Effect of variation of angle of attack on the performance of two-strut scramjet combustor

Scramjet combustor development Dr. Satish Kumar & Team Head, Hypersonic Propulsion Division & Dy. Project Director, HSTDV, DRDL, Hyderabad. Cecere, 2011, Hydrogen/air supersonic combustion for future hypersonic vehicles, Int J Hydrogen Energy, 36, 11969, 10.1016/j.ijhydene.2011.06.051 Pandey, 2015, Computational analysis of hypersonic combustor using strut injector at flight mach 7, Combust Sci Technol, 187, 1392, 10.1080/00102202.2015.1035371 Pandey, 2011, CFD analysis of mixing and combustion of a scramjet combustor with a planer strut injector, Int J Environ Sci Dev, 2, 102, 10.7763/IJESD.2011.V2.105 Pandey, 2011, CFD analysis of hydrogen fuelled mixture in scramjet combustor with a strut injector by using fluent software, Int J Eng Technol, 3, 109, 10.7763/IJET.2011.V3.208 Kumaran, 2009, Investigation of the effect of chemistry models on the numerical predictions of the supersonic combustion of hydrogen, Combust Flame, 156, 826, 10.1016/j.combustflame.2009.01.008 Waidmann, 1994, Experimental investigation of hydrogen combustion process in a supersonic combustion ramjet (SCRAMJET)” DGLR, Jahrestag Erlangen, Ger, 629 Waidmann, 1995, Supersonic combustion of hydrogen/air in a scramjet combustion chamber, Space Technol, 15, 421, 10.1016/0892-9270(95)00017-8 Waidmann, 1996, Experimental investigation of supersonic ramjet combustion (Scramjet) Brown, 1974, On density effects and large structure in turbulent mixing layers, J Fluid Mech, 64, 775, 10.1017/S002211207400190X Reinartz, 2003, Aerodynamic performance analysis of a hypersonic inlet isolator using computation and experiment, J Propuls Power, 19, 868, 10.2514/2.6177 Huang, 2015, Investigation on the effect of strut configurations and locations on the combustion performance of a typical scramjet combustor, J Mech Sci Technol, 29, 5485, 10.1007/s12206-015-1150-6 Huang, 2016, Numerical investigation on the ram-scram transition mechanism in a strut-based dual-mode scramjet combustor, Int J hydrogen energy, 41, 4799, 10.1016/j.ijhydene.2016.01.062 Fureby, 2015, A computational study of supersonic combustion in strut injector and hyper mixer flow fields, Proc Combust Inst, 35, 2127, 10.1016/j.proci.2014.06.113 Huang, 2012, Investigation on high angle of attack characteristics of hypersonic space vehicle, Sci China Technol Sci, 55, 1437, 10.1007/s11431-012-4760-6 Huang, 2011, Parametric effects on the combustion flow field of a typical strut-based scramjet combustor, Chin Sci Bull, 56, 3871, 10.1007/s11434-011-4823-2 Deepu, 2007, Recent advances in experimental and numerical analysis of scramjet combustor flow fields, Inst Eng India (IE-I), 88, 13 Pandey, 2010, Recent advances in scramjet fuel injection – a review, Int J Chem Eng Appl, 1, 294 Santana, 2012 ANSYS, 2011 Ferziger, 2002 Menter, 1994, Two-equation eddy-viscosity turbulence models for engineering applications, AIAA J, 32, 1598, 10.2514/3.12149 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 Tu, 2008 Oevermann, 2000, Numerical investigation of turbulent hydrogen combustion in a scramjet using flamelet modelling, Aerosp Sci Technol, 4, 463, 10.1016/S1270-9638(00)01070-1 Gerlinger, 2008, Numerical investigation of mixing and combustion enhancement in supersonic combustors by strut induced stream wise vorticity, Aerosp Sci Technol, 12, 159, 10.1016/j.ast.2007.04.003 Rajasekaran, 2006, Numerical simulation of three-dimensional reacting flow in a model supersonic combustor, J Propuls Power, 22, 820, 10.2514/1.14952 Huang, 2010, Research status about key techniques of shock-induced combustion ramjet (scramjet) engine, Sci China Technol Sci, 53, 220, 10.1007/s11431-009-0379-7 Huang, 2012, Effect of geometric parameters on the drag of the cavity flameholder based on the variance analysis method, Aerosp Sci Technol, 21, 24, 10.1016/j.ast.2011.04.009 Huang, 2013, Performance evaluation and parametric analysis on cantilevered ramp injector in supersonic flows, Acta Astronaut, 84, 141, 10.1016/j.actaastro.2012.11.011 Fureby, 2014, A computational study of supersonic combustion behind a wedge-shaped flameholder, Shock Waves, 24, 41, 10.1007/s00193-013-0459-2 Genin, 2010, Simulation of turbulent mixing behind a strut injector in supersonic flow, AIAA J, 48, 526, 10.2514/1.43647 Potturi, 2014, Hybrid large-eddy/reynolds-averaged Navier–Stokes simulations of flow through a model scramjet, AIAA J, 52, 1417, 10.2514/1.J052595