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Part 2: Supercritical Fluid Injection, Mixing, and Combustion

CRYOGENIC FLUID JETS AND MIXING LAYERS IN TRANSCRITICAL AND SUPERCRITICAL ENVIRONMENTS

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Pages 193-227 | Received 05 Feb 2005, Accepted 26 Jul 2005, Published online: 25 Jan 2007

REFERENCES

  • Abramovich , G.N. ( 1976 ) Applied Gas Dynamics , Nauka , Moscow , Russia .
  • Amielh , M. , Djeridane , T. , Anselmet , F. , and Fulachier , L. ( 1996 ) Velocity near field of variable density turbulent jets . Int. J. Heat Mass Transfer , 39 , 2149 – 2164 . [CSA]
  • Atsavapranee , P. and Gharib , M. ( 1997 ) Structures in stratified plane mixing layers and the effects of cross-shear . J. Fluid Mech. , 342 , 53 – 86 . [CSA] [CROSSREF] [CROSSREF]
  • Bazarov , V.G. and Yang , V. ( 1998 ) Liquid-propellant rocket engine injector dynamics . J. Propul. Power , 14 , 797 – 806 . [CSA]
  • Bazarov , V.G. , Yang , V. , and Puneesh , P. ( 2004 ) Design and dynamics of jet and swirl injectors . In Yang , V. , Habiballah , M. , Hulka , J. , and Popp , M. (Eds.) Liquid Rocket Thrust Chambers: Aspect of Modeling, Analysis, and Design , Progress in Astronautics and Aeronautics , Vol. 200 , pp. 19 – 104 .
  • Branam , R. and Mayer , W. ( 2003 ) Characterization of cryogenic injection at supercritical pressure . J. Propul. Power , 19 , 342 – 355 . [CSA]
  • Candel , S. , Juniper , M. , Singla , G. , Scouflaire , P. , and Rolon , C. ( 2005 ) Structure and dynamics of cryogenic flames at supercritical pressure. To be published in Combust. Sci. and Tech. [CSA]
  • Carlos , B. , Guillaume , B. , Patrick , B. , and Olivier , M. ( 2003 ) Instability and transition in high velocity ratio coaxial jets: A Numerical Study . 3rd International Symposium on Turbulence and Shear Flow Phenomena , Sendai , Japan .
  • Chehroudi , B. , Cohn , R. , Talley , D. , and Badakhshan , A. ( 2002a ) Cryogenic shear layers: experiments and phenomenological modeling of the initial growth rate under subcritical and supercritical conditions . Int. J. Heat Fluid Fl. , 23 , 554 – 563 . [CSA] [CROSSREF] [CROSSREF]
  • Chehroudi , B. and Talley , D. ( 2002 ) Interaction of acoustic waves with a cryogenic nitrogen jet at sub- and super-critical pressures . AIAA Paper No. 2002-0342 .
  • Chehroudi , B. , Talley , D. , and Coy , E. ( 2002b ) Visual characteristics and initial growth rates of round cryogenic jets at subcritical and supercritical pressures . Phys. Fluids , 14 , 850 – 861 . [CSA] [CROSSREF] [CROSSREF]
  • Davis , D. and Chehroudi , B. ( 2004 ) The effects of pressure and acoustic field on a cryogenic coaxial jet . AIAA Paper No. 2004-1330 .
  • Dimotakis , P.E. ( 1986 ) Two-dimensional shear-layer entrainment . AIAA J. , 21 , 1791 – 1796 . [CSA]
  • Ely , J.F. and Hanley , H.J. ( 1981 ) Prediction of transport properties. 1. Viscosity of fluids and mixtures . Ind. Eng. Chem. Fundamentals , 20 , 323 – 332 . [CSA] [CROSSREF] [CROSSREF]
  • Ely , J.F. and Hanley , H.J. (1983) Prediction of transport properties. 2. Thermal conductivity of pure fluids and mixtures. Ind. Eng. Chem. Fundamentals , 22, 90–97. [CSA] [CROSSREF] [CROSSREF]
  • Erlebacher , G. , Hussaini , M.Y. , Speziale , C.G. , and Zang , T.A. ( 1992 ) Toward the large eddy simulation of compressible turbulent flows . J. Fluid Mech. , 238 , 155 – 185 . [CSA]
  • Graboski , M.S. and Daubert , T.E. ( 1978 ) A modified Soave equation of state for phase equilibrium calculation, 1. Hydrocarbon systems . Ind. Eng. Chem. Proc. Design Dev. , 17 , 443 – 448 . [CSA] [CROSSREF] [CROSSREF]
  • Habiballah , M. , Orain , M. , Grisch, F. , Vingert , L. , and Gicquel , P. ( 2005 ) Experimental studies of high pressure cryogenic flames on the Mascotte facility. To be published in Combust. Sci. Tech. [CSA]
  • Hannoun , I.A. , Fernando , H.J.S. , and List , E.J. ( 1988 ) Turbulence structure near a sharp density interface . J. Fluid Mech. , 189 , 189 – 209 . [CSA]
  • Herding , G. , Snyder , R. , Rolon , C. , and Candel , S. ( 1998 ) Investigation of cryogenic propellant flames using computerized tomography of emission images . J. Propul. Power , 14 , 146 – 151 . [CSA]
  • Ho , C.M. and Huerre , P. ( 1984 ) Perturbed free shear layers . Ann. Rev. Fluid Mech. , 16 , 365 – 422 . [CSA] [CROSSREF] [CROSSREF]
  • Hsieh , S.Y. and Yang , V. ( 1997 ) A preconditioned flux-differencing scheme for chemically reacting flows at all Mach numbers . Int. J. Comput. Fluid Dyn. , 8 , 31 – 49 . [CSA]
  • Hulka , J. and Makel , D. ( 1993 ) Liquid oxygen/hydrogen testing of a single swirl coaxial injector element in a windowed combustion chamber . AIAA Paper No. 1993-1954 .
  • Hulka , J. and Schneider , J.A. ( 1991 ) Performance and stability of a booster class LOX/H2 swirl coaxial element injector . AIAA Paper No. 1991-1877 .
  • Hulka , J. and Schneider , J.A. ( 1993 ) Single element injector cold flow testing for STME swirl coaxial injector element design . AIAA Paper No. 1993-2161 .
  • Ivancic , B. and Mayer , W. ( 2002 ) Time- and length scales of combustion in liquid rocket thrust chambers . J. Propul. Power , 18 , 247 – 253 . [CSA]
  • Jacobsen , R.T. and Stewart , R.B. ( 1973 ) Thermodynamic properties of nitrogen including liquid and vapor phases from 63 K to 2000 K with pressure to 10,000 bar . J. Phys. Chem. Ref. Data , 2 , 757 – 922 . [CSA]
  • Juniper , M. , Tripathi , A. , Scouflaire , P. , Rolon , C. , and Candel , S. ( 2000 ) Structure of cryogenic flames at elevated pressures . Proc. Combust. Inst. , 28 , 1103 – 1109 . [CSA]
  • Kendrick , D. , Herding , G. , Scouflaire , P. , Rolon , C. , and Candel , S. ( 1999 ) Effects of recess on cryogenic flame stabilization . Combust. Flame , 118 , 327 – 339 . [CSA] [CROSSREF] [CROSSREF]
  • Liu , T. , Zong , N. , and Yang , V. ( 2005 ) Temporal and spatial stability of real-fluid mixing layer with density stratification. To be submitted to Phys. Fluids . [CSA]
  • Mayer , W. , Ivancic , B. , Schik , A. , and Hornung , U. (2001) Propellant atomization and ignition phenomena in liquid oxygen/gaseous hydrogen rocket combustors. J. Propul. Power , 15, 794–799. [CSA]
  • Mayer , W. , Schik , A. , Schaffler , M. , and Tamura , H. ( 2000 ) Injection and mixing processes in high-pressure liquid oxygen/gaseous hydrogen rocket combustor . J. Propul. Power , 16 , 823 – 828 . [CSA]
  • Mayer , W. and Smith , J.J. ( 2004 ) Fundamentals of supercritical mixing and combustion of cryogenic propellants . In Yang , V. , Habiballah , M. , Hulka , J. , and Popp , M. (Eds.) Liquid Rocket Thrust Chambers: Aspect of Modeling, Analysis, and Design , Progress in Astronautics and Aeronautics , Vol. 200 , 339 – 368 .
  • Mayer , W. and Tamura , H. ( 1996 ) Propellant injection in a liquid oxygen/gaseous hydrogen rocket engine . J. Propul. Power , 12 , 1137 – 1147 . [CSA]
  • Meng , H. and Yang , V. ( 2003 ) A unified treatment of general fluid thermodynamics and its application to a preconditioning scheme . J. Comput. Phys. , 189 , 277 – 304 . [CSA] [CROSSREF] [CROSSREF]
  • Meng , H. , Hsiao , G.C. , Yang , V. , and Shuen , J.S. ( 2005 ) Transport and dynamics of liquid oxygen droplets in supercritical hydrogen streams . J. Fluid Mech. , 527 , 115 – 139 . [CSA] [CROSSREF] [CROSSREF]
  • Miller , R.S. , Harstad , K.G. , and Bellan , J. ( 2001 ) Direct numerical simulations of supercritical fluid mixing layers applied to heptane-nitrogen . J. Fluid Mech. , 436 , 1 – 39 . [CSA] [CROSSREF] [CROSSREF]
  • Oefelein , J.C. ( 2003 ) LES of supercritical LOX-H2 injection and combustion in shear-coaxial uni-element rocket . AIAA paper No. 2003-479 .
  • Oefelein , J.C. ( 2005 ) Simulation and analysis of cryogenic LOX-H2 combustion processes at supercritical pressure. To be published in Combust. Sci. Tech . [CSA]
  • Oefelein , J.C. and Yang , V. ( 1998 ) Modeling high-pressure mixing and combustion processes in liquid rocket engines . J. Propul. Power , 14 , 843 – 857 . [CSA]
  • Okong'o , N.A. and Bellan , J. ( 2002 ) Direct numerical simulation of a transitional supercritical binary mixing layer: heptane and nitrogen . J. Fluid Mech. , 464 , 1 – 34 . [CSA] [CROSSREF] [CROSSREF]
  • Okong'o , N.A. and Bellan , J. ( 2004 ) Turbulent and fluid-front area production in binary-species, supercritical, transitional mixing layers . Phys. Fluids , 16 , 1467 – 1492 . [CSA] [CROSSREF] [CROSSREF]
  • Okong'o , N.A. , Harstad , K.G. , and Bellan , J. ( 2002 ) Direct numerical simulation of O2/H2 temporal mixing layers under supercritical conditions . AIAA J. , 40 , 914 – 926 . [CSA]
  • Oschwald , M. and Schik , A. ( 1999 ) Supercritical nitrogen free jet investigated by spontaneous Raman scattering . Exp. Fluids , 27 , 497 – 506 . [CSA] [CROSSREF] [CROSSREF]
  • Oschwald , M. , Smith , J.J. , Branam , R. , Hussong , J. , Schik , A. , Chehroudi , B. , and Talley , D. ( 2005 ) Injection of fluid into supercritical environments. To be published in Combust. Sci. Tech. [CSA]
  • Papamoschou , D. and Roshko , A. (1988) The compressible turbulent shear layer: An experimental study. J. Fluid Mech. , 197, 453–477. [CSA]
  • Rehab , H. , Villermaux , E. , and Hopfinger , E.J. ( 1997 ) Flow regimes of large-velocity-ratio coaxial jets . J. Fluid Mech. , 345 , 357 – 381 . [CSA] [CROSSREF] [CROSSREF]
  • Reitz , R.D. and Bracco , F.V. ( 1979 ) On the dependence of spray angle and other spray parameters on nozzle design and operating condition . SAE Paper no. 790494 .
  • Rubinsky , V.R. ( 1996 ) Combustion instability in the RD-0110 Engine . In Yang , V. and Anderson , W. (Eds.) Liquid Rocket Engine Combustion Instability , Progress in Astronautics and Aeronautics, AIAA , Washington , DC , Vol. 169 , pp. 89 – 112 .
  • Sasaki , M. , Sakamoto , H. , Takahashi , M. , Tomita , T. , and Tamura , H. ( 1997 ) Comparative study of recessed and non-recessed swirl coaxial injectors . AIAA Paper No. 1997-2907 .
  • Schadow , K.C. and Gutmark , E. ( 1992 ) Combustion instability related to vortex shedding in dump combustors and their passive control . Prog. Energy Combust. Sci. , 18 , 117 – 132 . [CSA] [CROSSREF] [CROSSREF]
  • Singla , G. , Scouflaire , P. , and Candel , S. ( 2004 ) Transcritical oxygen/transcritical or supercritical methane combustion . Proc. Combust. Inst. , 30 , 2921 – 2928 . [CSA] [CROSSREF] [CROSSREF]
  • Soteriou , M.C. and Ghoniem , A. ( 1995 ) Effects of the free-stream density ratio on free and forced spatially developing shear layers . Phys. Fluids , 7 , 2036 – 2051 . [CSA] [CROSSREF] [CROSSREF]
  • Strakey , P.A. , Talley , D. , and Hutt , J.J. ( 2001 ) Mixing characteristics of coaxial injectors at high gas/liquid momentum ratios . J. Propul. Power , 17 , 402 – 410 . [CSA]
  • Swanson , R.C. and Turkel , E. ( 1992 ) On central difference and upwind schemes . J. Comput. Phys. , 101 , 292 – 306 . [CSA] [CROSSREF] [CROSSREF]
  • Takahashi , S. ( 1974 ) Preparation of a generalized chart for diffusion coefficients of gases at high pressures . J. Chem. Eng (Japan) , 7 , 417 – 420 . [CSA]
  • Tanasawa , Y. and Kobayasi , K. ( 1955 ) A study on swirl atomizer . Technical report of Tohoku University , 20 , 27 – 58 . [CSA]
  • Wang , S.W. , Hseih , S.Y. , and Yang , V. ( 2005 ) Unsteady flow evolution in swirl injector with radial entry, Part I: Stationary conditions . Phys. Fluids , 17 , 045106 . [CSA] [CROSSREF] [CROSSREF]
  • Wee , D. , Yi , T. , Annaswamy , A. , and Ghoniem , A.F. ( 2004 ) Self-sustained oscillations and vortex shedding in backward-facing step flows: Simulation and linear instability analysis . Phys. Fluids , 16 , 3361 – 3373 . [CSA] [CROSSREF] [CROSSREF]
  • Yang , V. ( 2000 ) Modeling of supercritical vaporization, mixing, and combustion processes in liquid-fueled propulsion systems . Proc. Combust. Inst. , 28 , 925 – 942 . [CSA]
  • Yu , M.H. and Monkewitz , P.A. ( 1990 ) The effect of nonuniform density on the absolute instability of two-dimensional inertial jets and wakes . Phys. Fluids A , 2 , 1175 – 1181 . [CSA] [CROSSREF] [CROSSREF]
  • Zhou , X. , Luo , K.H. , and Williams , J.J.R. (2001) Study of density effects in turbulent buoyant jets using large-eddy simulation. Theoret. Comput. Fluid Dynamics , 15, 95–120. [CSA] [CROSSREF] [CROSSREF]
  • Zong , N. , Meng , H. , Hsieh , S.Y. , and Yang , V. ( 2004 ) A numerical study of cryogenic fluid injection and mixing under supercritical conditions . Phys. Fluids , 16 , 4248 – 4261 . [CSA] [CROSSREF] [CROSSREF]
  • Zong , N. and Yang , V. ( 2004 ) Dynamics of simplex swirl injectors for cryogenic propellants at supercritical conditions . AIAA Paper No. 2004-1332 .
  • Zong , N. ( 2005 ) Modeling and simulation of cryogenic fluid injection and mixing dynamics under supercritical conditions. Ph.D. dissertation, Department of Mechanical and Nuclear Engineering , Pennsylvania State University , University Park , PA .
  • Zong , N. and Yang , V. ( 2005a ) A numerical study of high-pressure oxygen/methane mixing and combustion of a shear coaxial injector . AIAA Paper No. 2005-0152 .
  • Zong , N. and Yang , V. ( 2005b ) An efficient preconditioning scheme for general fluid mixture using primitive variables. To be submitted to J. Comput. Phys. [CSA]
  • Zurbach , S. , Thomas , J.L. , Verplancke , C. , Vingert , L. , and Habiballah , M. ( 2003 ) LOX/Methane studies for fuel rich preburner . AIAA Paper No. 2003-5063 .

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