] Juntao Chang,et al. Thermodynamic analysis on specific thrust of the hydrocarbon fueled scramjet , 2014 .
[54] Richard E. Brown,et al. An improved engine analysis and optimization tool fo hypersonic combined cycle engines , 2015 .
[55] S. Molder,et al. Hypersonic wavecatcher intakes and variable-geometry turbine based combined cycle engines , 2019, Progress in Aerospace Sciences.
[56] Wei Huang,et al. A design approach of wide-speed-range vehicles based on the cone-derived theory , 2017 .