MIXING AND COMBUSTION OF CRYOGENIC OXYGEN-HYDROGEN SHEAR-COAXIAL JET FLAMES AT SUPERCRITICAL PRESSURE

REFERENCES

• Bird , R.B. , Stewart , W.E. , and Lightfoot , E.N. ( 1960 ) Transport Phenomena , John Wiley and Sons, Inc. , New York, New York .
   Google Scholar
• Candel , S. , Herding , G. , Snyder , R. , Scouflaire , P. , Rolon , C. , and Vingert , L. ( 1998 ) Experimental investigation of shear coaxial cryogenic jet flames . Journal of Propulsion and Power , 14 ( 5 ), 826 – 834 . [CSA]
   Web of Science ®Google Scholar
• Candel , S. , Juniper , M. , Singla , G. , Scouflaire , P. , and Rolon , C. ( 2005 ) Structure and dynamics of cryogenic flames at supercritical pressure , Combust. Sci. Tech. , 177 : 2199 – 2230 . [CSA]
   Google Scholar
• Ely , J.F. and Hanley , H.J.M. ( 1981a ) Prediction of transport properties. 1. Viscosity of fluids and mixtures . Industrial and Engineering Chemistry Fundamentals , 20 ( 4 ), 323 – 332 . [CSA] [CROSSREF]
   Web of Science ®Google Scholar
• Ely , J.F. and Hanley , H.J.M. ( 1981b ) Prediction of transport properties. 2. Thermal conductivity of pure fluids and mixtures . Industrial and Engineering Chemistry Fundamentals , 22 ( 1 ), 90 – 97 . [CSA] [CROSSREF]
   Web of Science ®Google Scholar
• Gordon , S. and McBride , B.J. ( 1971 ) Computer program for calculation of complex chemical equilibrium compositions, rocket performance, incident and reflected shocks and Chapman-Jouguet detonations , Technical Report NASA SP-273 , National Aeronautics and Space Administration .
   Google Scholar
• Gurliat , O. , Schmidt , V. , Haidn , O.J. , and Oschwald , M. ( 2003 ) Ignition of cryogenic H2/LOX sprays . Aerospace Science and Technology , 7 , 517 – 531 . [CSA] [CROSSREF]
   Web of Science ®Google Scholar
• Habiballah , M. , Orain , M. , Grisch , F. , Vingert , L. , and Gicquel , P. ( 2005 ) Experimental studies of high pressure cryogenic flames on the mascotte facility , Combust. Sci. Tech. , 177 : 2139 – 2166 . [CSA]
   Google Scholar
• Herding , G. , Snyder , R. , Rolon , C. , and Candel , S. (1998) Investigation of cryogenic propellant flames using computerized tomography of emission images. Journal of Propulsion and Power , 13(2), 146–151. [CSA]
   Web of Science ®Google Scholar
• Hirschfelder , J.O. , Curtiss , C.F. , and Bird , R.B. ( 1964 ) Molecular Theory of Gases and Liquids, , 2nd ed. , John Wiley and Sons, Inc. , New York, New York .
   Google Scholar
• Juniper , M. , Tripathi , A. , Scouflaire , P. , Rolon , C. , and Candel , S. ( 2000 ) Structure of cryogenic flames at elevated pressures . Proceedings of the Combustion Institute , 28 ( 1 ), 1103 – 1109 . [CSA]
   Web of Science ®Google Scholar
• Kee , R.J. , Rupley , F.M. , and Miller , J.A. ( 1990 ) Chemkin thermodynamic data base , Technical Report SAND87-8215B , Sandia National Laboratories . Supersedes SAND87-8215 dated April 1987 .
   Google Scholar
• Kendrick , D. , Herding , G. , Scouflaire , P. , Rolon , C. , and Candel , S. ( 1999 ) Effects of a recess on cryogenic flame stabilization . Combustion and Flame , 118 , 327 – 339 . [CSA] [CROSSREF]
   Web of Science ®Google Scholar
• Leland , T.W. and Chappelear , P.S. ( 1968 ) The corresponding states principle. A review of current theory and practice . Industrial and Engineering Chemistry Fundamentals , 60 ( 7 ), 15 – 43 . [CSA] [CROSSREF]
   Web of Science ®Google Scholar
• Mayer , W. and Tamura , H. ( 1996 ) Propellant injection in a liquid oxygen/gaseous hydrogen rocket engine . Journal of Propulsion and Power , 12 ( 6 ), 1137 – 1147 . [CSA]
   Web of Science ®Google Scholar
• Mayer , W. , Schik , A. , Schäffler , M. , and Tamura , H. ( 2000 ) Injection and mixing processes in high-pressure liquid oxygen/gaseous hydrogen rocket combustors . Journal of Propulsion and Power , 16 ( 5 ), 823 – 828 . [CSA]
   Web of Science ®Google Scholar
• Mayer , W. , Schik , A. , Vieille , B. , Chaveau , C , Gökalp , I. , Talley , D. , and Woodward , R. ( 1998 ) Atomization and breakup of cryogenic propellants under high-pressure subcritical and supercritical conditions . Journal of Propulsion and Power , 14 ( 5 ), 835 – 842 . [CSA]
   Web of Science ®Google Scholar
• Oefelein , J.C. ( 1997 ) Simulation and Analysis of Turbulent Multiphase Combustion Processes at High Pressures, PhD thesis, The Pennsylvania State University , University Park , Pennsylvania .
   Google Scholar
• Oefelein , J.C. ( 2005 ) Thermophysical characteristics of LOX–H2 flames at supercritical pressure . Proceedings of the Combustion Institute , 30 ( 1 ), 2929 – 2937 . [CSA] [CROSSREF]
   Web of Science ®Google Scholar
• Oefelein , J.C. and Yang , V. ( 1998 ) Modeling high-pressure mixing and combustion processes in liquid rocket engines . Journal of Propulsion and Power , 14 ( 5 ), 843 – 857 . [CSA]
   Web of Science ®Google Scholar
• Oschwald , M. , Smith , J.J. , Branam , R. , Hussong , J. , and Schik , A. ( 2005 ) Injection of fluids into supercritical environments , Combust. Sci. Tech. , 177 : 2087 – 2138 . [CSA]
   Google Scholar
• Reid , R.C. , Prausnitz , J.M. , and Polling , B.E. ( 1987 ) The Properties of Liquids and Gases, , 4th ed. , McGraw-Hill , New York, New York .
   Google Scholar
• Rowlinson , J.S. and Watson , I.D. ( 1969 ) The prediction of the thermodynamic properties of fluids and fluid mixtures–I. The principle of corresponding states and its extensions . Chemical Engineering Science , 24 ( 8 ), 1565 – 1574 . [CSA] [CROSSREF]
   Web of Science ®Google Scholar
• Takahashi , S. (1974) Preparation of a generalized chart for the diffusion coefficients of gases at high pressures. Journal of Chemical Engineering of Japan , 7(6), 417–420. [CSA]
   Google Scholar
• VanWylen , G.J. and Sonntag , R.E. ( 1986 ) Fundamentals of Classical Thermodynamics, , 3rd ed. , John Wiley and Sons, Inc. , New York, New York .
   Google Scholar
• Westbrook , C.K. and Dryer , F.L. ( 1984 ) Chemical kinetics modeling of hydrocarbon combustion . Progress in Energy and Combustion Science , 10 ( 1 ), 1 – 57 . [CSA] [CROSSREF]
   Web of Science ®Google Scholar
• Yetter , R.A. , Dryer , F.L. , and Rabitz , H. ( 1991 ) A comprehensive reaction mechanism for carbon monoxide/hydrogen/oxygen kinetics . Combustion Science and Technology , 79 , 97 – 128 . [CSA]
   Web of Science ®Google Scholar
• Portions of this work have been funded by the United States Department of Energy, Office of Basic Energy Sciences and the NASA Marshall Space Flight Center. The support provided is gratefully acknowledged.
   Google Scholar
• The U.S. Department of Energy, Office of Basic Energy Sciences, Division of Chemical Sciences, Geosciences, and Biosciences supported this work. Sandia National Laboratories is a multiprogram laboratory operated by Sandia Corporation, a Lockheed Martin Company, for the United States Department of Energy under contract DE-AC04-94-AL 85000.
   Google Scholar