Table Of Content

J. THERMOPHYSICS, VOL. 6, NO. 4: 1992 INDEX Subject Index Aircraft Technology, Conventional, Microstructure Effects on the Conjugate Models of Energy-Exchange Mechanics Ap- STOL/VTOL Heat Transfer Along a Vertical Circular plicable to a Particle Simulation of Reac- Pia 92-023 tive Flow 792-036 Aerodynamics Boundary Layers and Heat Inlet, Nozzle, Diffusor, and Channel Laminar Mixed Convection from a Uniform Transfer—Turbulent Flows Heat Flux Horizontal Cylinder in a Cross- Wall Heating Effects in Mixed Convection in Surface Cooling by Transpiration of a Freez- flow T92-046 Vertical Annulus with Variable Properties ing Liquid 192-022 192-045 Aerospace Plane Surface Cooling by Transpiration of a Freez- Jets, Wakes, and Viscid-Inviscid Flow ing Liquid T92-022 Surface Cooling of Scramjet Engine Inlets Interactions Rough-Wall Turbulent Heat Transfer with Using Heat Pipe, Transpiration, and Film Step-Wall Temperature Boundary Condi- Application of Laser Holographic Interfer- Cooling 792-079 tions 792-011 ometry to Temperature Measurements in Buoyant Air Jets T92-060 Manufacturing ComputaFtluiido Dnynaamlic s Experimental Investigation of Film Cooling Thermophysical Properties of ——— Solution of the Parabolized Navier-Stokes Effectiveness for Slots of Various Exit (Protein) Solutions Equations Using Osher’s Upwind Scheme Geometries T92-049 T92-069 Energy Accuracy of the Burnett Equations for Multiphase Flows Hypersonic Real Gas Flows 792-068 Investigation of Liquid Droplet Evaporation Conservation Thermochemical Nonequilibrium Flow Com- in Subcritical and Supercritical Gaseous Second-Law Optimization of Forced Con- putations of Flow Around the Aeroassist Environments T92-123 vection of Non-Newtonian Fluids in Ducts Flight Experiment T92-066 Convective Heat Transfer of a Particulate 792-085 Laminar Impingement Jet Mach Number Suspension 792-089 Transient Solidification of a Binary Mixture and Temperature Effects on Heat Transfer Thermal Radiation Effects on a Shocked in an Inclined Rectangular Cavity 92-050 Particle-Laden Gas 192-075 Heat Transfer in the Entrance Region of Entrance Heat Transfer in Isosceles and Semicircular Ducts with Internal Fins Right Triangular Ducts 192-026 Flywheels 192-048 Experimental Investigation of Transition Laminar Mixed Convection from a Uniform Boiling in Forced Convection 192-020 Convective Thermal Ignition of an Individ- Heat Flux Horizontal Cylinder in a Cross- Analytical Two-Phase Flow Void Prediction ual Polymethylmethacrylate Particle flow T92-046 Method 792-019 192-054 Diagonal Implicit Scheme for Computing Magnetohydrodynamic Power Flows with Finite Rate Chemistry Plasmadynaamndi cMsH D Generation 192-037 Bias in Emission Absorption Measurements Biaosf iTne mEpmeirsastiuorne Abasnodr pAttioomni cM eaDsenusrietmye nts MixFleudi d Coinn vtehcet iAonnn uloif Lofo wR otPartainndgt l CyNlu1i9mn2bd-ee0r2rs4 of Temperature and Atomic Densit19y2 -124 T92-124 Flowfield Analysis for High-Enthalpy Arc ArcnM e lTso r anstiothiyodnr oadnyd Groiwcst hG enoefr aBtiogr- A9rC2ch-s0a 7n3i-n MBiuPcoHriyeonaastn t tr-uTTcrhtaeunrrsmefoe cr aEpfAiflleolctnasgr y ao nF Vleorttwhi ec awlCi othnC ij7r9uc2Ngu-oa0lnt2a-e3r ArnHceel aTstgr eanrnessti othiyodnr odayn d Groics wthG enoefr aBtiogr- AT1r99Cc22hs--a 00n79i-35n uniform Supra-Heating: II. Two-Phase Nuclear Fission Electron Temperature and Electron Density Behavior 792-015 in a Rarefied Air Plasma Jet 92-033 Analytical Two-Phase Flow Void Prediction Buoyant-Thermocapillary Flow with Non- Method 92-019 uniform Supra-Heating: I. Liquid-Phase Rarefied Flows Behavior 192-014 Rotating Machinery Numerical Simulation of Rarefied Gas Flow Three-Dimensional Direct Particle Simula- Turbulent Heat Transfer in a Square Chan- Through a Slit 192-003 tion on the Connection Machine T92-108 Radiation Modeling with Direct Simulation nel with Staggered Discrete Ribs 192-027 Hydrodynamics Monte Carlo T92-107 Fluid Dynamics AccAerlteerrya tiHoena-tI ndPuicpeeds Depriming of Ex7t9e2r-n0a8l7 MoSnhtoec k CaFrrloon tSsi mulation of NonequiliTb92r-i1u0m6 Rotational Temperature Measurements in an Boundary Layers and Heat Hypersonic Flow Arc Jet 792-093 Transfer—Laminar Accuracy of the Burnett Equations for Three-Dimensional Direct Particle Simula- Hypersonic Real Gas Flows 792-068 Effect of Thermal Creep on Buoyancy- tion on the Connection Machine T92-108 Direct Simulation of Re-Entry Flows with Induced Flows in Low-Gravity 192-125 Monte Carlo Simulation of Nonequilibrium Ionization 192-065 Free Convection About Vertical Needles Shock Fronts T92-106 Models of Energy-Exchange Mechanics Ap- Embedded in a Saturated Porous Medium Laminar Heat Transfer to Blunt Cones in plicable to a Particle Simulation of Reac- T92-092 High-Enthalpy Hypervelocity Flows tive Flow 792-036 Laminar Impingement Jet Mach Number 92-070 Electron Temperature and Electron Density and Temperature Effects on Heat Transfer Solution of the Parabolized Navier-Stokes in a Rarefied Air Plasma Jet 792-033 T92-050 Equations Using Osher’s Upwind Scheme Wall Heating Effects in Mixed Convection in 92-069 Numerical Simulation of Rarefied Gas Flow Through a Slit 192-003 Vertical Annulus with Variable Properties Accuracy of the Burnett Equations for 192-045 Hypersonic Real Gas Flows 192-068 ReaFclowst anid Cnombgusti on Numerical Solutions of Natural Convection Thermochemical Nonequilibrium Flow Com- in Enclosure with Boundary Condition putations of Flow Around the Aeroassist Vibration-Dissociation Coupling in Non- Switching Method 192-044 Flight Experiment 792-066 equilibrium Flows T92-109 Entrance Heat Transfer in Isosceles and Direct Simulation of Re-Entry Flows with Monte Carlo Simulation of Nonequilibrium Right Triangular Ducts 192-026 Ionization T92-065 Shock Fronts T92-106 Mixed Convection of Low Prandtl Number Diagonal Implicit Scheme for Computing Chlorine Utilization Study for Uniform- Fluid in the Annuli of Rotating Cylinders Flows with Finite Rate Chemistry Droplet Singlet Delta Oxygen Generators 92-024 192-037 192-074 758 . THERMOPHYSICS, VOL. 6, NO. 4: 1992 INDEX Temperature Measurement of Reacting Heat Pipe and Surface Mass Transfer Cool- Dependent Scattering by Parallel Fibers: Flowfield by Phase-Shifting Holographic ing of Hypersonic Vehicle Structures Effects of Multiple Scattering and Wave Interferometry 792-072 T92-078 Interference 92-101 Modeling of an Argon Plasma in a Bound- Modeling the Postcure Regime of Ablative Effect of Surface Material Properties and ary-Layer Flow T92-038 Composite Materials 792-007 Surface Characteristics in Evaporative Flat-Ended Circular Cylinder in Hypersonic Spray Cooling 192-080 Rarefied Flow T92-004 Propulsion Separated Flows Convective Thermal Ignition of an Individ- Airbreathing Propulsion Structural Mechanics and Materials ual Polymethylmethacrylate Particle Experimental Investigation of Film Cooling 92-054 Effectiveness for Slots of Various Exit StrucFitniute rElaemlent s Geometries 792-049 Thermal-Structural Finite Element Analysis Shock Waves and Detonations Using Linear Flux Formulation 192-055 Thermal Radiation Effects on a Shocked Particle-Laden Gas 192-075 Spacecraft Technology Thermal Effects Thermal-Structural Finite Element Analysis Supersonic Flow Aerobraking Configurations/ Using Linear Flux Formulation 192-055 Flat-Ended Circular Cylinder in Hypersonic Aerothermodynamics Three-Dimensional Thermal Structural Anal- Rarefied Flow T92-004 Three-Dimensional Direct Particle Simula- ysis of a Swept Cowl Leading Edge Sub- tion on the Connection Machine T92-108 jected to Skewed Shock-Shock Interference Laminar Heat Transfer to Blunt Cones in Heating 792-006 High-Enthalpy Hypervelocity Flows GuidConatroln, acnd eDyn,ami cs 792-070 Technology Nonequilibrium Chemical and Radiation Thermophysics and Heat Transfer Coupling, Part II: Results for AOTV Information Processing Flowfields 792-064 Nonequilibrium Chemical and Radiation Ablation, Pyrolysis, Thermal Convective Flows in Enclosures with Vertical Coupling, Part I: Theory and Models Decomposition and Degradation Temperature or Concentration Gradients 792-061 192-063 Convective Thermal Ignition of an Individ- Earth Atmospheric Entry Studies for ual Polymethylmethacrylate Particle Interdisciplinary Topics Manned Mars Missions 792-035 792-054 Modeling the Postcure Regime of Ablative AerobrFliaghkt iMecnhagnic s Aerospace Management Composite Materials T92-007 Earth Atmospheric Entry Studies for Surface Cooling by Transpiration of a Freez- Manned Mars Missions 192-035 AerothermodTyhenrmaalm Piroctesct/io n ing Liquid 192-022 Spacecraft Thermal Energy Accommodation Space Experiments Analanyd Ntumeiriccal aMeltho ds from Atomic Recombination . 192-110 Flat-Ended Circular Cylinder in Hypersonic Vibration-Dissociation Coupling in Non- Three-Dimensional Thermal Structural Anal- Rarefied Flow T92-004 equilibrium Flows T92-109 ysis of a Swept Cowl Leading Edge Sub- Analytic Solution of the Transient Behavior jected to Skewed Shock-Shock Interference Space Processing of Radiation-Backscattering Heat Shields Heating 792-006 Effect of Thermal Creep on Buoyancy- T92-104 Lasers and Laser Applications TheIrnmdoupcheyd siFclaolw s Pirno pLeortwi-eGsr avioft y Lys1o9z2-y1m2e5 DepEfefnedcetsn t of SMcuatltteirpilneg Scbayt tePrairnagl lealn d FiWbaervse: Investigation of Mixed Convection About a (Protein) Solutions T92-083 Interference 92-101 Rotating Sphere by Holographic Interfer- Buoyant-Thermocapillary Flow with Non- Backward Monte Carlo Modeling for Rocket ometry 192-121 uniform Supra-Heating: II. Two-Phase Plume Base Heating 792-091 Correlation Transfer: Application of Radi- Behavior 792-015 Transient Combined Conduction and Ra- ative Transfer Solution Methods to Photon Buoyant-Thermocapillary Flow with Non- diation in Anisotropically Scattering Correlation Problems 792-100 uniform Supra-Heating: I. Liquid-Phase Spherical Media 92-090 Chlorine Utilization Study for Uniform- Behavior 192-014 Conduction—Radiation Interaction in Ab- Droplet Singlet Delta Oxygen Generators sorbing, Emitting and Anisotropically 192-074 Spacecraft Contamination/ Sterilization Scattering Media with Variable Thermal Temperature Measurement of Reacting Conductivity 192-084 Flowfield by Phase-Shifting Holographic Thermal Control Coatings Performance at Heat Pipe and Surface Mass Transfer Cool- Interferometry 192-072 Near Geosynchronous Altitude 192-112 ing of Hypersonic Vehicle Structures Two-Dimensional Radiative Transfer in a Spacecraft Power T92-078 Cylindrical Layered Medium with Reflect- Arc Heater Nozzle Heating Test with Hy- ing Interfaces 792-040 Transient Thermal Analysis of Three Fast- drogen Combustion Products 192-071 Charging Latent Heat Storage Configura- Laminar Heat Transfer to Blunt Cones in Sensor Systems tions 792-021 High-Enthalpy Hypervelocity Flows T92-070 Transient Conjugated Heat Transfer From a Spacecraft Propulsion System Stagnation Point Nonequilibrium Radiative Rectangular Hot Film T92-056 Integration Heating and the Influence of Energy Experimental Verification of Scaling Param- Exchange Models 192-067 eters for Thermal Stratification 192-082 Nonequilibrium Chemical and Radiation Launch Vehicle and Missile (LV/M) Coupling, Part II: Results for AOTV Technology Spacecraft Sensor Systems Flowfields 192-064 Nonequilibrium Chemical and Radiation Practical Model for Molecular Contaminant Coupling, Part I: Theory and Models Thermal Protection Systems Deposition Kinetics T92-111 T92-063 Dependent Scattering by Parallel Fibers: Experimental Investigation of Film Cooling Spacecraft Thermal Management Effects of Multiple Scattering and Wave Effectiveness for Slots of Various Exit Interference 792-101 Transient Behavior of Heat Pipes with Ther- Geometries 192-049 Backward Monte Carlo Modeling for Rocket mal Energy Storage Under Reversed- Earth Atmospheric Entry Studies for Plume Base Heating 792-091 Pulsed Heat Loads 92-115 Manned Mars Missions 192-035 J. THERMOPHYSICS, VOL. 6, NO. 4: 1992 INDEX Electron Temperature and Electron Density Periodically Fully Developed Flow in Chan- Thermal Contacts in Transient States: A in a Rarefied Air Plasma Jet 792-033 nels with Conducting Blockages 192-012 New Model and Two Experiments Monte Carlo Simulation of Vibrational Re- 192-057 laxation in Nitrogen T92-002 Transient Conjugated Heat Transfer From a Cryogenics Rectangular Hot Film 92-056 Experimental Verification of Scaling Param- Two-Dimensional Effects in a Triangular Boiling/ Condensation eters for Thermal Stratification 192-082 Convecting Fin 192-025 Mixed Convection of Low Prandtl Number Investigation of Liquid Droplet Evaporation Fluid in the Annuli of Rotating Cylinders in Subcritical and Supercritical Gaseous Electronics Cooling T92-024 Environments 792-123 Enhanced Cooling of Electronic Components Microstructure Effects on the Conjugate Effect of Surface Material Properties and by Flow Oscillation 192-117 Heat Transfer Along a Vertical Circular Surface Characteristics in Evaporative Effect of Surface Material Properties and Pin 792-023 Spray Cooling T92-080 Surface Characteristics in Evaporative Periodically Fully Developed Flow in Chan- Filmwise Condensation from a Flowing Spray Cooling 92-080 nels with Conducting Blockages 192-012 Vapor onto Isothermal, Axisymmetric Laminar Coupled Flow Downstream of an Rough-Wall Turbulent Heat Transfer with Bodies 92-052 Asymmetric Sudden Expansion 192-047 Step-Wall Temperature Boundary Condi- Steady-State Post-Critical Heat Flux Heat Numerical Study of Natural Convection tions 192-011 Transfer to a Refrigerant 192-051 from Discrete Heat Sources in a Vertical Thermal Performance of Thermal Pad Con- Experimental Investigation of Transition Square Enclosure T92-016 tact Heat Exchangers 92-009 Boiling in Forced Convection 192-020 Thermal Gap Conductance: Effects of Gas Thermal Gap Conductance: Effects of Gas Analytical Two-Phase Flow Void Prediction Pressure and Mechanical Load 192-008 Pressure and Mechanical Load 192-008 Method 792-019 Forced Convection Heat Pipes Computational Heat Transfer Investigation of Mixed Convection About a Transient Behavior of Heat Pipes with Ther- Effect of Free Surface Shape on Combined Rotating Sphere by Holographic Interfer- mal Energy Storage Under Reversed- Thermocapillary and Natural Convection ometry 792-121 Pulsed Heat Loads 792-115 792-120 Enhanced Cooling of Electronic Components Transient Heat-Pipe Modeling: A Quasi- Iterative Temperature Calculation Method by Flow Oscillation 792-117 steady, Incompressible Vapor Model for Rectangular Sandwich Panel Fins Combined Conjugated Heat Transfer from a T92-097 792-116 Scattering Medium T92-088 Analytical Investigation of the Rewetting of Prediction of Radiative Transfer in Cylin- Second-Law Optimization of Forced Con- Grooved Surfaces T92-094 drical Enclosures with the Finite Volume vection of Non-Newtonian Fluids in Ducts Acceleration-Induced Depriming of External Method T92-103 T92-085 Artery Heat Pipes 192-087 Source Function Approach for Radiative Turbulent Transport Phenomena in a Chan- Heat Pipe and Surface Mass Transfer Cool- Heat Transfer Analysis T92-096 nel with Periodic Rib Turbulators ing of Hypersonic Vehicle Structures Turbulent Transport Phenomena in a Chan- 792-081 792-078 nel with Periodic Rib Turbulators Arc Heater Nozzle Heating Test with Hy- Fixed Conductance Heat Pipe Performance 792-081 drogen Combustion Products 792-071 with a Liquid Slug 192-077 Surface Cooling of Scramjet Engine Inlets Transient Solidification of a Binary Mixture Convective Flows in Enclosures with Vertical Using Heat Pipe, Transpiration, and Film in an Inclined Rectangular Cavity Temperature or Concentration Gradients Cooling 192-079 T92-053 192-061 Thermophoresis of a Radiating Aerosol in Filmwise Condensation from a Flowing Transient Behavior of Axially Grooved Heat Laminar Boundary-Layer Flow 192-076 Vapor onto Isothermal, Axisymmetric Pipes with Thermal Energy Storage Solution of the Parabolized Navier-Stokes Bodies 792-052 792-058 Equations Using Osher’s Upwind Scheme Heat Transfer in the Entrance Region of T92-069 Semicircular Ducts with Internal Fins Stagnation Point Nonequilibrium Radiative 192-048 Melting/ Solidification Heating and the Influence of Energy Laminar Coupled Flow Downstream of an Exchange Models 192-067 Asymmetric Sudden Expansion 192-047 Visualization of a Solidification Process in Transient Conjugated Heat Transfer From a Wall Heating Effects in Mixed Convection in Microgravity 92-122 Rectangular Hot Film T92-056 Vertical Annulus with Variable Properties Transient Thermal Analysis of Three Fast- Thermal-Structural Finite Element Analysis 792-045 Charging Latent Heat Storage Configura- Using Linear Flux Formulation 192-055 Transient Laminar Forced Convection From tions 192-021 Heat Transfer in the Entrance Region of a Circular Cylinder Using a Body-Fitted Rate Parameters for Coupled Vibration- Semicircular Ducts with Internal Fins Coordinate System 192-032 Dissociation in a Generalized SSH Ap- 92-048 Laminar Forced Convection in Circular Duct proximation 792-001 Laminar Coupled Flow Downstream of an Inserted with a Longitudinal Rectangular Asymmetric Sudden Expansion 192-047 Plate 92-029 Mixed Convection Numerical Solutions of Natural Convection Turbulent Heat Transfer in a Square Chan- in Enclosure with Boundary Condition nel with Staggered Discrete Ribs 192-027 Investigation of Mixed Convection About a Switching Method 192-044 Experimental Investigation of Transition Rotating Sphere by Holographic Interfer- Effects of g-Jitter on a Thermally Buoyant Boiling in Forced Convection T92-020 ometry 192-121 Flow 192-042 Effect of a Coaxial Jet on the Film-Cooling Effect of Free Surface Shape on Combined Discrete-Ordinates Solution of Radiative Performance Downstream of a Suddenly Thermocapillary and Natural Convection Transfer Equation in Nonaxisymmetric Expanded Swirling Flow 92-018 792-120 Cylindrical Enclosures 792-041 Periodically Fully Developed Flow in Chan- Measurements of Heat Transfer and Flow Radiative Transfer in Multidimensional En- nels with Conducting Blockages 192-012 Structure in Heated Vertical Channels closures with Specularly Reflecting Walls 792-118 192-034 Laminar Mixed Convection from a Uniform Transient Laminar Forced Convection From Heat Flux Horizontal Cylinder in a Cross- Heat Conduction a Circular Cylinder Using a Body-Fitted flow 192-046 Coordinate System 192-032 Analytical Investigation of the Rewetting of Natural Convection Heat Transfer in Rec- Two-Dimensional Effects in a Triangular Grooved Surfaces 92-094 tangular Cavities Partially Heated from Convecting Fin 192-025 Combined Conjugated Heat Transfer from a Below 192-043 Numerical Study of Natural Convection Scattering Medium T92-088 Laminar Mixed Convection in a Vertical from Discrete Heat Sources in a Vertical Fixed Conductance Heat Pipe Performance Tube with a Longitudinal Rectangle Insert Square Enclosure 792-016 with a Liquid Slug 192-077 792-013 760 J. THERMOPHYSICS, VOL. 6, NO. 4: 1992 INDEX Natural Convection Source Function Approech for Radiative Conduction—Radiation Interaction in Ab- Heat Transfer Analysis T92-096 sorbing, Emitting and Anisotropically Effect of Thermal Creep on Buoyancy- Backward Monte Carlo Modeling for Rocket Scattering Media with Variable Thermal Induced Flows in Low-Gravity 192-125 Plume Base Heating 792-091 Conductivity 92-084 Effect of Free Surface Shape on Combined Transient Combined Conduction and Ra- Fixed Conductance Heat Pipe Performance Thermocapillary and Natural Convection diation in Anisotropically Scattering with a Liquid Slug 192-077 792-120 Spherical Media T92-090 Transient Behavior of Axially Grooved Heat Combined Natural Convection and Radia- Combined Conjugated Heat Transfer from a Pipes with Thermal Energy Storage tion from Heated Cylinders Inside a Con- Scattering Medium T92-088 792-058 tainer 792-119 Boundary Heat Fluxes for Spectral Radia- Thermal Contacts in Transient States: A Free Convection About Vertical Needles tion from a Uniform Temperature Rec- New Model and Two Experiments Embedded in a Saturated Porous Medium Medium 792-086 192-057 T92-092 Conduction—Radiation Interaction in Ab- Analytical Solution for the Integral Contact Numerical Solutions of Natural Convection sorbing, Emitting and Anisotropically Line Evaporative Heat Sink 192-017 in Enclosure with Boundary Condition Scattering Media with Variable Thermal Thermal Performance of Thermal Pad Con- Switching Method 792-044 Conductivity 192-084 tact Heat Exchangers 792-009 Natural Convection Heat Transfer in Rec- Thermophoresis of a Radiating Aerosol in Thermal Gap Conductance: Effects of Gas tangular Cavities Partially Heated from Laminar Boundary-Layer Flow 192-076 Pressure and Mechanical Load 192-008 Below 792-043 Thermal Radiation Effects on a Shocked Effects of g-Jitter on a Thermally Buoyant Particle-Laden Gas 192-075 Flow 192-042 Stagnation Point Nonequilibrium Radiative Numerical Study of Natural Convection Heating and the Influence of Energy Thermal Modeling and Analysis from Discrete Heat Sources in a Vertical Exchange Models 792-067 Iterative Temperature Calculation Method Square Enclosure 792-016 Influence of Nonuniform Particle Temper- for Rectangular Sandwich Panel Fins Buoyant-Thermocapillary Flow with Non- ature on the Radiatively Active Particle T92-116 uniform Supra-Heating: II. Two-Phase Ignition 792-062 Practical Model for Molecular Contaminant Behavior 792-015 Discrete-Ordinates Solution of Radiative Deposition Kinetics 792-111 Buoyant-Thermocapillary Flow with Non- Transfer Equation in Nonaxisymmetric Spacecraft Thermal Energy Accommodation uniform Supra-Heating: I. Liquid-Phase Cylindrical Enclosures 192-041 from Atomic Recombination 92-110 Behavior 192-014 Two-Dimensional Radiative Transfer in a Analytic Solution of the Transient Behavior Natural Convection from Isothermal Plates Cylindrical Layered Medium with Reflect- of Radiation-Backscattering Heat Shields Embedded in Thermally Stratified Porous ing Interfaces 792-040 T92-104 Media T90-087 Effect of Linear-Anisotropic Scattering on Acceleration-Induced Depriming of External Spectral Emission from Cylindrical Plumes Artery Heat Pipes 792-087 792-039 Experimental Verification of Scaling Param- Nonintrusive Diagnostics Radiative Transfer in Multidimensional En- eters for Thermal Stratification 792-082 closures with Specularly Reflecting Walls Influence of Nonuniform Particle Temper- Bias in Emission Absorption Measurements T92-034 ature on the Radiatively Active Particle of Temperature and Atomic Density Determination of Optical Properties by Ignition 92-062 792-124 Two-Dimensional Scattering 792-031 Use of Membrane Transport in an Absorp- Visualization of a Solidification Process in Two-Dimensional Radiation in a Cylinder tion Thermal Transfer Cycle 792-059 Microgravity T92-122 with Spatially Varying Albedo 192-030 Transient Behavior of Axially Grooved Heat Correlation Transfer: Application of Radi- Finite Difference Solution for Transient Pipes with Thermal Energy Storage ative Transfer Solution Methods to Photon Cooling of a Radiating-Conducting Sem- 792-058 Correlation Problems T92-100 itransparent Layer 792-010 Transient Laminar Forced Convection From Rotational Temperature Measurements in an Doppler Shift Effects on Infrared Band a Circular Cylinder Using a Body-Fitted Arc Jet 792-093 Models 92-005 Coordinate System 792-032 Temperature Measurement of Reacting Two-Dimensional Effects in a Triangular Flowfield by Phase-Shifting Holographic Convecting Fin 792-025 Interferometry 792-672 Transient Thermal Analysis of Three Fast- Application of Laser Holographic Interfer- Radiation IntercBethweaen nSgurfeac es Charging Latent Heat Storage Configura- ometry to Temperature Measurements in Combined Natural Convection and Radia- tions 792-021 Buoyant Air Jets 792-060 tion from Heated Cylinders Inside a Con- Analytical Solution for the Integral Contact Two-Dimensional Radiative Transfer in a tainer 792-119 Line Evaporative Heat Sink 192-017 Cylindrical Layered Medium with Reflect- Bidirectional Reflectance and Specularity of Thermal Performance of Thermal Pad Con- ing Interfaces 792-040 Twelve Spacecraft Thermal Control Ma- tact Heat Exchangers T92-009 Determination of Optical Properties by terials 792-113 Three-Dimensional Thermal Structural Anal- Two-Dimensional Scattering 792-031 Practical Method for Calculating Radiation ysis of a Swept Cowl Leading Edge Sub- Incident upon a Panel in Orbit 192-028 jected to Skewed Shock-Shock Interference Heating 792-006 Monte Carlo Simulation of Vibrational Re- Radiation in Participating Media laxation in Nitrogen T92-002 Thermal Control Radiation Modeling with Direct Simulation Monte Carlo 792-107 Combined Natural Convection and Radia- Development of a Nonequilibrium Radiative tion from Heated Cylinders Inside a Con- Thermochaned mCheimicsalt Krineyti cs Heating Prediction Method for Coupled tainer T92-119 Flowfield Solutions T92-105 Transient Behavior of Heat Pipes with Ther- Spacecraft Thermal Energy Accommodation Analytic Solution of the Transient Behavior mal Energy Storage Under Reversed- from Atomic Recombination 92-110 of Radiation-Backscattering Heat Shields Pulsed Heat Loads 92-115 Vibration-Dissociation Coupling in Non- 792-104 Bidirectional Reflectance and Specularity of equilibrium Flows T92-109 Pzediction of Radiative Transfer in Cylin- Twelve Spacecraft Thermal Control Ma- Chlorine Utilization Study for Uniform- drical Enclosures with the Finite Volume terials 792-113 Droplet Singlet Delta Oxygen Generators Method 792-103 Thermal Control Coatings Performance at 192-074 Refractive Index Effects on Radiative Be- Near Geosynchronous Altitude 192-112 Thermochemical Nonequilibrium Flow Com- havior of a Heated Absorbing-Emitting Analytical Investigation of the Rewetting of putations of Flow Around the Aeroassist Layer T92-102 Grooved Surfaces T92-094 Flight Experiment 192-066 Correlation Transfer: Application of Radi- Transient Combined Conduction and Ra- Nonequilibrium Chemical and Radiation ative Transfer Solution Methods to Photon diation in Anisotropically Scattering Coupling, Part II: Results for AOTV Correlation Problems T92-100 Spherical Media T92-090 Flowfields T92-064 J. THERMOPHYSICS, VOL. 6, NO. 4: 1992 INDEX Nonequilibrium Chemical and Radiation Thermophysical Properties Rotational Temperature Measurements in an Coupling, Part I: Theory and Models Arce Jet 192-093 792-063 Normal Spectral Emittance of W-Re-HfC Thermophysical Properties of Lysozyme Modeling of an Argon Plasma in a Bound- and W-Re-ThO? Alloys 792-114 (Protein) Solutions T92-083 ary-Layer Flow T92-038 Bidirectional Reflectance and Specularity of Thermal Contacts in Transient States: A Diagonal Implicit Scheme for Computing Twelve Spacecraft Thermal Control Ma- New Modei and Two Experiments 192-057 Flows with Finite Rate Chemistry 192-037 terials T92-113 Effect of Linear-Anisotropic Scattering on Models of Energy-Exchange Mechanics Ap- Thermal Control Coatings Performance at Spectral Emission from Cylindrical Plumes plicable to a Particle Simulation of Reac- Near Geosynchronous Altitude 192-112 792-039 tive Flow 792-036 Practical Model for Molecular Contaminant Determination of Optical Properties by Monte Carlo Simulation of Vibrational Re- Deposition Kinetics T92-111 Two-Dimensional Scattering 792-031 laxation in Nitrogen 792-002 J. THERMOPHYSICS, VOL. 6, NO. 4: 1992 INDEX Author Index Ackerson, B. J., T92-100 Fivel, H. J., T92-071 Lago, V., T92-093 Reed, R. A., 792-005 Agarwal, R. K., T92-069 Fiveland, W. A., T92-034 Lai, F. C., T90-087 Reguigui, N. M., T92-040, T92-100 Ahmad, R. A., T92-046 Fletcher, L. S., T92-009 Lai, W. Z., 792-072 Ren, Z., T92-119 Ahmed, G. R., T92-016 Fote, A. A., T92-112 Lakshminarayanan, R., T92-026 Sakurai, H., T92-122 Anand, N. K., T92-012 France, D. M., T92-051 Lamine, A., 792-057 Satheesh, K. A., T92-073 Arai, Y., T92-122 Furukawa, M., T92-028 Landrum, D. B., T92-109 Schiller, D. N., T92-014, T92-015 Arimilli, R. V., 792-021 Gai, S. L., T92-070 Lasgorceix, P., T92-033, T92-093 Schindel, L., 792-022 Aung, W., T92-045, T92-118 Gally, T. A., T92-063, T92-064 Lau, S. C., 'T92-027 Schmitt, R. G., 792-075 Azar, K., T92-117 Garner, J. W., T92-011 Lazic, Z. R., T92-007 Schonberg, J. A., T92-017 Aziz, A., T92-025 Gau, C., T92-018, T92-045, T92-118 Lee, S., T92-101 Schwartz, S. H., T92-082 Baek, S. W., T92-062 George C. M., T92-051 Lee, T. S., T92-024 Sehmbey, M. S., T92-080 Bauman, L. E., T92-124 Gerbsch, R. A., T92-069 Li, H. Y., 792-030 Sharma, S. P., T92-001 Bejan, A., T90-087 Gilmore, M. R., T92-004 Liang, P. W., T92-056 Siegel, R., T92-010, T92-086, T92-102 Bilgen, E., T92-043 Glass, C. E., 792-006 Liou, T.-M., T92-081 Sirignano, W. A., T92-014, T92-015, Blackler, D., T92-009 Glassford, A. P. M., T92-111 Liu, J., 792-083 T92-042 Bobco, R. P., T92-077 Gnoffo, P. A., T92-067 Loth, J. L., 792-019 Smith, P. J., T92-041 Bose, T. K., 792-050 Gogos, G., T92-123 Lovrich, T. N., T92-082 Smith, T. F., 792-075 Bowman, W. J., T92-097 Gorla, R. S. R., T92-023 Lumpkin, F. E., III, 792-068 Song, S., T92-008 Butler, P. B., 792-075 Gousset, G., T92-093 Ma, A., T92-031 Spring, S. D., T92-049 Candler, G. V., T92-109 Haas, B. L., T92-036 Mackowski, D. W., T92-125 Spuckler, C. M., T92-102 Cao, W.-Z., T92-053 Haferman, J. L., 792-075 Marinelli, W. J., 792-110 Stovall. T. K., 792-021 Carleton, K. L., T92-110 Haji-Sheikh, A., T92-026 Martin, H. L., T92-097 Stoy, S. L., 192-071 Carlson, A. B., T92-065, T92-107 Hall, D. F., T92-112 Masson, B. S., T92-074 Sun, D. J., T92-061 Carlson, L. A., T92-063, T92-064 Hartung, L. C., T92-067, T92-105 McMillin, R. D., T92-027 Tanimoto, M., T92-122 Cayet, S., 792-033 Harvey, J. K., 792-004 Mehiman, B. P., T92-049 Taslim, M. E., 792-049 Celenligil, M. C., 792-004 Haskin, W. L., T92-059 Milos, F. S., T92-095 Tauber, M. E., T92-035 Cernogora, G., T92-093 Hasnaoui, M., T92-043 Minkowycz, W. J., T92-051 Taylor, R. P., T92-011 Chai, A. T., T92-061 Hassan, H. A., T92-002, T92-065, Mitcheltree, R. A., 792-067 Thynell, S. T., 792-039 Chamkha, A. J., T92-089 T92-106, T92-107 Modlin, J. M., T92-078, T92-079 Tieng, S., T92-060 Chang, K., T92-060 Hiers, R. E., III, 792-005 Moghadam, H. E., T92-045 Tieng, S. M., T92-072, T92-121 Chang, M., T92-058, T92-115 Hochard, L., T92-093 Moraga, N. O., T92-114 Truman, C. R., 92-074 Chang, W. S., T92-058, T92-059, Hochstein, J. 1., 792-082 Morgan, M., T92-115 Tsai, J. R., 792-030 T92-115 Holmes, L. A., T92-082 Morgan, M. J., T92-058 Tsao, B., T92-114 Chapman, D. R., T92-068 Hosni, M. H., T92-011 Moss, J. N., T92-002, T92-106 Tsau, F., 792-042 Chen, C., T92-032 Hosokawa, S., T92-122 Moyne, C., T92-057 Tseng, C., T92-084 Chen, G., T92-092 Howe, J. T., T92-104 Nakajima, K., T92-116 Tsou, F. K., T92-045 Chen, J., T92-013 Hrabar, J. P., 792-007 Naraghi, M. H. N., T92-096 Vandromme, D., T92-038 Chen, L., T92-020 Hsieh, S., 792-013, T92-029 Nelson, H. F., T92-091 VanNostrand, L., T92-047 Chen, S.-H., T92-081 Hsu, I. C., 792-031 Nguyen, H., 92-025 Vasseur, P., T92-043 Cheng, J., 792-029 Huan, J., T92-096 Nho, K., T92-008 Vedha-Nayagam, M., T92-125 Chow, L. C., 792-058, T92-080, Huang, J., T92-060 Nobbmann, U., T92-100 Vervisch, P., T92-038 792-115 Huang, T. M., 792-018 Okazaki, K., T92-073 Voisin, C., T92-033 Chu, H., 792-084, T92-090 Hughes, P. M. J., T92-103 Okumura, Y., T92-073 Vradis, G. C., 792-047 Chui, E. H., T92-103 Huo, W. M., T92-001 Olynick, D. P., T92-002, T92-106 Wang, G., T92-054 Chung, B. T. F., T92-088 Hug, R., 792-019 Orozco, J., T92-020 Wang, L. W., 192-061 Chung, C., T92-003 Hwang, J.-J., T92-081 Ozisik, M. N., T92-030 Watanabe, T., T92-122 Cipolla, J. W., Jr., 192-076 Imlay, S., 192-037 Pais, M. R., T92-080 Wayner, P. C., Jr., T92-017 Ishikawa, M., T92-122 Palmer, G., T92-056 Weng, L., T92-090 Iwasaki, A., T92-122 Palmer, G. E., 92-035 Wieting, A. R., T92-055 Jacobi, A. M., 792-052 Pandey, A. K., T92-055 Winn, R. C., 92-097 Cornelison, C. J., 792-104 Jacobson, D. L., 792-114 Pandey, A. K., T92-006 Woolhiser, C. C., 192-074 Cunnington, G. R., Jr., 792-031 Jamaluddin, A. S., 792-034, T92-041 Papadopoulos, P., T92-051 Wu, S., T92-032 Dagum, L., T92-108 Jeng, D., T92-003 Paraschivoiu, I., T92-044 Yan, A. C., T92-121 De Witt, K. J., 792-003 Ji, H.-C., 792-082 Park, C., T92-001 Yang, J., 792-054 Dechaumphai, P., T92-006, T92-055 Jia, G., T92-076 Paske, J. M., T92-051 Yang, L., T92-035 Degiovanni, A., T92-057 Jia, H., 792-123 Peng, C., T92-092 Yang, W., T92-083 Domingo, P., T92-038 Joe, W. S., T92-070 Peng, X. F., T92-087, T92-094 Yang, Y.-T., T92-032 Dominy, R. G., T92-004 Jumper, E. J., 792-074 Peterson, G. P., T92-009, T92-087, Yener, Y., T92-076 Dougherty, R. L., 192-040, T92-100 Kamei, S., T92-122 T92-094 Yih, K. A., 792-118 Drakes, J. A., T92-005 Kamotani, Y., T92-120 Platt, J., 792-120 Yovanovich, M. M., T92-008, Driftmyer, R., 92-022 Kassemi, M., T92-088 Polesky, S. P., T92-006 T92-016 Drolen, B. L., T92-077, T92-113 Kawai, S., T92-122 Pop, I., T90-087 Yu, J. S., 792-059 Dudeck, M., T92-093 Keith, T. G., Jr., T92-003 Poulikakos, D., 192-053, T92-085, Yuen, W. W., T92-031 Dudeck, M. A., T92-033 Kim, B. S. C., T92-071 T92-119 Zeng, T., T92-092 Ebadian, M. A., T92-048 Kim, S. H., 792-012 Qureshi, Z. H., 792-046 Zhang, H. Y., 192-048 Eberhar<'t, S., 792-037 Kudo, I., T92-122 Raithby, G. D., T92-103 Zhao, Z., T92-119 Elghobashi, S., T92-042 Kukreja, R. T., 792-027 Ramalingam, M. L., T92-114 Fang, Z., T92-044 Kulacki, F. A., T90-087 Rastogi, S. K., 792-085 J. THERMOPHYSICS, VOL. 6, NO. 4: 1992 INDEX Chronological Index 190-087 Natural Convection from Isothermal Plates Embedded 92-012 Periodically Fully DevelopeFldo w iinn Channels with in Thermally Stratified Porous Media. F. C. Lai, Colorado Conducting S. H. Kim and N. K. Anand, Texas State University; 1. Pop, University of Cluj, Romania; and F. A. A&M University (6, 1, p.91) Article Kulacki, Colorado State University (4, 4, p. 533) Technical Note 792-013 Laminar Mixed Convection in a Vertical Tube with a Technical Comment by Adrian Bejan, Duke University (6, 3, Longitudinal Insert. Jun-Dar Chen and Shou-Shing p. 574) Hsieh, National Sun Yat-Sen University, Taiwan, ROC (6, 1, Reply (6, 3, p. 575) p. 98) Article 792-001 Rate Parameters for Coupled Vibration-Dissociatioin n 192-014 Buoyant-Thermocapillary Flow with Nonuniform a Generalized SSH Approximation. Surendra P. Sharma, Supra-Heating: I. Liquid-Phase Behavior. David N. Schiller Winifred M. Huo and Chul Park, NASA Ames Research and William A. Sirignano, University of California, Irvine (6, 1, Center (6, 1, p.9) Article based on AIAA Paper 88-2714 p. 105) Article 192-002 Monte Carlo Simulation of Vibrational Relaxation in T92-015 Buoyant-Thermocapillary Flow with Nonuniform Nitrogen. David P. Olynick, North Carolina State University; Supra-Heating: II. Two-Phase Behavior. David N. Schiller and James N. Moss, NASA Langley Research Center; and H. A. William A. Sirignano, University of California, Irvine (6, 1, Hassan, North Carolina State University (6, 1, p.22) Article p. 113) Article based on AIAA Paper 90-1767 792-016 Numerical Study of Natural Convection from Discrete 792-003 Numerical Simulation of Rarefied Gas Flow Through a Heat Sources in a Vertical Square Enclosure. G. Refai Ahmed Slit. Chan-Hong Chung, Duen-Ren Jeng, Kenneth J. De Witt and M. M. Yovanovich, University of Waterloo, Canada (6, 1, and Theo G. Keith Jr., University of Toledo (6, 1, p. 27) Article p. 121) Article based on AIAA Paper 90-0256 based on AIAA Paper 90-1694 792-017 Analytical Solution for the Integral Contact Line Evanorative Heat Sink. J. A. Schonberg and P. C. Wayner Jr., 92-004 Flat-Ended Circular Cylinder in Hypersonic Rarefied Rensselaer Polytechnic Institute (6, 1, p. 128) Article Flow. J. K. Harvey, M. C. Celenligil, R.G. Dominy and M. R. Gilmore, Imperial College, England, UK (6, 1, p.35) Article based on AIAA Paper 89-1709 792-018 Effect of a Coaxial Jet on the Film-Cooling Per- formance Downstream of a Suddenly Expanded Swirling Flow. C. Gau and T. M. Huang, National Cheng Kung University, 192-005 Doppler Shift Effects on Infrared Band Models. J. A. Taiwan, ROC (6, 1, p. 135) Article Drakes, R. E. Hiers III and R. A. Reed, Sverdrup Technology, Inc. Arnold AFB (6, 1, p. 44) Article based on AIAA Paper 89-1678 T92-019 Analytical Two-Phase Flow Void Prediction Method. Reazul Huq, BWR Thermal Hydraulics, SIEMENS/KWU, FRG; and John L. Loth, West Virginia University (6, 1, p. 139) T92-006 Three-Dimensional Thermal Structural Analysis of a Article based on AIAA Paper 90-1738 Swept Cowl Leading Edge Subjected to Skewed Shock-Shock Interference Heating. Sandra P. Polesky, Pramote T92-020 Experimental Investigation of Transition Boiling in Dechaumphai and Christopher E. Glass, NASA Langley Re- Forced Convection. J. Orozco and L. Chen, University of search Center; and Ajay K. Pandey, Lockheed Engineering & Illinois at Chicago (6, 1, p. 145) Article Sciences Company (6, 1, p. 48) Article based on AIAA Paper 90-1710 792-021 Transient Thermal Analysis of Three Fast-Charging Latent Heat Storage Configurations. Therese K. Stovall, Oak 92-007 Modeling the Postcure Regime of Ablative Composite Ridge National Laboratory; and Rao V. Arimilli, University of Materials. Zivorad R. Lazic and Jova P. Hrabar, Military Tennessee (6, 1, p. 152) Article Technical Institute, Yugoslavia (6, 1, p.55) Article T92-022 Surface Cooling by Transpiration of a Freezing Liquid. 192-008 Thermal Gap Conductance: Effects of Gas Pressure L. Schindel and R. Driftmyer, Naval Surface Warfare Center and Mechanical Load. S. Song, JBM; M. M. Yovanovich and (6, 1, p. 158) Technical Note based on AIAA Paper 89-1774 K. Nho, University of Waterloo, Canada (6, 1, p. 62) Article based on AIAA Paper 89-0429 92-023 Microstructure Effects on the Conjugate Heat Transfer Along a Vertical Circular Pin. Rama Subba Reddy Gorla, 792-009 Thermal Performance of Thermal Pad Contact Heat Cleveland State University (6, 1, p. 160) Technical Note Exchangers. G. P. Peterson and L. S. Fletcher, Texas A&M University; and David Blackler, Rockwell International Cor- T92-024 Mixed Convection of Low Prandtl Number Fluid in the poration (6, 1, p.69) Article based on AIAA Paper 91-0364 Annuli of Rotating Cylinders. T. S. Lee, National University of Singapore (6, 1, p. 162) Technical Note 792-010 Finite Difference Solution for Transient Cooling of a Radiating-Conducting Semitransparent Layer. Robert Siegel, T92-025 Two-Dimensional Effects in a Triangular Convecting NASA Lewis Research Center (6, 1, p.77) Article Fin. A. Aziz and H. Nguyen, Gonzaga University (6, 1, p. 165) Technical Note 92-011 Rough-Wall Turbulent Heat Transfer with Step-Wall Temperature Boundary Conditions. Robert P. Taylor, M. H. T92-026 Entrance Heat Transfer in Isosceles and Right Tri- Hosni, James W. Garner and Hugh W. Coleman, Mississippi angular Ducts. R. Lakshminarayanan, Ketema Inc.; and A. State University (6, 1, p. 84) Article based on AIAA Paper Haji-Sheikh, University of Texas at Arlington (6, 1, p. 167) 90-1501 Technical Note 764 J. THERMOPHYSICS, VOL. 6, NO. 4: 1992 INDEX 192-027 Turbulent Heat Transfer in a Square Channel with 92-042 Effects of g-Jittero n a Thermally Buoyant Flow. F. Staggered Discrete Ribs. S.C. Lau, R. T. Kukreajnda R . D. Tsau, S. Elghobashi and W. A. Sirignano, University of McMillin, Texas A&M University (6, 1, p. 171) Technical Note California at Irvine (6, 2, p. 246) Article based on AIAA Paper 90-0653 192-028 Practical Method for Calculating Radiation Incident upon a Panel in Orbit. Masao Furukawa, National Space 92-043 Natural Convection Heat Transfer in Rectangular Development Agency, Japan (6, 1, p. 173) Technical Note Cavities Partially Heated from Below. M. Hasnaoui, E. Bilgen and P. Vasseur, Ecole Polytechnique de Montréal, Canada (6, 2, 92-029 Laminar Forced Convection in Circular Duct Inserted p. 255) Article with a Rectangular Plate. Jun-Dar Cheng and Shou-Shing Hsieh, National Sun Yat-Sen University, Taiwan, 192-044 Numerical Solutions of Natural Convection in Enclo- ROC 6, 1, p. 177) Technical Note sure with Condition Switching Method. Z. Fang and I. Paraschivoiu, Ecole Polytechnique de Montréal, Canada (6, 2, 92-630 Two-Dimensional Radiation in a Cylinder with Spa- p. 265) Article tially Varying Albedo. H. Y. Li, M. N. Ozisik and J. R. Tsai, North Carolina State University (6, 1, p. 180) Technical Note T92-045 Wall Heating Effects in Mixed Convection in Vertical Annulus with Variable F. K. Tsou, Drexel Univer- 192-031 Determination of Optical Properties by Two-Dimen- sity; Win Aung and Hamid E. Moghadam, Howard University; sional Scattering. W. W. Yuen and A. Ma, University of and C. Gau, National Cheng Kung University, Taiwan, ROC (6, California at Santa Barbara; 1. C. Hsu and G. R. Cunnington 2, p. 273) Article Jr., Lockheed Missiles & Space Company, Inc. (6, 1, p. 182) Technical Note based on AIAA Paper 90-1719 T92-046 Laminar Mixed Convection from a Uniform Heat Flux Horizontal Cylinder in a Crossflow. R. A. Ahmad, Thiokol 192-032 Transient Laminar Forced Convection From a Circu- Corporation; and Z. H. Qureshi, Westinghouse Savannah River lar Cylinder Using a Body-Fitted Coordinate System. Yue-Tzu Company (6, 2, p. 277) Article based on AIAA Paper 91-0383 Yang, Cha’o-Kuang Chen and Sang-Ru Wu, National Cheng- Kung University, Taiwan, ROC (6, 1, p. 184) Technical Note 192-047 Laminar Coupled Flow Downstream of an Asymmetric 792-633 Electron T and Electron Density in a Sudden Expansion. George C. Vradis and Lara VanNostrand, Rarefied Air Plasma Jet. M. A. Dudeck, P. Lasgorceix, C. Polytechnic University (6, 2, p.288) Article based on AIAA Voisin and S. Cayet, Centre National de la Recherche Paper 91-0162 Scientifique, France (6, 1, p. 188) Technical Note T92-048 Heat Transfer in the Entrance Regiono f Semicircular 792-634 Radiative Transfer in Multidimensional Enclosures Ducts with Internal Fins. H. Y. Zhang and M. A. Ebadian, with Specularly Reflecting Walls. A. S. Jamaluddin and W. A. Florida International University (6, 2, p. 296) Article Fiveland, Babcock & Wilcox (6, 1, p. 190) Technical Note T92-049 Experimental Investigation of Film Cooling Effec- 792-635 Earth Ai Entry Studies for Manned Mars tiveness for Slots of Various Exit Geometries. M. E. Taslim, Missions. M. E. Tauber and G. E. Palmer, NASA Ames Northeastern University; S. D. Spring and B. P. Mehiman, GE Research Center; and Lily Yang, Sterling Software (6, 2, Aircraft Engines (6, 2, p. 302) Article based on AIAA Paper p. 193) Article based on AIAA Paper 90-1699 90-2266 792-036 Models of Energy-Exchange Mechanics Applicable to a Particle Simulation of Reactive Flow. Brian L. Haas, Stanford T92-050 Laminar Impingement Jet Mach Number and Tem- University (6, 2, p. 200) Article based on AIAA Paper 90-1749 Effects on Heat Transfer. Tarit Kumar Bose, Indian Institute of Technology, India (6, 2, p. 308) Article 7192-037 Diagonal Implicit Scheme for Computing Flows with T92-051 Steady-State Post-Critical Heat Flux Heat Transfer to Finite Rate Chemistry. Scott Eberhardt, University of Wash- a Refrigerant. J. M. Paske, P. Papadopoulos, C. M. George, ington; and Scott Imlay, Amtech Engineering, Inc. (6, 2, p. 208) D. M. France and W. J. Minkowycz, University of Illinois at Article based on AIAA Paper 90-1577 Chicago (6, 2, p. 314) Article 792-038 Modeling of an Argon Plasma in a Boundary-Layer 92-052 Filmwise Condensation from a Flowing Vapor onto Flow. Pascale Domingo, Dany Vandromme and P. Vervisch, Isothermal, Axisymmetric Bodies. Anthony M. Jacobi, Johns CORIA—URA, France (6, 2, p.217) Article Hopkins University (6, 2, p.321) Article 192-439 Effect of Linear-Anisotropic Scattering on Spectral 792-053 Transient Solidification of a Binary Mixture in an Emission from Cylindrical Plumes. S. T. Thynell, Pennsylvania Inclined R Cavity. W.-Z. Cao and D. Poulikakos, State University (6, 2, p. 224) Article based on AIAA Paper University of Illinois at Chicago (6, 2, p. 326) Article 90-0137 92-054 Convective Thermal Ignition of an Individual Poly- 192-040 Two-Dimensional Radiative Transfer in a Cylindrical methyimethacrylate Particle. Gwo-Guang Wang and Jing- Layered Medium with Reflecting Interfaces. N. M. Reguigui Tang Yang, National Tsing Hua University, Taiwan, ROC (6, 2, and R. L. Dougherty, Oklahoma State University (6, 2, p. 232) p. 333) Article Article based on AIAA Paper 90-1779 192-055 Thermal-Structural Finite Element Analysis Using 192-041 Discrete-Ordinates Solution of Radiative Transfer Linear Flux Formulation. Ajay K. Pandey, Lockheed Engi- Equation in Nonaxisymmetric Enclosures. A. S. neering & Sciences Company; Pramote Dechaumphai and Jamaluddin, Babcock & Wilcox, Alliance Research Center; and Allan R. Wieting, NASA Langley Research Center (6, 2, p. 341) P. J. Smith, University of Utah (6, 2, p. 242) Article Article based on AIAA Paper 89-1224 CP891 J. THERMOPHYSICS, VOL. 6, NO. 4: 1992 INDEX 765 92-056 Transient Conjugated Heat Transfer From a Rectan- 92-069 Solution of the Parabolized Navier-Stokes Equations gular Hot Film. P. W. Liang and K. D. Cole, University of Using Osher’s Upwind Scheme. R. A. Gerbsch and R. K. Nebraska-Lincoln (6, 2, p. 349) Article Agarwal, McDonnell Douglas Research Laboratories (6, 3, p. 426) Article based on AIAA Paper 90-0392 92-057 Thermal Contacts in Transient States: A New Model and Two Experiments. Alain Degiovanni, Anne-Sophie 192-070 Laminar Heat Transfer to Blunt Cones in High- Lamine and Christian Moyne, Unité de Recherche Associée, Enthalpy Hypervelocity Flows. S. L. Gai, University College, France (6, 2, p. 356) Article based on AIAA Paper 90-0542 University of New South Wales, Australia; and W. S. Joe, Australian National University (6, 3, p. 433) Article 92-058 Transient Behavior of Axially Grooved Heat Pipes with Thermal Energy Storage. Ming-Jr Chang and Louis C. Chow, 192-07A1r c Heater Nozzle Heating Test with Hydrogen University of Kentucky; Won Soon Chang and Micheal J. Combustion Products. Bernard S. C. Kim, Stanley L. Sioy and Morgan, Wright Research and Development Center, Wright- Herschel J. Fivel, McDonnell Douglas Missile Systems Com- Patterson AFB (6, 2, p. 364) Article based on AIAA Paper pany (6, 3, p. 439) Article based on AIAA Paper 91-1413 90-1754 T92-072 Temperature Measurement of Reacting Flowfield by 92-059 Use of Membrane Transport in an Absorption Thermal Phase-Shifting Interferometry. Sheng Mao Tieng Transfer Cycle. J.S. Yu, West Virginia Institute of Technology; and Wen Zen Lai, National Cheng Kung University, Taiwan, W. S. Chang and W. L. Haskin, Wright Laboratory, Wright- ROC (6, 3, p.445) Article based on AIAA Paper 91-1388 Patterson AFB (6, 2, p.371) Article based on AIAA Paper 90-1683 792-073 Arc Transition and Growth of Big-Arcs in Magne- tohydrodynamics Generator Channels. K. A. Satheesh, Y. T92-060 Application of Laser Holographic Interferometry to Okumura and K. Okazaki, Toyohashi University of Technology, Temperature Measurements in Buoyant Air Jets. Keh-Chin Japan (6, 3, p. 452) Article Chang, Jim-Ming Huang and Sheng-Mao Tieng, National Cheng-Kung University, Taiwan, ROC (6, 2, p. 377) Technical 792-074 Chiorine Utilization Study for Uniform-Droplet Singlet Note Delta Oxygen Generators. Craig C. Woolhiser, Phillips Laboratory, Kirtland AFB; C. Randall Truman, University of 192-061 Convective Flows in Enclosures with Vertical Tem- New Mexico; Eric J. Jumper, University of Notre Dame; and or Concentration Gradients. L.W . Wang, Yuan-Ze Bruce S. Masson, Phillips Laboratory, Kirtland AFB (6, 3, Institute of Technology, Taiwan, ROC; A. T. Chai, NASA p. 460) Article based on AIAA Paper 90-1576 Lewis Research Center; and D. J. Sun, National Cheng Kung University, Taiwan, ROC (6, 2, p. 379) Technical Note based 792-075 Thermal Radiation Effects on a Shocked Particle- on AIAA Paper 89-0069 Laden Gas. J. !.. Haferman, R. G. Schmitt, T. F. Smith and P. B. Butler, University of Iowa (6, 3, p. 467) Article 92-062 Influence of Nonuniform Particle Temperature on the Radiatively Active Particle Ignition. Seung Wook Back, Korea 192-076 Thermophoresis of a Aerosol in Laminar Advanced Institute of Science and Technology (6, 2, p. 382) Boundary-Layer Flow. G. Jia, J. W. Cipolla Jr. and Y. Yener, Technical Note based on AIAA Paper 91-0483 Northeastern University (6, 3, p. 476) Article 192-063 Nonequilibrium Chemical and Radiation Coupling, Part 192-077 Fixed Conductance Heat Pipe Performance with a I: Theory and Models. Leland A. Carlson and Thomas, A. Liquid Slug. R. P. Bobco and B. L. Drolen, Hughes Aircraft Gally, Texas A&M University (6, 3, p. 385) Article based on Company (6, 3, p. 483) Article based on AIAA Paper 90-1794 AIAA Paper 91-0569 192-078 Heat Pipe and Surface Mass Transfer Cooling of 792-064 N Chemical and Radiation Coupling, Part Hypersonic Vehicle Structures. Gene T. Colwell, Georgia Il: Results for AOTV Flowfields. Thomas A. Gally and Leland Institute of Technology; and James M. Modlin, U. S. Army A. Carlson, Texas A&M University (6, 3, p. 392) Article based Strategic Defense Command (6, 3, p. 492) Article on AIAA Paper 91-0569 92-079 Surface Cooling of Scramjet Engine Inlets Using Heat 192-065 Direct Simulation of Re-Entry Flows with Ionization. Pipe, Transpiration, and Film Cooling. James M. Modlin, U. S. Ann B. Carlson, NASA Langley Research Center; and H. A. Army Strategic Defense Command; and Gene T. Colwell, Hassan, North Carolina State University (6, 3, p. 400) Article Georgia Institute of Technology (6, 3, p. 500) Article based on AIAA Paper 90-0144 92-080 Effect of Surface Material and Surface Characteristics in Evaporative Spray Cooling. M. S. Sehmbey, 792-066 Thermochemical Nonequilibrium Flow Computations of Flow Around the Aeroassist Grant Palmer, M. R. Pais and L. C. Chow, University of Kentucky (6, 3, NASA Ames Research Center (6, 3, p. 405) Article based on p. 505) Article based on AIAA Paper 90-1729 AIAA Paper 90-1702 792-081 Turbulent Phenomena in a Channel with 192-067 Stagnation Point Nonequilibrium Radiative Heating Periodic Rib Turbulators. T.-M. Liou, J.-J. Hwang and S.-H. and the Influence of ModLein lC. sHar,tun g, Chen, National Tsing Hua University, Taiwan, ROC (6, 3, Robert A. Mitcheltree and Peter A. Gnoffo, NASA Langley p. 513) Article Research Center (6, 3, p. 412) Article based on AIAA Paper 91-0571 192-082 Experimental Verification of Scaling Parameters for Thermal Stratification. H.-C. Ji, Washington University; S. H. 792-068 Accuracy of the Burnett Equations for Hypersonic Real Schwartz, California State University; T. N. Lovrich, Gas Flows. Forrest E. Lumpkin III, NASA Ames Research McDonnell Douglas Corporation; J. 1. Hochstein, Memphis Center; and Dean R. Chapman, Stanford University (6, 3, State University; and L. A. Holmes, Modesto College (6, 3, p. 419) Article based on AIAA Paper 91-0771 p. 522) Article 766 J. THERMOPHYSICS, VOL. 6, NO. 4: 1992 INDEX 192-083 Thermophysical Properties of Lysozyme (Protein) T92-100 Correlation Transfer: Application of Radiative Transfer Solutions. Jiaching Liu and Wen-Jei Yang, University of Solution Methods to Photon Correlation Problems. B. J. Michigan (6, 3, p. 531) Article Ackerson, R. L. Dougherty, N. M. Reguigui and U. Nobbmann, Oklahoma State University (6, 4, p. 577) Article 92-084 Conduction—Radiation Interaction in Absorbing, Emit- based on AIAA Paper 91-1433 ting and Anisotropically Scattering Media with Variable Thermal Conductivity. Hsin-Sen Chu and Chung-Jen Tseng, T92-101 Dependent Scattering by Parallel Fibers: Effects of National Chiao Tung University, Taiwan, ROC (6, 3, p. 537) Multiple Scattering and Wave Interference. Siu-Chun Lee, Technical Note Applied Science Laboratory, Inc. (6, 4, p. 589) Article based on AIAA Paper 91-1398 792-085 Second-Law Optimization of Forced Convection of Non-Newtonian Fluids in Ducts. S. K. Rastogi and D. 92-102 Refractive Index Effects on Radiative Behavior of a Poulikakos, University of Illinois at Chicago (6, 3, p. 540) Heated Absorbing-Emitting Layer. C. M. Spuckler and R. Technical Note Siegel, NASA Lewis Research Center (6, 4, p.596) Article 192-086 Boundary Heat Fluxes for Spectral Radiation from a T92-103 Prediction of Radiative Transfer in Cylindrical Enclo- Uniform Temperature Rectangular Medium. Robert Siegel, sures with the Finite Volume Method. E. H. Chui and G. D. NASA Lewis Research Center (6, 3, p. 543) Technical Note Raithby, University of Waterloo, Canada; and P. M. J. Hughes, Energy Research Laboratories, Canada (6, 4, p. 605) Article 192-087 Acceleration-Induced Depriming of External Artery Heat Pipes. X. F. Peng and G. P. Peterson, Texas A&M 92-104 Analytic Solution of the Transient Behavior of Radi- University (6, 3, p. 546) Technical Note ation-Backscattering Heat Shields. Charles J. Cornelison and John T. Howe, NASA Ames Research Center (6, 4, p. 612) Article based on AIAA Paper 91-1322 192-088 Combined Conjugated Heat Tranfrosm af Sceattreri ng Medium. M. Kassemi, NASA Lewis Research Center; and B. T92-105 Development of a Nonequilibrium Radiative Heating T. F. Chung, University of Akron (6, 3, p. 548) Technical Note Prediction Method for Coupled Flowfield Solutions. Lin C. Hartung, NASA Langley Research Center (6, 4, p. 618) Article 792-089 Convective Heat Transfer of a Particulate Suspension. based on AIAA Paper 91-1406 Ali J. Chamkha, Fleetguard, Inc. (6, 3, p. 551) Technical Note T92-106 Monte Carlo Simulation of Nonequilibrium Shock 192-090 Transient Combined Conduction and Radiation in Fronts. David P. Olynick, North Carolina State University; Anisotropically Scattering Spherical Media. Hsin-Sen Chu and James N. Moss, NASA Langley Research Center; and H. A. Ling-Chia Weng, National Chiao Tung University, Taiwan, Hassan, North Carolina State University (6, 4, p. 626) Article ROC (6, 3, p. 553) Technical Note based on AIAA Paper 91-1341 92-091 Backward Monte Carlo Modeling for Rocket Plume T92-107 Radiation Modeling with Direct Simulation Monte Base Heating. H. F. Nelson, University of Missouri—Rolla (6, Carlo. Ann B. Carlson, NASA Langley Research Center; and 3, p. 556) Technical Note H. A. Hassan, North Carolina State University (6, 4, p. 631) Article based on AIAA Paper 91-1409 92-092 Free ConvecAbotuti Voertnica l Needles Embedded in T92-108 Three-Dimensional Direct Particle Simulation on the a Saturated Porous Medium. Chunmei Peng, Taofang Zeng Connection Machine. Leonardo Dagum, NASA Ames Re- and Gang Chen, Huazhong University of Science and Tech- search Center (6, 4, p.637) Article based on AIAA Paper nology, PRC (6, 3, p. 558) Technical Note 91-1365 92-093 Rotational Temperature Measurements in an Arc Jet. T92-109 Vibration-Dissociation Coupling in Nonequilibrium G. Cernogora, G. Gousset and L. Hochard, Université Flows. D. Brian Landrum and Graham V. Candler, North Paris-Sud, France; M. Dudeck, P. Lasgorceix and V. Lago, Carolina State University (6, 4, p. 643) Article based on AIAA Centre National de la Recherche Scientifique, France (6, 3, Paper 91-0466 p. 561) Technical Note T92-110 Spacecraft Thermal Energy Accommodation from 192-094 Analytical Investigation of the Rewetting of Grooved Atomic Recombination. Karen L. Carleton and William J. Surfaces. X. F. Peng and G. P. Peterson, Texas A&M Marinelli, Physical Sciences, Inc. (6, 4, p. 650) Article based on University (6, 3, p. 563) Technical Note AIAA Paper 91-1337 792-095 Flowfield Analysis for High-Enthalpy Arc Heaters. T92-111 Practical Model for Molecular Contaminant Deposition Frank S. Milos, NASA Ames Research Center (6, 3, p. 565) Kinetics. A. P. M. Glassford, Lockheed Missiles & Space Technical Note based on AIAA Paper 91-1384 Company (6, 4, p. 656) Article T92-096 Source Function Approach for Radiative Heat Transfer 192-112 Thermal Control Coatings Performance at Near J. Huan and M. H. N. Naraghi, Manhattan College Geosynchronous Altitude. D. F. Hall and A. A. Fote, The (6, 3, p. 568) Technical Note Aerospace Corporation (6, 4, p. 665) Article based on AIAA Paper 91-1325 92-097 Transient Heat-Pipe Modeling: A Quasisteady, In- compressible Vapor Model. W. Jerry Bowman, U. S. Air Force 92-113 Bidirectional Reflectance and of Twelve Institute of Technology, Wright-Patterson AFB; Robert C. Spacecraft Thermal Control Materials. B. L. Drolen, Hughes Winn and Harold L. Martin, U. S. Air Force Academy (6, 3, Aircraft Company (6, 4, p. 672) Article based on AIAA Paper p. 571) Technical Note 91-1326