Cavity-based flameholding for chemically-reacting supersonic flows

Progress in Aerospace Sciences - Tập 76 - Trang 24-41 - 2015
F.W. Barnes1, Corin Segal1
1Department of Mechanical and Aerospace Engineering, University of Florida, Gainesville, FL 32611, United States

Tóm tắt

Từ khóa


Tài liệu tham khảo

Allen, 2005

F.W. Barnes, Qiuya Tu, C. Segal, Mixing and mass exchange for cavities in supersonic flows 2014, in: Proceedings of 19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference Atlanta, GA.

R.C. Bauer, R. E. Dix, Engineering Model of Unsteady Flow in a Cavity, Calspan Corp./AEDC Operations, Arnold Engineering Development Center, TR-91-17, 1991.

R.A. Baurle, C.-J. Tam, S. Dasgupta, Analysis of unsteady cavity flows for scramjet applications, in: Proceedings of the 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Las Vegas, NV, AIAA Paper 2000-3617, 2000 .

Baurle, 2003, Hybrid simulation approach for cavity flows: blending, algorithm, and boundary treatment issues, AIAA J., 41, 1463, 10.2514/2.2129

Ben-Yakar, 2000

Bogdanoff, 1983, Compressibility effects in turbulent shear layers, AIAA J., 21, 926, 10.2514/3.60135

I. Bermejo-Moreno, J. Larsson, J. Bodart, R. Vicquelin, Wall-modeled large-eddy simulations of the HIFiRE-2 Scramjet, Center for Turbulence Research, Annual Research Briefs, 2013.

L.N. Cattafesta III, S. Garg, M.S. Kegerise, G.S. Jones, Experiments on compressible flow-induced cavity oscillations, in: Proceedings of the 29th AIAA, Fluid Dynamics Conference, AIAA Paper 98-2912, 1998.

J.-Y. Choi, F. Ma, V. Yang, Dynamics combustion characteristics in scramjet combustors with transverse fuel injection, in: Proceedings of the 41st AIAA/ASME/ASEE Joint Propulsion Conference and Exhibit, Tucson, AZ, AIAA Paper 2005-4428, 2005.

Chinzei, 1986, Spreading of two-stream supersonic turbulent mixing layers, Phys. Fluids, 29, 1345, 10.1063/1.865698

D.F. Cuesta, C. Segal, A. Goldman, P. Ortwerth, Effects of hydrogen and ethylene injection schemes in a supersonic airstream, in: Proceedings of the 12th International Space Planes and Hypersonic Systems Conference, AIAA Paper 2003-6913, 2003.

E.T. Curran, An investigation of flame stability in a coaxial dump combustor (Ph.D. dissertation), Department of Aeronautics and Astronautics, Air Force Institute of Technology, Wright-Patterson Air Force Base, OH, 1979.

D.L. Davis, Numerical analysis of two and three dimensional recessed flameholders for scramjet applications (Ph.D. dissertation), Department of Aeronautics and Astronautics, Air Force Institute of Technology, Wright-Patterson Air Force Base, OH, 1996.

Day, 1998, The structure of the compressible reacting mixing layer: insights from linear stability analysis, Phys. Fluids, 10, 993, 10.1063/1.869619

Dimotakis, 1991, Turbulent free shear layer mixing and combustion, 265

D.S. Dolling, S.W. Perng, Y.L. Leu, An Experimental Study of Passive Control of Hypersonic Cavity Flow Oscillations, Center for Aeromechanics Research, Department of Aerospace Engineering and Engineering Mechanics, The University of Texas at Austin, ARFL-SR-BL-TR-98, 1998.

Donbar, 2000, OH planar laser-induced fluorescence imaging in a hydrocarbon-fueled scramjet combustor, Proc. Combust. Inst., 28, 679, 10.1016/S0082-0784(00)80269-6

Donohue, 2014, Dual-mode scramjet flameholding operability measurements, J. Propuls. Power, 30, 592, 10.2514/1.B35016

Driscoll, 2005, Correlation and analysis of blowout limits of flames in high-speed airflows, J. Propuls. Power, 21, 1035, 10.2514/1.13329

Ebrahimi, 2012, Numerical simulation of injection strategies in a cavity-based supersonic combustor, J. Propuls. Power, 28, 991, 10.2514/1.B34512

S.G. Edens, P.I. King, M.R. Gruber, K.-Y. Hsu, Performance measurements of direct air injection in a cavity-based flameholder for a supersonic combustor, in: Proceedings of the 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Sacramento, CA, AIAA Paper 2006-4861, 2006.

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

Gharib, 1983

Gharib, 1987, The effect of flow oscillations on cavity drag, J. Fluid Mech., 177, 501, 10.1017/S002211208700106X

C.D. Ghodke, J.J. Choi, S. Srinivasan, S. Menon. Large eddy simulation of supersonic combustion in a cavity-strut flameholder, in: Proceedings of the 49th AIAA Aerospace Sciences Meeting and Exhibit, Orlando, FL, 2011.

P. Gokulakrishnan, S. Pal, M.S. Klassen, A.J. Hamer, R.J. Roby, O. Kozaka, S. Menon. Supersonic combustion simulation of cavity-stabilized hydrocarbon flames using ethylene reduced kinetic mechanism, in: Proceedings of the 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit Sacramento, CA, 2006.

M.A. Goldfeld, A.A. Mishunin, A.V. Starov, A.B. Mathur, Investigation of hydrocarbon fuels combustion in supersonic combustor, in: Proceedings of the 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Ft. Lauderdale, FL, AIAA Paper 2004-3487, 2004.

N.R. Grady, Hydroxyl tagging velocimetry in a supersonic flow over a ramped-wall cavity flameholder with an upstream strut (M.S. thesis), Department of Mechanical Engineering, Vanderbilt University, Nashville, TN, 2010.

Gruber, 2001, Fundamental studies of cavity-based flameholder concepts for supersonic combustors, J. Propuls. Power, 17, 146, 10.2514/2.5720

Gruber, 2004, Mixing and combustion studies using cavity-based flameholders in a supersonic flow, J. Propuls. Power, 20, 769, 10.2514/1.5360

M.R. Gruber, K. Jackson, J. Liu, Hydrocarbon-fueled scramjet combustor flowpath development for Mach 6–8 HIFiRE flight experiments, in: Proceedings of the JANNAF Joint Subcommittee Meeting, AFRL-RZ-WP-TP-2010-2243, 2008.

Hall, 1993, Experiments in non-reacting compressible shear layers, AIAA J., 31, 2247, 10.2514/3.11922

Hammack, 2013, High-repetition rate OH planar laser-induced fluorescence of a cavity flameholder, J. Propuls. Power, 29, 1248, 10.2514/1.B34756

H.H. Heller, D.B. Bliss, The Physical Mechanism of Flow Induced Pressure Fluctuations in Cavities and Concepts for their Suppression, AIAA Paper 75-491, 1975.

Heller, 1996, Cavity pressure oscillations: the generation mechanism visualized, J. Sound Vib., 196, 248, 10.1006/jsvi.1996.0480

Hermanson, 1985

Hermanson, 1989, Effects of heat release in a turbulent reacting shear layer, J. Fluid Mech., 159, 151

Hsu, 2010, Experimental study of cavity–strut combustion in supersonic flow, J. Propuls. Power, 26, 1237, 10.2514/1.45767

Jackson, 2015, Mach 6–8+ hydrocarbon-fueled scramjet flight experiment: the HIFiRE flight 2 project, J. Propuls. Power, 31, 36, 10.2514/1.B35350

Jeong, 2008, Investigation of supersonic combustion with angled injection in a cavity-based combustor, J. Propuls. Power, 24, 1258, 10.2514/1.36519

Kim, 2004, Numerical study on supersonic combustion with cavity-based fuel injection, Int. J. Heat Mass Transf., 47, 271, 10.1016/j.ijheatmasstransfer.2003.07.004

Lahr, 2010, Hydroxyl-tagging-velocimetry measurements of a supersonic flow over a cavity, J. Propuls. Power, 26, 790, 10.2514/1.47264

Li, 2014, Ignition transients in a scramjet engine with air throttling Part 1: nonreacting flow, J. Propuls. Power, 30, 438, 10.2514/1.B34763

K.-C. Lin, C.-J. Tam, I. Boxx, C. Carter, K. Jackson, M. Lindsey, Flame characteristics and fuel entrainment inside a cavity flame holder in a scramjet combustor, in: Proceedings of the 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Cincinnati, OH, AIAA Paper 2007-5382, 2007

K.-C. Lin, C.-J. Tam, K. Jackson, Study on the operability of cavity flameholders inside a scramjet combustor, in: Proceedings of the 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Denver, CO, 2009.

Lin, 2010, Acoustic characterization of an ethylene-fueled scramjet combustor with a cavity flameholder, J. Propuls. Power, 26, 1161, 10.2514/1.43338

J. Liu, C.-J. Tam, T. Lu, C.K. Law, Simulations of cavity-stabilized flames in supersonic flows using reduced chemical kinetic mechanisms, in: Proceedings of the 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Sacramento, CA, 2006.

Mathur, 2001, Supersonic combustion experiments with a cavity-based fuel injector, J. Propuls. Power, 17, 1305, 10.2514/2.5879

Maull, 1963, Three-dimensional flow in cavities, J. Fluid Mech., 16, 620, 10.1017/S0022112063001014

C. McClinton, A. Roudakov, V. Semenov, V. Kopehenov, Comparative Flow Path Analysis and Design Assessment of an Axisymmetric Hydrogen Fueled Scramjet Flight Engine at a Mach Number of 6.5, AIAA Paper 96-4571, 1996

P.A. McMurtry, W.-H. Jou, R.W. Metcalfe, J.J. Riley, Direct Numerical Simulations of a Reacting Mixing Layer with Chemical Heat Release 23rd AIAA Aerospace Sciences Meeting, Reno, NV, AIAA Paper 85-0143, 1985.

Micka, 2010

D.J. Micka, J.F. Driscoll, Reaction zone imaging in a dual-mode scramjet combustor using CH-PLIF, in: Proceedings of the 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Hartford, CT, 2008.

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

R.T. Milligan, Dual mode scramjet: a computational investigation of combustor design and operation (M.S. thesis), Department of Mechanical and Materials Engineering, Wright State University, Dayton, OH, 2009.

Mishra, 2012, Numerical study on effect of fuel injection angle on the performance of a 2D supersonic cavity combustor, J. Aerosp. Eng., 25, 161, 10.1061/(ASCE)AS.1943-5525.0000093

Mohamed Ali, 2005, Cavity-based injections into supersonic flow, J. Propuls. Power, 21, 1130, 10.2514/1.15716

Murray, 2001, Characteristics of the compressible shear layer over a cavity, AIAA J., 39, 846, 10.2514/2.1388

D.A. Orodnikov, V.A. Vinogradov, Y.M. Shikhman, V.N. Strokin, Design and Research Russian Program of Experimental Hydrogen-Fueled Dual-Mode Scramjet: Choice of Concept and Results of Pre-Flight Tests, AIAA Paper 98-1586, 1998

P.J. Ortwerth, A.B. Mathur, V.A. Vinogradov, V.T. Grin, M.A. Goldfeld, A. Starov, Experimental and Numerical Investigation of Hydrogen and Ethylene Combustion in a Mach 3–5 Channel with a Single Injector, in: Proceedings of the 32nd AIAA/ASME/SAE/ASEE Join Propulsion Conference and Exhibit, Lake Buena Vista, FL, AIAA Paper 96-3245, 1996.

P.J. Ortwerth, A.B. Mathur, C. Segal, M.G. Owens, Combustion stability limits of hydrogen in a non-premixed, supersonic Flow, in: Proceedings of the 14th International Symposium on Airbreathing Engines, 1999.

Owens, 1998, Flame-holding configurations for kerosene combustion in a Mach 1.8 airflow, J. Propuls. Power, 14, 456, 10.2514/2.5322

R.I. Ozawa, Survey of Basic Data on Flame Stabilization and Propagation for High Speed Combustion Systems, Marquardt Co., TR AFAPL-TR-70-81, 1971.

Pan, 2011, Experimental investigation of combustion mechanisms of kerosene-fueled scramjet engines with double-cavity flameholders, Acta Mech. Sin., 27, 891, 10.1007/s10409-011-0470-8

Pan, 2012, Flame quenching process in cavity based on model scramjet combustor, Acta Mech. Sin., 28, 73, 10.1007/s10409-012-0020-z

Papamoschou, 1988, The compressible turbulent shear layer: an experimental study, J. Fluid Mech., 197, 453, 10.1017/S0022112088003325

S.W. Perng, D.S. Dolling, Passive control of pressure oscillations in hypersonic cavity flow, in: Proceedings of the 34th AIAA Aerospace Sciences Meeting & Exhibit, Reno, NV, AIAA Paper 96-0444, 1998.

Pourhassan, 1999

Rasmussen, 2005, Stability limits of cavity-stabilized flames in supersonic flow, Proc. Combust. Inst., 30, 2825, 10.1016/j.proci.2004.08.185

Rasmussen, 2007, Visualization of flameholding mechanisms in a supersonic combustor using PLIF, Proc. Combust. Inst., 31, 2505, 10.1016/j.proci.2006.08.007

Retaureau, 2012

G.J. Retaureau, S. Menon, Experimental studies on flame stability of a fueled cavity in a supersonic crossflow, in: Proceedings of the 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Nashville, TN, 2010.

J.E. Rossiter, Wind-tunnel experiments on the flow over rectangular cavities at subsonic and transonic speeds, Aeronautical Research Council Reports and Memoranda, No. 3838, 1964.

T. Rossmann, M.G. Mungal, R.K. Hanson, An Experimental Investigation of High-Compressibility Non-Reacting Mixing Layers, AIAA Paper 2000-0663, 2000.

Rowley, 2002, On self-sustained oscillations in two-dimensional compressible flow over rectangular cavities, J. Fluid Mech., 455, 315, 10.1017/S0022112001007534

Ryan, 2009, Planar laser-induced fluorescence imaging of OH in a supersonic combustor fueled with ethylene and methane, Proc. Combust. Inst., 32, 2429, 10.1016/j.proci.2008.06.209

Samimy, 1990, Effects of compressibility on the characteristics of free shear flows, AIAA J., 28, 439, 10.2514/3.10412

Samimy, 1986, Study of compressible turbulent reattaching free shear layers, AIAA J., 24, 261, 10.2514/3.9254

Segal, 2009

V. Strokin, V. Grachov, The peculiarities of hydrogen combustion in model scramjet combustion, in: Proceedings of the International Symposium on Airbreathing Engines, ISABE Paper 97-7056, 1997, pp. 374–384.

F.D. Stull, R.R. Craig, J.T. Hojnacki, Dump Combustor Parametric Investigation, AFAPL-TR-74-90, U.S. Air Force, 1975.

Thakur, 2008, Concentration distribution in a supersonic flow recirculation, J. Propuls. Power, 24, 64, 10.2514/1.25396

Tuttle, 2014, Particle image velocimetry in a nonreacting and reacting high-speed cavity, J. Propuls. Power, 30, 576, 10.2514/1.B34974

Ukeiley, 2004, Suppression of pressure loads in cavity flows, AIAA J., 42, 70, 10.2514/1.9032

Ö.H. Unalmis, N.T. Clemens, D.S. Dolling, Planar Laser Imaging of High-Speed Cavity Flow Dynamics, AIAA Paper 98-0776, 1998.

Ö.H. Unalmis, N.T. Clemens, D.S. Dolling, Planar Laser Imaging of a Supersonic Side-Facing Cavity, AIAA Paper 99-0297, 1999.

Unalmis, 2001, Experimental study of shear-layer/acoustics coupling in Mach 5 cavity flow, AIAA J., 39, 242, 10.2514/2.1319

Unalmis, 2004, Cavity oscillation mechanisms in high-speed flows, AIAA J., 42, 2035, 10.2514/1.1000

Vinogradov, 2013, Operation process and stabilization of kerosene combustion in a combustor model with high flow velocities at the combustor entrance, Combust. Explos. Shock Waves, 49, 512, 10.1134/S001050821305002X

Wang, 2013, Combustion characteristics in a supersonic combustor with hydrogen injection upstream of cavity flameholder, Proc. Combust. Inst., 34, 2073, 10.1016/j.proci.2012.06.049

Wang, 2013, Combustion modes of hydrogen jet combustion in a cavity-based supersonic combustor, Int. J. Hydrog. Energy, 38, 12078, 10.1016/j.ijhydene.2013.06.132

G. Winterfeld, On processes of turbulent exchange behind flame holders, in: Proceedings of the Tenth International Symposium on Combustion, Combustion Institute, Pittsburgh, PA, 1965, pp. 1265–1275.

V. Yang, J. Li, J.Y. Choi, K.-C. Lin, Ignition transient in an ethylene fueled scramjet engine with air throttling, Part II: ignition and flame development, in: Proceedings of the 48th AIAA Aerospace Sciences Meeting and Exhibit, Orlando, FL, 2010.

Yeom, 2013, Numerical analysis of a scramjet engine with intake sidewalls and cavity flameholder, AIAA J., 51, 1566, 10.2514/1.J051677

K.H. Yu, K.J. Wilson, K.C. Schadow, Effect of Flame-Holding Cavities on Supersonic Combustion Performance, AIAA Paper 99-2638, 1999.

Zhang, 1998, The effect of trailing edge geometry on cavity flow oscillation driven by a supersonic shear layer, Aeronaut. J. R. Aeronaut. Soc., 102, 129

Zhang, 1990, An investigation of supersonic oscillatory cavity flows driven by thick shear layers, Aeronaut. J. R. Aeronaut. Soc., 94, 353

Zhuang, 2007

E.E. Zukoski, F.E. Marble, Experiments concerning the mechanism of flame blowoff from bluff bodies, in: Proceedings of the Gas Dynamics Symposium on Aerothermochemistry, Northwestern University, 1956.