Investigation of performance and mode transition in a variable divergence ratio dual-mode combustor

Liu, 2017, Experimental and numerical investigation of smooth turbine-based combined-cycle inlet mode transition, Aerosp. Sci. Technol., 60, 124, 10.1016/j.ast.2016.11.005

Kodera, 2014

Savino, 2015, Performances of a small hypersonic airplane (HyPlane), Acta Astronaut., 115, 338, 10.1016/j.actaastro.2015.06.006

Zuo, 2016, Investigation of internal-waverider-inlet flow pattern integrated with variable-geometry for TBCC, Aerosp. Sci. Technol., 59, 69, 10.1016/j.ast.2016.10.009

Bizzarri, 2008, Propulsion vehicle integration for reusable launcher using in-flight oxygen collection, Aerosp. Sci. Technol., 12, 429, 10.1016/j.ast.2007.10.012

Fernández, 2014, Installed performance evaluation of an air turbo-rocket expander engine, Aerosp. Sci. Technol., 35, 63, 10.1016/j.ast.2014.03.005

Huang, 2016, Combustion oscillation study in a kerosene fueled rocket-based combined-cycle engine combustor, Acta Astronaut., 129, 260, 10.1016/j.actaastro.2016.09.024

Huang, 2016, Large eddy simulation of combustion characteristics in a kerosene fueled rocket-based combined-cycle engine combustor, Acta Astronaut., 127, 326, 10.1016/j.actaastro.2016.06.016

Huang, 2014, Survey on the mode transition technique in combined cycle propulsion systems, Aerosp. Sci. Technol., 39, 685, 10.1016/j.ast.2014.07.006

Zhang, 2018, Effect of Mach number and equivalence ratio on the pressure rising variation during combustion mode transition in a dual-mode combustor, Aerosp. Sci. Technol., 46, 516, 10.1016/j.ast.2017.11.042

Tian, 2015, Experimental and computational study on combustion performance of a kerosene fueled dual-mode scramjet engine, Aerosp. Sci. Technol., 46, 451, 10.1016/j.ast.2015.09.002

Kumar, 2014, Application of CFD and the Kriging method for optimizing the performance of a generic scramjet combustor, Acta Astronaut., 101, 111, 10.1016/j.actaastro.2014.04.003

Choubey, 2017, Effect of different strut + wall injection techniques on the performance of two-strut scramjet combustor, Int. J. Hydrog. Energy, 42, 13259, 10.1016/j.ijhydene.2017.04.024

Zhang, 2012, Combustion of vaporized kerosene in supersonic model combustors with dislocated dual cavities, J. Propuls. Power, 30, 1152, 10.2514/1.B35096

Sun, 2016, Experimental investigation on combustion performance of cavity-strut injection of supercritical kerosene in supersonic model combustor, Acta Astronaut., 127, 112, 10.1016/j.actaastro.2016.05.035

Wang, 2015, Fluid redistribution in the turbulent boundary layer under the microramp control, AIAA J., 53, 3777, 10.2514/1.J054074

Falempin, 2011

Bouchez, 2011

Avrashkov, 2010, Investigation of high-speed ramjet engines, Combust. Explos. Shock Waves, 46, 400, 10.1007/s10573-010-0054-0

Feng, 2017, Numerical studies for performance improvement of a variable geometry dual mode combustor by optimizing deflection angle, Aerosp. Sci. Technol., 68, 320, 10.1016/j.ast.2017.05.025

Feng, 2017, Experimental and numerical investigation on hysteresis characteristic and formation mechanism for a variable geometry dual-mode combustor, Aerosp. Sci. Technol., 67, 96, 10.1016/j.ast.2017.03.040

Feng, 2017, Numerical and experimental investigation of improving combustion performance of variable geometry dual-mode combustor, Aerosp. Sci. Technol., 64, 213, 10.1016/j.ast.2017.02.002

Wei, 2012, Study on integrated aeroramp injector/gas-pilot flame in a supersonic combustor, J. Propuls. Power, 28, 486, 10.2514/1.B34305

Zhang, 2017, Flow field characteristics analysis and combustion modes classification for a strut/cavity dual-mode combustor, Acta Astronaut., 137, 44, 10.1016/j.actaastro.2017.03.023

Huang, 2014, Molecular weight and injector configuration effects on the transverse injection flow field properties in supersonic flows, Acta Astronaut., 32, 94

Qin, 2014, Numerical investigation of the impact of asymmetric fuel injection on shock train characteristics, Acta Astronaut., 105, 66, 10.1016/j.actaastro.2014.08.025

Kumaran, 2010, Numerical investigation of the supersonic combustion of kerosene in a strut-based combustor, J. Propuls. Power, 26, 1084, 10.2514/1.46965

Huang, 2016, Numerical investigation on the ram-scram transition mechanism in a strut-based dual-mode scramjet combustor, Int. J. Hydrog. Energy, 41, 4799, 10.1016/j.ijhydene.2016.01.062

Huang, 2011, Effect of cavity location on combustion flow field of integrated hypersonic vehicle in near space, J. Vis., 14, 339, 10.1007/s12650-011-0100-3

Smirnov, 2015, Accumulation of errors in numerical simulations of chemically reacting gas dynamics, Acta Astronaut., 117, 338, 10.1016/j.actaastro.2015.08.013

Shapiro, 1953, 220

Curran, 2000, Scramjet Propulsion, vol. 189, 588

Van Driest, 2003, Turbulent boundary layer in compressible fluids, J. Propuls. Power, 40, 1012

Heiser, 1994, Hypersonic Airbreathing Propulsion, 339

Zhang, 2015, Nonlinear characteristics and detection of combustion modes for a hydrocarbon fueled scramjet, Acta Astronaut., 110, 89, 10.1016/j.actaastro.2014.11.023

Zhang, 2017, Effect of heat release on movement characteristics of shock train in an isolator, Acta Astronaut., 133, 185, 10.1016/j.actaastro.2017.01.031

Xiao, 2015, Experimental and numerical investigations of combustion mode transition in a direct-connect scramjet combustor, Aerosp. Sci. Technol., 46, 331, 10.1016/j.ast.2015.08.001