Survey on the mode transition technique in combined cycle propulsion systems

Bao, 2013, Combustion characteristic using O2-pilot strut in a liquid-kerosene-fueled strut-based dual-mode scramjet, Proc. Inst. Mech. Eng., Part G J. Aerosp. Eng., 227, 1870, 10.1177/0954410012464455

Bao, 2013, Dynamic characteristics of combustion mode transitions in a strut-based scramjet combustor model, J. Propuls. Power, 29, 1244, 10.2514/1.B34921

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

M.J. Bulman, A. Siebenhaar, Combined cycle propulsion: aerojet innovations for practical hypersonic vehicles, in: 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, San Francisco, California, 2011, AIAA Paper 2011-2397.

Cao, 2013, Analysis of combustion mode and operating route for hydrogen fueled scramjet engine, Int. J. Hydrog. Energy, 38, 5928, 10.1016/j.ijhydene.2013.02.135

Chen, 2007, Mode transition study of turbine based combined cycle engine concepts

Chen, 2009, Goal programming for stable mode transition in tandem turbo–ramjet engines, Chin. J. Aeronaut., 22, 486, 10.1016/S1000-9361(08)60130-2

Csank, 2012, A turbine based combined cycle engine inlet model and mode transition simulation based on HiTECC tool

Cui, 2008, Distributed parameter control arithmetic for an axisymmetrical dual-mode scramjet, Aeronaut. J., 112, 557, 10.1017/S0001924000002517

Cui, 2008, Topological geometry interpretation of supersonic inlet start/unstart based on catastrophe theory, J. Aircr., 45, 1464, 10.2514/1.34125

Cui, 2009, Catastrophe model for supersonic inlet start/unstart, J. Aircr., 46, 1160, 10.2514/1.38926

Cui, 2012, Hysteresis phenomenon of mode transition in ramjet engines and its topological rule, J. Propuls. Power, 28, 1277, 10.2514/1.B34419

Etele, 2007, Analysis of increased compression through area constriction on ejector-rocket performance, J. Spacecr. Rockets, 44, 355, 10.2514/1.26915

Foster, 2012, Highlights from a Mach 4 experimental demonstration of inlet mode transition for turbine-based combined cycle hypersonic propulsion

Fotia, 2012, Experimental investigation of ram/scram-mode transition mechanics

Fotia, 2013, Ram-scram transition and flame/shock–train interactions in a model scramjet experiment, J. Propuls. Power, 29, 261, 10.2514/1.B34486

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

Gamble, 2010, Thermal management and fuel system model for TBCC dynamic simulation

Ghosh, 2010, Simulation of shock/boundary–layer interactions with bleed using immersed-boundary methods, J. Propuls. Power, 26, 203, 10.2514/1.45297

Goyne, 2007, Test gas vitiation effects in a dual-mode scramjet combustor, J. Propuls. Power, 23, 559, 10.2514/1.24663

Haftka, 1985, An analytical investigation of shape control of large space structures by applied temperatures, AIAA J., 23, 1

Huang, 2009, Analysis of mode transition with thrust smoothing of small turbine/ramjet combined cycle engine, J. Aerosp. Power, 24, 2756

Huang, 2010, Exploring mode transition with air mass flow smoothing of small turbine/ramjet engine (TRE), J. Northwestern Polytech. Univ., 28, 234

Huang, 2011, Numerical investigation on the shock wave transition in a three-dimensional scramjet isolator, Acta Astronaut., 68, 1669, 10.1016/j.actaastro.2010.12.011

Huang, 2012, Influences of H2O mass fraction and chemical kinetics mechanism on the turbulent diffusion combustion of H2–O2 in supersonic flows, Acta Astronaut., 76, 51, 10.1016/j.actaastro.2012.02.017

Huang, 2012, Flow-field analysis of a typical hydrogen-fueled dual-mode scramjet combustor, J. Aerosp. Eng., 25, 336, 10.1061/(ASCE)AS.1943-5525.0000136

Huang, 2012, Flow-field analysis of a typical hydrogen-fueled dual-mode scramjet combustor, J. Aerosp. Eng., 25, 336, 10.1061/(ASCE)AS.1943-5525.0000136

Huang, 2014, Variation of inlet boundary conditions on the combustion characteristics of a typical cavity-based scramjet combustor, Proc. Inst. Mech. Eng., Part G J. Aerosp. Eng., 228, 627, 10.1177/0954410013480076

Jahingir, 2005, Design optimization of rocket-based combined-cycle inlet/ejector system, J. Propuls. Power, 21, 650, 10.2514/1.10788

Kanda, 2007, Conceptual study of a rocket-ramjet combined-cycle engine for an aerospace plane, J. Propuls. Power, 23, 301, 10.2514/1.22899

Ketsdever, 2010, Overview of advanced concepts for space access, J. Spacecr. Rockets, 47, 238, 10.2514/1.46148

Le, 2012, A framework for simulating turbine-based combined-cycle inlet mode-transition

Li, 2009, Numerical study of the unsteady mode transition process of an over-under TBCC exhaust system

Li, 2014, Experimental investigation of vitiation on effects on supersonic combustor performance, Acta Astronaut., 96, 296, 10.1016/j.actaastro.2013.11.016

Liu, 2009, Present situation and progress of investigation on rocket based combined cycle (RBCC) propulsion system, J. Solid Rocket Technol., 32, 288

Liu, 2009, Selection of ejector–ramjet mode transition interval on RBCC, J. Solid Rocket Techn., 32, 500

Liu, 2009, Numerical simulation for operation process of ejector/ramjet mode transition of RBCC, J. Propuls. Technol., 30, 641

Liu, 2009, Numerical simulation of performance for turbine based combined cycle propulsion system, J. Propuls. Technol., 30, 1

Marshall, 2004, Critical issues in TBCC modeling

Masatoshi, 2003, Mach 6 test of a scramjet engine with boundary-layer bleeding and two-staged fuel injection

Masumoto, 2010, Experimental study on effect of boundary layer on combustion modes in a supersonic combustor

Masumoto, 2011, Experimental study on combustion modes in a supersonic combustor, J. Propuls. Power, 27, 346, 10.2514/1.B34020

McDaniel, 2009, US national center for hypersonic combined cycle propulsion: an overview

Mercurio, 2010, Experimental studies of the unsteady ejector mode of a pulse detonation rocket-based combined cycle engine

Micka, 2009, Combustion characteristics of a dual-mode scramjet combustor with cavity flameholder, Proc. Combust. Inst., 32, 2397, 10.1016/j.proci.2008.06.192

Noda, 2011, Estimation of enthalpy effects in direct-connect dual-mode combustor, J. Therm. Sci. Technol., 6, 289, 10.1299/jtst.6.289

Noda, 2012, Quasi-one dimensional modeling on vitiation effects for a dual-mode combustor

Pastrone, 2009, Multi-objective optimization of rocket-based combined-cycle engine performance using a hybrid evolutionary algorithm, J. Propuls. Power, 25, 1140, 10.2514/1.41327

Qin, 2010, Research status and perspective of rocket based combined cycle propulsion system, J. Propuls. Technol., 31, 660

Rockwell, 2011, Experimental study of test-medium vitiation effects on dual-mode scramjet performance, J. Propuls. Power, 27, 1135, 10.2514/1.B34180

Shapiro, 1953

Steffen, 2002

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

Torrez, 2013, New method for computing performance of choked reacting flows and ram-to-scram transition, J. Propuls. Power, 29, 433, 10.2514/1.B34496

Turner, 2013, Mode change characteristics of a three-dimensional scramjet at Mach 8, J. Propuls. Power, 29, 982, 10.2514/1.B34569

Vyas, 2010

Wang, 2003, Research status about rocket based combined cycle (RBCC) propulsion system, J. Solid Rocket Techn., 26, 1

Wang, 2007, Numerical research on subsonic-combustion and supersonic-combustion modes in scramjet chamber, J. Solid Rocket Techn., 30, 26

Wang, 2014, Review of cavity-stabilized combustion for scramjet applications, Proc. Inst. Mech. Eng., Part G J. Aerosp. Eng., 10.1177/0954410014521172

Yu, 2009, Catastrophe hysteresis and bifurcation of mode transition in scramjet engines and its model, Sci. China Ser. E Technol. Sci., 52, 1543, 10.1007/s11431-009-0181-6