Table Of Content

JOURNAL OF PROPULSION AND POWER Volume 18, No. 6, November—December 2002 2002 Journal of Propulsion and Power Index How to Use the Index In the Subject Index, pages 1313-1318, each technical paper is listed under a maximum of three appropriate headings. Note the locating number in boldface type preceding each paper title, and use that number to find the paper in the Chronological Index. The Author Index, pages 1319 and 1320, lists all authors associated with a given technical paper. The locating numbers are identical to those in the Subject Index. The Chronological Index, pages 1321-1327, also lists all papers by their locating numbers. This listing contains titles, authors and their affiliations, and volume, issue number, and page where the paper appeared. It also gives the AIAA paper number, if any, on which the article was based, as well as the ISBN number if the paper was published in a bound collection of meetings papers. Comments, Replies, and Errata are listed directly beneath the paper to which they refer. If the paper to which they refer was published prior to 2002, that paper also will appear in both the Subject and Chronological Indexes. Authors of Comments also are listed in the Author Index. Subject Index Aircraft Technology, Conventional, STOL/VTOL/STOVL B02-046 Numerical Simulations of the Slinga- tron STOL/VTOL B02-094 Geometric Evaluation of Axisymmet- B02-044 Slingatron: A High Velocity Rapid Fire ric Thrust-Vectoring Nozzles for Aerodynamic Aerodynamics Performance Predictions Sling B02-069 Study of the Phase-Lock Phenomenon B02-086 Aerodynamic Optimization of Turbo- for a Circular Slingatron machinery Cascades Using Euler/Boundary- Energy Layer Coupled Genetic Algorithms Solar Power Alternate Fuels B02-171 Effects of End Wall Geometry and B02-153 Mass-Based Optimization of Thermal Stacking on Supersonic Turbine Performance B02-110 Asphaltic Thermoplastic Propellants Management and Power Systems for Space B02-027 Equation for Additive Drag Coefficient Fuel Cells Applications at Static Conditions B02-029 Optimal Three-Dimensinal Nozzle B02-064 Recent GRC Aerospace Technologies Stirling Engine Shape Design Using CFD and Parallel Simulat- Applicable to Terrestrial Energy Systems B02-092 Experimental Study of a 3-kW Stirling ed Annealing Fuel Economy Engine B02-012 Shock Fitting a Transonic Cascade B02-064 Recent GRC Aerospace Technologies Solution into an Inverse Design Technique B02-032 Development of Advanced Industrial Applicable to Terrestrial Energy Systems Furnace Using Highly Preheated Combustion B02-066 Transonic Rotor Blade Pressure Mea- surement Using Flourescent Paints Air Thermoelectric Aeroelasticity and Aeroservoelasticity Magnetohydrodynamic Power Generation B02-031 Multilevel Analysis of Pulsed Detona- B02-057 Magnetohydrodynamic Power Extrac- tion Engines B02-107 Computational-Fluid-Dynamics Inves- tion from Cold Hypersonic Airflows with Exter- tigation of Aeromechanics nal Ionizers Fluid Dynamics Noise Nuclear Fission Aeroacoustics B02-0% High-Intensity Sound Absorption at an B02-068 Project Orion and Future Prospects for B02-011 Active Control of Discrete-Frequency Orifice with Bias Flow Nuclear Pulse Propulsion Noise Generated by Rotor-Stator Interactions Powerplant Integration Reciprocating Machinery B02-042 Effect of Nozzle Cavity on Resonance in Large SRM: Theoretical Modeling B02-075 High-Pressure Steam Flow in Turbine B02-044 Slingatron: A High Velocity Rapid Fire B02-006 Experimental Investigation of Limit- Bypass Valve System Part |: Valve Flow Sling Cycle Oscillations in an Unstable Gas Turbine Rotating Machinery Combustor Safety B02-096 High-Intensity Sound Absorption at an B02-011 Active Control of Discrete-Frequency B02-038 Leak Fault Detection of Liquid Rocket Orifice with Bias Flow Noise Generated by Rotor-Stator Interactions Engine Based on Strong Tracking Filter B02-074 Development of High-Performance Boundary Layers and Heat Transfer— Airfoils for Axial Flow Compressors Using Evo- Simulation Laminar lutionary Computation B02-038 Leak Fault Detection of Liquid Rocket B02-147 Experimental Investigation of End- B02-119 Control of Low-Pressure Turbine Sep- Engine Based on Strong Tracking Filter Wall Flow in Turbine Rotor aration Using Vortex-Generator Jets 4 1313 1314 J. PROPULSION, VOL. 18, NO. 6: 2002 INDEX B02-031 Multilevel Analysis of Pulsed Detona- B02-035 Computations of Axisymmetric Plug- B02-004 Numerical Simulation of the Ram tion Engines Nozzle Flowfields: Flow Structures and Thrust Accelerator Using a New Chemical Kinetics Performance Mechanism Boundary Layers and Heat Transfer— B02-135 Effect of Integration of Scramjet into B02-023 Reduced Chemical Kinetic Mecha- Turbulent Airframe on Engine Performance and Payload nisms for Hydrocarbon Fuels B02-031 Multilevel Analysis of Pulsed Detona- 802-094 Geometric Evaluation of Axisymmet- B02-169 Interaction of Decaying Freestream tion Engines ric Thrust-Vectoring Nozzles for Aerodynamic Turbulence with a Moving Shock Wave: Pres- B02-041 Numerical Predictions of Channel Performance Predictions sure Field Flows with Fluid Injection Using Reynolds- B02-093 Improved Mean-Flow Solution for B02-163 Thermochemistry of Species Produced Stress Model Slab Rocket Motors with Regressing Walls from Monomethylhydrazine in Propulsion and B02-081 Solid-Fuel Regression Rate Behavior B02-002 Integrated Design and Analysis of Space-Related Applications of Vortex Hybrid Rocket Engines Intakes and Nozzles in Air-Breathing Engines B02-087 When Do Open-Loop Strategies for B02-158 Motor and Plume Particle Size Predic- Combustion Control Work? Boundary-Layer Stability and Transition tion in Solid-Propellant Rocket Motors B02-041 Numerical Predictions of Channel B02-036 Numerical Simulation of Side Loads in Separated Flows Flows with Fluid Injection Using Reynolds- an Ideal Truncated Nozzle B02-078 Appearance of Restricted Shock Sepa- Stress Model B02-029 Optimal Three-Dimensinal Nozzle ration in Rocket Nozzles Shape Design Using CFD and Parallel Simulat- B02-119 Control of Low-Pressure Turbine Sep- Computational Fluid Dynamics ed Annealing aration Using Vortex-Generator Jets B02-086 Aerodynamic Optimization of Turbo B02-079 Performance Analysis of Secondary B02-036 Numerical Simulation of Side Loads in machinery Cascades Using Euler/Boundary- Gas Injection into a Conical Rocket Nozzle an Ideal Truncated Nozzle Layer Coupled Genetic Algorithms B02-146 Study of Flow Separation in Truncated B02-146 Study of Flow Separation in Truncated B02-151 Analysis and Application — of Ideal Contour Nozzle Ideal Contour Nozzle Chorochronic Periodicity in Turbomachinery Rotor/Stator Interaction Computations Jets, Wakes, and Viscid-Inviscid Flow Shock Waves and Detonations B02-122 Automated Design Optimization of a Interactions B02-169 Interaction of Decaying Freestream Three-Dimensional S-Shaped Subsonic Diffuser B02-108 Facility Effects on Performance Mea- Turbulence with a Moving Shock Wave: Pres- B02-040 Characteristic Analysis of Flow- surements of Micropropulsion Systems that Uti- sure Field Induced Vibrations on Inducer of Oxygen Pump lize Gas Expansion B02-107 Computational-Fluid-Dynamics Inves- B02-010 Flow Control via Rotor Trailing Edge Subsonic Flow tigation of Aeromechanics Blowing in a Rotor/Stator Axial Compressor B02-122 Automated Design Optimization of a B02-074 Development of High-Performance B02-079 Performance Analysis of Secondary Three-Dimensional S-Shaped Subsonic Diffuser Airfoils for Axial Flow Compressors Using Evo- Gas Injection into a Conical Rocket Nozzle lutionary Computation Transonic Flow B02-171 Effects of End Wall Geometry and Multiphase Flows Stacking on Supersonic Turbine Performance B02-129 A PIV Investigation of Rotor-IGV B02-002 Integrated Design and Analysis of B02-022 Flow Past Stationary Spherical Parti- Interactions in a Transonic Compressor Intakes and Nozzles in Air-Breathing Engines cles with Streamwise Velocity Fluctuation B02-066 Transonic Rotor Blade Pressure Mea- B02-052 Linear Deterministic Source Terms for B02-161 Modeling Cavitating Venturi Flows surement Using Flourescent Paints 802-137 Numerical Simulation of a Pulse Deto- Hot Streak Simulations nation Engine with Hydrogen Fuels Unsteady Flows B02-161 Modeling Cavitating Venturi Flows B02-030 Propagation of Acoustic Waves in a B02-072 Multiobjective Optimization of Rocket B02-129 A PIV Investigation of Rotor-IGV Two-Phase Vaporizing Mixture Engine Pumps Using Evolutionary Algorithm Interactions in a Transonic Compressor B02-157 Numerical Reconstruction of Ejector Plasmadynamics and MHD B02-011 Active Control of Discrete-Frequency Rocket Experimental Tests Noise Generated by Rotor-Stator Interactions B02-004 Numerical Simulation of the Ram B02-150 Advanced Performance Modeling of B02-168 Airfoil Row/Wake Interactions in a Accelerator Using a New Chemical Kinetics Experimental Laser Lightcraft High-Speed Axial Compressor Mechanism B02-017 Design of a Fusion Propulsion Sys- B02-151 Analysis and Application of B02-029 Optimal Three-Dimensinal Nozzle tem—Part |: Gigawatt-Level Magnetoplasma- Chorochronic Periodicity in Turbomachinery Shape Design Using CFD and Parallel Simulat- dynamic Source Rotor/Stator Interaction Computations ed Annealing B02-028 Intercusp Electron Transport in an B02-107 Computational-Fluid-Dynamics Inves- B02-079 Performance Analysis of Secondary NSTAR-Derivative lon Thruster tigation of Aeromechanics Gas Injection into a Conical Rocket Nozzle B02-019 Interior and Exterior Laser-Induced B02-171 Effects of End Wall Geometry and B02-012 Shock Fitting a Transonic Cascade Flourescence and Plasma Measurements within Stacking on Supersonic Turbine Performance Solution into an Inverse Design Technique a Hall Thruster B02-006 Experimental Investigation of Limit- B02-067 Unsteady Flow in a Supersonic Tur- B02-057 Magnetohydrodynamic Power Extrac- Cycle Oscillations in an Unstable Gas Turbine bine with Variable Specific Heats tion from Cold Hypersonic Airflows with Exter- Combustor Hydrodynamics nal lonizers B02-022 Flow Past Stationary Spherical Parti- cles with Streamwise Velocity Fluctuation Rarefied Flows B02-161 Modeling Cavitating Venturi Flows B02-133 High-Speed Centrifugal Compressor B02-137 Numerical Simulation of a Pulse Deto- B02-108 Facility Effects on Performance Mea- Surge Initiation Characterization nation Engine with Hydrogen Fuels surements of Micropropulsion Systems that Uti- B02-093 Improved Mean-Flow Solution for lize Gas Expansion Slab Rocket Motors with Regressing Walls Hypersonic Flow B02-062 Massively Parallel Simulation of the B02-138 Influence of Radical Concentration and Reacting Flows and Combustion Unsteady Flow in an Axial Turbine Stage Fuel Decomposition on Ignition of Propane/Air B02-095 Combustion Characteristics of Ethyl- B02-166 Measured Flow Oscillations and Insta- Mixture ene in Scramjet Engines bilities in Labyrinth Seal Cavities B02-053 Combustion Instability Active Control B02-036 Numerical Simulation of Side Loads in Inlet, Nozzle, Diffuser, and Channel Using Periodic Fuel Injection an Ideal Truncated Nozzle Flows B02-139 Effects of Halons and Halon Replace- B02-060 Particle Image Velocimetry Characteri- B02-078 Appearance of Restricted Shock Sepa- ments on Hydrogen-Fueled Laminar Premixed zation of a Chordwise Bending Cascade Flow- ration in Rocket Nozzles Flames field B02-122, Automated Design Optimization of a B02-137 |N umerical Simulation of a Pulse Deto- B02-061 Rotor Blade-to-Blade Wake Variability Three-Dimensional S-Shaped Subsonic Diffuser nation Engine with Hydrogen Fuels and Effect on Downstream Vane Response J. PROPULSION, VOL. 18, NO. 6: 2002 INDEX 1315 B02-146 Study of Flow Separation in Truncated B02-127 Laser-Air Interactions in an Internal B02-046 Numerical Simulations of the Slinga- Ideal Contour Nozzle Supersonic Flowpath tron B02-169 Interaction of Decaying Freestream B02-015 Overview of the Development of Turbulence with a Moving Shock Wave: Pres- Multidisciplinary Design Optimization Hydrazinium Nitroformate sure Field B02-121 Optimum Mixing of Core and Bypass B02-016 Overview of the Development of B02-07% Unsteady Cascade Aerodynamics in Streams in a High-Bypass Civil Turbofan Hydrazinium Nitroformate-Based Propellants the Time Domain B02-068 Project Orion and Future Prospects for B02-067 Unsteady Flow in a Supersonic Tur- Safety Nuclear Pulse Propulsion bine with Variable Specific Heats B02-116 Heat Release Rates of Burning Items in B02-045 Sizing a Slingatron-Based Space Viscous Non-Boundary-Layer Flows Fires Launcher B02-044 Slingatron: A High Velocity Rapid B02-022 Flow Past Stationary Spherical Parti- Fire Sling Launch Vehicle and Missile (LV/M) cles with Streamwise Velocity Fluctuation B02-067 Unsteady Flow in a Supersonic Tur- B02-093 Improved Mean-Flow Solution for Technology bine with Variable Specific Heats Slab Rocket Motors with Regressing Walls Launch Vehicle and Sounding Rocket Vortices Systems Airbreathing Propulsion B02-147 Experimental Investigation of End- B02-124 Analysis of a Fusion-Electric Air- B02-129 A PIV Investigation of Rotor-IGV Wall Fiow in Turbine Rotor breathing Earth to Orbit Launch Vehicle Interactions in a Transonic Compressor B02-096 High-Intensity Sound Absorption at an B02-127_ Laser-Air Interactions in an Internal B02-086 Aerodynamic Optimization of Turbo- Orifice with Bias Flow Supersonic Flowpath machinery Cascades Using Euler/Boundary- Layer Coupled Genetic Algorithms Propulsion and Propellant Systems Guidance, Control, and Dynamics B02-168 Airfoil Row/Wake Interactions in a Technology B02-162 Hydrogen Peroxide Decomposition on High-Speed Axial Compressor Various Supported Catalysts Effect of Stabilizers BO2-151 Analysis and Application — of Artificial Intelligence B02-150 Advanced Performance Modeling of Chorochronic Periodicity in Turbomachinery Experimental Laser Lightcraft Rotor/Stator Interaction Computations B02-059 Fuzzy Logic Intelligent System for Gas B02-082 Combustion of Liquefying Hybrid Pro- B02-124 Analysis of a Fusion-Electric Air- Turbine Module and System Fault Isolation pellants: Part 1, General Theory breathing Earth to Orbit Launch Vehicle Control System Design B02-083 Combustion of Liquefying Hybrid Pro- B02-051 Chemiluminescence-Based Feedback pellants: Part 2, Stability of Liquid Films Control of Equivalence Ratio for a Continuous B02-053 Combustion Instability Active Control B02-101 Effect of ESEX 26-kW Arcjet Opera- Combustor Using Periodic Fuel Injection tion on Spacecraft Communications B02-055 Combustion Air Jet Influence on Pri- B02-087 When Do Open-Loop Strategies for B02-104 Mass Deposition Measurements from mary Zone Characteristics for Gas-Turbine Combustion Control Work? 26-Kilowatt Electric Propulsion Space Experi- Combustors Dynamics ment Flight B02-126 Drag and Total Pressure Distributions B02-158 Motor and Plume Particle Size Predic- in Scramjet Engines at Mach 8 Flight B02-069 Study of the Phase-Lock Phenomenon tion in Solid-Propellant Rocket Motors B02-135 Effect of Integration of Scramjet into for a Circular Slingatron B02-046 Numerical Simulations of the Slinga- Airframe on Engine Performance and Payload tron B02-008 Fundamentals of Idealized Airbreath- Engine Control B02-097 Review of the Electric Propulsion ing Pulse-Detonation Engines B02-053 Combustion Instability Active Control Space Experiment (ESEX) Program B02-133 High-Speed Centrifugal Compressor Using Periodic Fuel Injection B02-070 Shape Optimization of Supersonic Tur- Surge Initiation Characterization B02-087 When Do Open-Loop Strategies for bines Using Global Approximation Methods B02-063 Impeller Blade Unsteady Aerodynamic Combustion Control Work? Response to Vaned Diffuser Potential Fields Testing, Flight and Ground B02-138 Influence of Radical Concentration and Launch Vehicle Dynamics B02-077 Acceptance Screening of Turbopump Fuel Decomposition on Ignition of Propane/Air B02-045 Sizing a Slingatron-Based Space Gears Using the Cepstrum Method Mixture Launcher B02-097 Review of the Electric Propulsion B02-123 Inlet/Compressor System Response to Space Experiment (ESEX) Program Short-Duration Acoustic Disturbances Interdisciplinary Topics Vibration B02-002 Integrated Design and Analysis of Intakes and Nozzles in Air-Breathing Engines Analytical and Numerical Methods B02-040 Characteristic Analysis of Flow- B02-127 Laser-Air Interactions in an Internal Induced Vibrations on Inducer of Oxygen Pump Supersonic Flowpath B02-080 Ejector Primary Flow Molecular B02-052 Linear Deterministic Source Terms for Weight Effects in an Ejector-Ram Rocket Engine Propulsion Hot Streak Simulations B02-056 Mach 8 Testing of a Scramjet Engine B02-069 Study of the Phase-Lock Phenomenon for a Circular Slingatron Advanced Space Propulsion with Ramp Compression B02-062 Massively Parallel Simulation of the B02-141 Assessment of Combustion Character- Atmospheric and Space Sciences Unsteady Flow in an Axial Turbine Stage istics and Mechanism of Hydroxylammonium B02-157 Numerical Reconstruction of Ejector B02-163 Thermochemistry of Species Produced Nitrate-Based Liquid Monopropellant Rocket Experimental Tests from Monomethylhydrazine in Propulsion and B02-035 Computations of Axisymmetric Plug- B02-121_ Optimum Mixing of Core and Bypass Space-Related Applications Nozzle Flowfields: Flow Structures and Thrust Streams in a High-Bypass Civil Turbofan Performance Lasers and Laser Applications B02-060 Particle Image Velocimetry Characteri- B02-017 Design of a Fusion Propulsion Sys- zation of a Chordwise Bending Cascade Flow- B02-124 Analysis of a Fusion-Electric Air- tem—Part |: Gigawatt-Level Magnetoplasma- field breathing Earth to Orbit Launch Vehicle dynamic Source B02-061 Rotor Blade-to-Blade Wake Variability B02-065 Correlating Laser Induced Fluores- B02-018 Design of a Fusion Propulsion Sys- and Effect on Downstream Vane Response cence and Molecular Beam Mass Spectrometry tem—Part 2: Numerical Simulation of Magnet- B02-012 Shock Fitting a Transonic Cascade lon Energy Distributions ic-Nozzle Flows Solution into an Inverse Design Technique B02-019 Interior and Exterior Laser-Induced B02-080 Ejector Primary Flow Molecular B02-049 Study of the High-Temperature Flourescence and Plasma Measurements within Weight Effects in an Ejector-Ram Rocket Autoignition of n-Alkane/O>/Ar Mixtures a Hall Thruster Engine 1316 J. PROPULSION, VOL. 18, NO. 6: 2002 INDEX B02-149 Supersonic Wave/Blade-Row Interac- Detonation Emissions and Noises tions Establish Boundary Conditions for Unsteady Inlet Flows B02-136 Direct Experimental Impulse B02-055 Combustion Air Jet Influence on B02-154 Thermodynamics of Airbreathing Measurements for Detonations and Primary Zone Characteristics for Gas-Turbine Pulse-Detonation Engines Deflagrations Combustors B02-032 Development of Advanced Industrial B02-007 Thermodynamic Cycle Analysis of B02-043 Dynamic Combustion of Solid Furnace Using Highly Preheated Combustion Pulse Detonation Engines Propellants: Effects of Unsteady Condensed Air B02-128 Timescaling Control Volumes During Phase Degradation Layer B02-091 —_E lliptic Coflow Effects on a Circular B02-047 Ethylene Ignition and Detonation Real Time Digital Simulation of a Military Tur- Gas Jet Flame bofan Chemistry, Part 1: Detailed Modeling and B02-106 Observations of Soot in the B02-024. Two-Dimensional Spectroscopic Experimental Comparison Combustion of Methanol/Toluene Spray Flames B02-048 Ethylene Ignition and Detonation B02-140 —_P ilot Flame Effects on Gas Jet Analysis of a Flame Using Highly Preheated Chemistry, Part 2: Ignition Histories and Flames in Crossflow Combustion Air Reduced Mechanisms B02-050 —_P rofiling of Redox Index During B02-071 Unsteady Cascade Aerodynamics in B02-008 Fundamentals of Idealized Combustion to Monitor C/C Composite the Time Domain Airbreathing Pulse-Detonation Engines Degradation in Flames B02-156 Work Potential Perspective of Engine B02-007 Thermodynamic Cycle Analysis of Component Performance Pulse Detonation Engines Engine Control Integration and Heaith B02-154. Thermodynamics of Airbreathing Monitoring Combustion and Combustor Designs Pulse-Detonation Engines B02-025 Anomalous Deflagration Behavior of B02-077 Acceptance Screening of Turbopump Gears Using the Cepstrum Method Ammonium Perchlorate at Elevated Pressures Droplet and Spray Characterization B02-134 Gas Turbine Engine and Sensor B02-084 Burning Aluminum Particles Inside a B02-026 Effects of GH,/LOX Velocity and Fault Diagnosis Using Optimization Techniques Laboratory-Scale Solid Rocket Motor Momentum Ratios on Shear Coaxial Injector B02-112_ Chemical Speciation and Dynamics in Atomization Engine Cooling and Heat Transfer the Surface Combustion Zone of Energetic B02-033 Effects of Liquid-Oxygen Post Biasing Materials on SSME Injector Wall Compatibility “2-033 Effects of Liquid-Oxygen Post B02-055 Combustion Air Jet Influence on Pri- B02-111 Model of Aluminum Agglomerate Biasing on SSME Injector Wall Compatibility mary Zone Characteristics for Gas-Turbine Evolution in Combustion Products of Solid Combustors Rocket Propellant Engine Performance B02-082 Combustion of Liquefying Hybrid Pro- B02-106 Observations of Soot in the Combus- B02-156 Work Potential Perspective of Engine pellants: Part 1, General Theory tion of Methanol/Toluene Spray Flames Component Performance B02-083 Combustion of Liquefying Hybrid Pro- B02-035 Computations of Axisymmetric Plug- Electric Propulsion Nozzle Flowfields: Flow Structures and Thrust pellants: Part 2, Stability of Liquid Films Performance B02-032 Development of Advanced Industrial B02-021 Cascade Arc Studies of B02-054 Constant Volume Limit of Pulsed Furnace Using Highly Preheated Combustion Hydrogen/Nitrogen Plasmas in Nonequilibrium Propulsion for a Constant Y Ideal Gas Air B02-172 Controlling Electron Backstreaming B02-018 Design of a Fusion Propulsion Sys- Phenomena Through the Use of a Transverse B02-091 Elliptic Coflow Effects on a Circular tem—Part 2: Numerical Simulation of Magnet- Gas Jet Flame Magnetic Field ic-Nozzle Flows B02-116 Heat Release Rates of Burning Items in B02-065 Correlating Laser Induced Fluores- B02-126 Drag and Total Pressure Distributions cence and Molecular Beam Mass Spectrometry in Scramjet Engines at Mach 8 Flight Fires lon Energy Distributions B02-080 Ejector Primary Flow Molecular B02-111 Model of Aluminum Agglomerate B02-099 Development and Flight Qualification Weight Effects in an Ejector-Ram Rocket Evolution in Combustion Products of Solid of a 26-Kilowatt Arcjet Propulsion Subsystem Engine Rocket Propellant B02-101 Effect of ESEX 26-kW Arcjet Opera- B02-008 Fundamentals of Idealized Airbreath- B02-106 Observations of Soot in the Combus- tion on Spacecraft Communications ing Pulse-Detonation Engines tion of Methanol/Toluene Spray Flames B02-108 Facility Effects on Performance Mea- B02-133 High-Speed Centrifugal Compressor B02-140 Pilot Flame Effects on Gas Jet Flames surements of Micropropulsion Systems that Uti- Surge Initiation Characterization B02-166 Measured Flow Oscillations and Insta- in Crossflow lize Gas Expansion bilities in Labyrinth Seal Cavities B02-023 Reduced Chemical Kinetic Mecha- B02-028 Intercusp Electron Transport in an B02-121 Optimum Mixing of Core and Bypass nisms for Hydrocarbon Fuels NSTAR-Derivative lon Thruster Streams in a High-Bypass Civil Turbofan B02-024. Two-Dimensional Spectroscopic B02-019 Interior and Exterior Laser-Induced B02-050 Profiling of Redox Index During Com- Analysis of a Flame Using Highly Preheated Flourescence and Plasma Measurements within bustion to Monitor C/C Composite Degradation Combustion Air a Hall Thruster in Flames B02-104 Mass Deposition Measurements from B02-154 Thermodynamics of Airbreathing Combustion Instability 26-Kilowatt Electric Propulsion Space Experi- Pulse-Detonation Engines ment Flight B02-007 Thermodynamic Cycle Analysis of B02-043 Dynamic Combustion of Solid Propel- B02-097 Review of the Electric Propulsion Pulse Detonation Engines lants: Effects of Unsteady Condensed Phase B02-128 Timescaling Control Volumes During Space Experiment (ESEX) Program Degradation Layer Real Time Digital Simulation of a Military Tur- B02-103 Solar Cell Degradation During the 26- B02-014 Effects of Grain Geometry on Pulse- bofan Kilowatt Electric Propulsion Space Experiment Triggered Combustion Instability in Rocket Flight Fuels and Propellants, Properties of Motors B02-098 System Engineering, Design, Integra- B02-085 Evaluation of Ultrasound Technique tion, and Qualification of Electric Propulsion BA0m2m-0o2n5 iumAn oPmearlcohulosr ateD efalta gErlaetviaotne d BPerheasvsiuorre s of for Solid-Propellant Burning-Rate Response Space Experiment B02-110 Asphaltic Thermoplastic Propellants Measurements B02-020 Verification Tests of Carbon-Carbon B02-141 Assessment of Combustion Character- B02-030 Propagation of Acoustic Waves in a Composite Grids for Microwave Discharge lon istics and Mechanism of Hydroxylammonium Two-Phase Vaporizing Mixture Thruster Nitrate-Based Liquid Monopropellant J. PROPULSION, VOL. 18, NO. 6: 2002 INDEX 1317 B02-112 Chemical Speciation and Dynamics in B02-081 Solid-Fuel Regression Rate Behavior B02-043, Dynamic Combustion of Solid Propel- the Surface Combustion Zone of Energetic of Vortex Hybrid Rocket Engines lants: Effects of Unsteady Condensed Phase Materials Degradation Layer B02-116 Heat Release Rates of Burning Items in Ignition and Ignitor Design B02-042 Effect of Nozzle Cavity on Resonance Fires B02-162 Hydrogen Peroxide Decomposition on in Large SRM: Theoretical Modeling B02-145 High Strain-Rate Constitutive Models Various Supported Catalysts Effect of Stabilizers 802-014 Effects of Grain Geometry on Pulse- for Solid Rocket Propellants B02-084 Burning Aluminum Particles Inside a Triggered Combustion Instability in Rocket B02-015 Overview of the Development of Laboratory-Scale Solid Rocket Motor Motors Hydrazinium Nitroformate B02-090 Effects of Airstream Mach Number on B02-085 Evaluation of Ultrasound Technique B02-016 Overview of the Development of H,/N, Plasma Igniter for Solid-Propellant Burning-Rate Response Hydrazinium Nitroformate-Based Propellants B02-014 Effects of Grain Geometry on Pulse- Measurements B02-050 Profiling of Redox Index During Com- Triggered Combustion Instability in Rocket B02-145 High Strain-Rate Constitutive Models bustion to Monitor C/C Composite Degradation Motors for Solid Rocket Propellants in Flames B02-047 Ethylene Ignition and Detonation B02-111 Model of Aluminum Agglomerate B02-109 Sensitivity of Solid Rocket Motors to Chemistry, Part 1: Detailed Modeling and Evolution in Combustion Products of Solid Electrostatic Discharge: History and Future Experimental Comparison Rocket Propellant B02-049 Study of the High-Temperature B02-048 Ethylene Ignition and Detonation B02-158 Motor and Plume Particle Size Predic- Autoignition of n-Alkane/O,/Ar Mixtures Chemistry, Part 2 Ignition Histories and tion in Solid-Propellant Rocket Motors B02-163 Thermochemistry of Species Produced Reduced Mechanisms B02-041 Numerical Predictions of Channel from Monomethylhydrazine in Propulsion and B02-049 Study of the High-Temperature Flows with Fluid Injection Using Reynolds- Space-Related Applications Autoignition of n-Alkane/O.,/Ar Mixtures Stress Model B02-034 Time- and Length Scales of Combus- B02-034 Time- and Length Scales of Combus- B02-015 Overview of the Development of tion in Liquid Rocket Thrust Chambers tion in Liquid Rocket Thrust Chambers Hydrazinium Nitroformate B02-024 Two-Dimensional Spectroscopic B02-016 Overview of the Development of Analysis of a Flame Using Highly Preheated Liquid Rocket Motors and Missile Hydrazinium Nitroformate-Based Propellants Combustion Air Systems B02-144 Property Transformation of Ther- Gas Turbine Engines B02-077. Acceptance Screening of Turbopump motropic Liquid Crystals Polymers Gears Using the Cepstrum Method B02-109 Sensitivity of Solid Rocket Motors to B02-164 Advanced Seals for Industrial Turbine B02-162 Hydrogen Peroxide Decomposition on Electrostatic Discharge: History and Future Applications: Design Approach and Static Seal Various Supported Catalysts Effect of Stabilizers Development Supersonic Combustion B02-078 Appearance of Restricted Shock Sepa- B02-165 Advanced Seals for Industrial Turbine ration in Rocket Nozzles B02-090 Effects of Airstream Mach Number on Applications: Dynamic Seal Development B02-037 Design Analysis of a Satellite H,/N, Plasma Igniter B02-168 Airfoil Row/Wake Interactions in a Hydrazine Propulsion System B02-056 Mach 8 Testing of a Scramjet Engine High-Speed Axial Compressor B02-026 Effects of GH,/LOX Velocity and with Ramp Compression B02-051 Chemiluminescence-Based Feedback Momentum Ratios on Shear Coaxial Injector Control of Equivalence Ratio for a Continuous Atomization Transient Combustion and Detonation Combustor B02-033 Effects of Liquid-Oxygen Post Biasing B02-006 Experimental Investigation of Limit- B02-054 Constant Volume Limit of Pulsed on SSME Injector Wall Compatibility Cycle Oscillations in an Unstable Gas Turbine Propulsion for a Constant Y Ideal Gas Combustor B02-072 Multiobjective Optimization of Rocket B02-043 Dynamic Combustion of Solid Propel- Engine Pumps Using Evolutionary Algorithm B02-059 Fuzzy Logic Intelligent System for lants: Effects of Unsteady Condensed Phase B02-039 Temperature-Dependent Modal Gas Turbine Module and System Fault Isolation Degradation Layer Test/Analysis Correlation of X-34 FASTRAC B02-134 Gas Turbine Engine and Sensor Fault B02-085 Evaluation of Ultrasound Technique Composite Rocket Nozzle Diagnosis Using Optimization Techniques for Solid-Propellant Burning-Rate Response B02-034 Time- and Length Scales of Combus- 802-094 Geometric Evaluation of Axisymmet- Measurements tion in Liquid Rocket Thrust Chambers ric Thrust-Vectoring Nozzles for Aerodynamic Performance Predictions Propulsion Hazards Turbomachinery B02-063 Impeller Blade Unsteady Aerodynam- ic Response to Vaned Diffuser Potential Fields B02-018 Design of a Fusion Propulsion Sys- B02-061 Rotor Blade-to-Blade Wake Variability tem—Part 2: Numerical Simulation of Magnet- B02-164 =A dvanced Seals for Industrial and Effect on Downstream Vane Response ic-Nozzle Flows Turbine Applications: Design Approach and B02-073 Three-Dimensional Hybrid Mesh Gen- B02-109 Sensitivity of Solid Rocket Motors to Static Seal Development eration for Turbomachinery Airfoils Electrostatic Discharge: History and Future B02-165 = Advanced Seals for Industrial Turbine Applications: Dynamic Seal B02-156 Work Potential Perspective of Engine Ramjets and Scramjets Developmen: Component Performance B02-119 Control of Low-Pressure Turbine B02-126 Drag and Total Pressure Distributions Separation Using Vortex-Generator Jets Hypersonic Propulsion in Scramjet Engines at Mach 8 Flight B02-074. Development of High-Performance B02-095 Combustion Characteristics of Ethyl- B02-135 Effect of Integration of Scramjet into Airfoils for Axial Flow Compressors Using ene in Scramjet Engines Airframe on Engine Performance and Payload B02-138 Influence of Radical Concentration and B02-090 Effects of Airstream Mach Number on Evolutionary Computation Fuel Decomposition on Ignition of Propane/Air H./N, Plasma Igniter B02-147. Experimental Investigation of End- Wall Flow in Turbine Rotor Mixture B02-056 Mach 8 Testing of a Scramjet Engine B02-010 Flow Control via Rotor Trailing B02-057 Magnetohydrodynamic Power Extrac- with Ramp Compression Edge Blowing in a Rotor/Stator Axial tion from Cold Hypersonic Airflows with Exter- B02-004 Numerical Simulation of the Ram Compressor nal lonizers Accelerator Using a New Chemical Kinetics B02-063 Impeller Blade Unsteady Mechanism Aerodynamic Response to Vaned Diffuser Hybrid Rocket Engines Solid Rocket Motors and Missile Systems Potential Fields B02-082 Combustion of Liquefying Hybrid Pro- B02-062 Massively Parallel Simulation of the pellants: Part 1, General Theory B02-025 Anomalous Deflagration Behavior of Unsteady Flow in an Axial Turbine Stage B02-083 Combustion of Liquefying Hybrid Pro- Ammonium Perchlorate at Elevated Pressures B02-166 Measured Flow Oscillations and pellants: Part 2, Stability of Liquid Films B02-110 Asphaltic Thermoplastic Propellants Instabilities in Labyrinth Seal Cavities B02-059 Fuzzy Logic Intelligent System for Gas B02-084 Burning Aluminum Particles Inside a Turbine Module and System Fault Isolation Laboratory-Scale Solid Rocket Motor 1318 J. PROPULSION, VOL. 18, NO. 6: 2002 INDEX B02-072 Multiobjective Optimization of Spacecraft Propulsion System Thermal Effects Rocket Engine Pumps Using Evolutionary Integration B02-039 Temperature-Dependent Modal Algorithm B02-037 Design Analysis of a Satellite Test/Analysis Correlation of X-34 FASTRAC B02-070 Shape Optimization of Supersonic Composite Rocket Nozzle Hydrazine Propulsion System Turbines Using Global Approximation Methods B02-099 Development and Flight Qualification B02-149 Supersonic Wave/Blade-Row of a 26-Kilowatt Arcjet Propulsion Subsystem Thermophysics and Heat Transfer Interactions Establish Boundary Conditions for B02-102 On-Orbit Optical Observations of Unsteady Inlet Flows Ablation, Pyrolysis, Thermal Electric Propulsion Space Experiment 26-Kilo- B02-073 Three-Dimensional Hybrid Mesh Decomposition, and Degradation watt Arcjet Generation for Turbomachinery Airfoils B02-068 Project Orion and Future Prospects for B02-141 Assessment of Combustion Character- istics and Mechanism of Hydroxylammonium Nuclear Pulse Propulsion Nitrate-Based Liquid Monopropellant Space Technology B02-105 Radiometric Analysis from the 26- B02-081 Solid-Fuel Regression Rate Behavior Kilowatt Electric Propulsion Space Experiment of Vortex Hybrid Rocket Engines Space Experiments Flight B02-045 Sizing a Slingatron-Based Space Aerothermodynamics/Thermal Protection B02-101 Effect of ESEX 26-kW Arcjet Opera- tion on Spacecraft Communications Launcher B02-120 Analysis and Multidisciplinary Opti- B02-104_ Mass Deposition Measurements from B02-098 System Engineering, Design, Integra- mization of Internal Coolant Networks in Tur- 26-Kilowatt Electric Propulsion Space Experi- tion, and Qualification of Electric Propulsion bine Blades Space Experiment ment Flight Computational Heat Transfer B02-105 Radiometric Analysis from the 26- Spacecraft Test and Evaluation B02-120 Analysis and Multidisciplinary Opti- Kilowatt Electric Propulsion Space Experiment B02-099 Development and Flight Qualification mization of Internal Coolant Networks in Tur- Flight of a 26-Kilowatt Arcjet Propulsion Subsystem bine Blades B02-103 Solar Cell Degradation During the 26- Kilowatt Electric Propulsion Space Experiment Spacecraft Thermal Management Laser Interaction Flight B02-150 Advanced Performance Modeling of B02-153 Mass-Based Optimization of Thermal B02-098 System Engineering, Design, Integra- Experimental Laser Lightcraft Management and Power Systems for Space tion, and Qualification of Electric Propulsion Applications Thermal Modeling and Analysis Space Experiment B02-120 Analysis and Multidisciplinary Opti- Space Systems Structural Mechanics and mization of Internal Coolant Networks in Tur- bine Blades B02-153 Mass-Based Optimization of Thermal Materials B02-092 Experimental Study of a 3-kW Stirling Management and Power Systems for Space Structural Dynamics and Engine Applications B02-113 Thermomechanical Analysis and Opti- Characterization mization of Cryogenic Liquid Rocket Engines Spacecraft Contamination/Sterilization B02-039 Temperature-Dependent Modal B02-105 Radiometric Analysis from the 26- Test/Analysis Correlation of X-34 FASTRAC Thermochemistry and Chemical Kinetics Kilowatt Electric Propulsion Space Experiment Composite Rocket Nozzle B02-095 Combustion Characteristics of Ethyl- Flight ene in Scramjet Engines B02-103 Solar Cell Degradation During the 26- Structural Finite Elements B02-047 Ethylene Ignition and Detonation Kilowatt Electric Propulsion Space Experiment B02-113_ Thermomechanical Analysis and Opti- Chemistry, Part 1: Detailed Modeling and Experimental Comparison Flight mization of Cryogenic Liquid Rocket Engines B02-048 Ethylene Ignition and Detonation Spacecraft Power Structural Optimization Chemistry, Part 2: Ignition Histories and Reduced Mechanisms B02-064 Recent GRC Aerospace Technologies B02-113_ Thermomechanical Analysis and Opti- B02-023 Reduced Chemical Kinetic Mecha- Applicable to Terrestrial Energy Systems mization of Cryogenic Liquid Rocket Engines nisms for Hydrocarbon Fuels J. PROPULSION, VOL. 18, NO. 6: 2002 INDEX Author Index Acharya, S., BO2-115 Dorney, Daniel J., BO2-067, B02-070, Heiser, William H., B02-007, BO2-027 Lear, W. E., BO2-153 Adams, Robert B., BO2—127, B02-124 B02-167, BO2-171 Heister, Stephen D., BO2-161 LeDuc, J. R., BO2-097 Adler, Dan, BO2-094 Draxler, G. R., BO2-075, B02-076 Hengli, Liang, BO2-040 Lee, J. H. S., BO2-148 Akihisa, Daisuke, BO2—135 Dulikravich, George S., BO2-120 Hepp. Aloysius F., B02-064 Lee, S. W., BO2-114 Akmandor, I. Sinan, BO2—086 Dulligan, M. J., BO2-097, BO2-101 Higgins, A. J., BO2-148 Lefantzi, Sophia, BO2-122 Aksit, Mahmut F., B02-164, B02-165 Dulligan, M. W., BO2-102 Hiraiwa, Tetsuo, BO2-126 Lieuwen, Tim C., B02-006 Alonso, Juan J., BO2-062 Dupays, Joél, BO2-030 Hirschberg, A., BO2-042 Lilley, David G., BO2-116, BO2-088, Altman, D., BO2-082 Ebrahimi, Houshang B., BO2-031, Ho. Sook-Ying, BO2-145 B02-089 Amano, R. S., BO2-076 B02-137 Hoberecht, Mark A., B02-064 Lin, M. C., BO2-112 Amano, R. S., BO2-075 Ehrlich, Daniel A., BO2-060 Horiuchi, Y., B02-020 Lior, Noam, B02-058 Andreopoulos, Y., BO2-169 Eklund, D. R., B02-131 Horning, D. C., B02-049 Liou, Meng-Sing, BO2-072 Anil Kumar, K. R., BO2-043 Eley, James A., BO2-107 Hoskins, W. A., BO2-099, BO2-100, Litzinger, Thomas A., BO2-112, Annaswamy, A. M., B02-053, Eloirdi, Rachel, BO2-162 B02-102 B02-160 B02-087 Engelman, S. F., BO2-104 Hsu, Tzu-Cheng, B02-118 Liu, Jiwen, BO2-150 Anthoine, J., BO2-042 Faeth, G. M., BO2-139 Huber, Frank, BO2-067 Liu, T., BO2-066 Arai, Norio, B02-058, B02-024, Fagan, John R., B02-133 Huber, Frank W., B02-171 Lo, A. C., BO2-010 B02-050 Farshchi, Mohammad, B02-014 Irvine, C. A., BO2-068 Louwers, J., BO2-015, BO2-016 Austin, J., BO2-136 Ferlauto, M., BO2-002 Ito, Takashi, BO2-035 Lu, Pong-Jeu, BO2-118, BO2-132 Avedisian, C. T., BO2-106 Ferraro, M., BO2-026 Ivancic, B., BO2-034 Luna, Sayela P., BO2-091 Babuk, V. A., BO2-111 Field, Robert, BO2-161 Jackson, S., BO2-136 Lyons, Valerie J., BO2-064 Baik, Doo S., BO2-003 Fite, J.M ., BO2-097, BO2-100 Jager, Bram de, BO2-009 Macheret, Sergey O., BO2-057 Bar-Yoseph, Pinhas Z., BO2-094 Flanagan, Joseph E., BO2-112 Jameson, Antony, BO2-062 Majdalani, Joseph, BO2-093 Barter, John W., BO2-052 Fleeter, S., BO2-066 Jianbo, Wang, BO2-038 Martin, Thomas J., BO2-120 Baurle, R. A., BO2-131 Fleeter, Sanford, BO2-011, BO2-063, Jing, Xiaodong, BO2-096 Masuya, Goro, B02-090, B02-135, Beckstead, Merrill C., BO2—112 B02-061, B02-060, BO2-071, Johnson, J. Wayne, BO2-166 B02-126 Ben-Yakar, Adela, BO2-—125 B02-130, BO2-129, BO2-133, Johnson, L. K., B02-097, BO2-100, Matesanz, A., BO2-157 Benini, Ernesto, BO2-074 B02-168 B02-101, BO2-102, BO2-103, Mattingly, Jack D., BO2-027 Berg, R. P. van den, BO2-015, B0O2-016 Fleifil, M., BO2-053 B02-104, BO2-105 Maurice, Lourdes Q., B02-023 Bleeg, James M., BO2-107 Foster, John E., B02-028, BO2-172 Johnston, R., BO2-066 Mayer, W., B02-034 Bonometti, J. A., BO2-068 Frayne, C., B02-055 Johnston, Robert T., BO2-168 Mead, Jr., Franklin B., BO2-150 Bons, Jeffrey P.. BO2-119 Frederick, Jr., R. A., BO2-142 Kagawa, Noboru, B02-092 Medd, Adam J., BO2-012 Briassulis, G., BO2-169 Freeman, Jeffrey M., BO2-025 Kanda, Takeshi, B02-056, B02-135 Melcher, John C., B02-084 Brill, Thomas B., BO2-112 Freudenberg, K. D., BO2-153 Kankam, M. David, B02-064 Merkle, Charles L., B02-031, B02-137 Bromaghim, D. R., BO2-097, Frey, M., BO2-078 Kappenstein, Charles, B02-160 Micci, M. M., B02-026 B02-100, BO2-101, BO2-102, Frey. Manuel, BO2-013 Karabeyoglu, M. A., B02-083, Michon, G. J., BO2-151 B62-103, BO2-104, BO2-105 Fujii, Kozo, BO2-035 B02-082 Mikellides, loannis G., BO2-017, Brown, Andrew M., B02-039 Funaki, I., BO2-020 Kavsaoglu, Mehmet S., BO2-086 B02-018 Buchlin, J-M., BO2-042 Furuhata, Tomohiko, BO2-058 Kayukawa, Naoyuki, B02-117 Mikellides, Pavlos G., BO2-017, Bumiy, M. L., BO2-046 Gallimore, Alec D., B02-065 Keefer, Dennis, B02-021 B02-018 Bundy, Mark L., BO2-045 Ganguli, Ranjan, BO2-059 Keizers, H. L. J., B02-015, B02-016 Miles, Richard B., BO2-057 Buriko, Yuriy Ya., BO2-138 Gerolymos, G. A., B02-151 Kentfield, J. A. C., BO2-008, BO2-154 Miner, K. I. , B02-033 Burton, Rodney L., BO2-084 Ghasripoor, Farshad, B02-165 Ketsdever, Andrew D., B02-108 Mitani, Tohru, BO2-126 Camwell, B. J., BO2-083, BO2-082 Ghassemi, Hojat, B02-014 Kim, C. H., B02-139 Mochida, S., BO2-032 Cappelli, M. A., BO2-019 Ghoniem, A. F., B02-053, BO2-087 Kim, Hyeong-Jin, BO2-116, BO2-088, Moeller, Trevor, BO2-021 Cassady, R. J., BO2-099 Glogowski, M.J., B02-026 B02-089 Mohanraj, Rajendran, B02-031 Cateaire, Laurent, B02-163 Gogineni, S., B02-055 Kim, Jong-Uk, B02-152 Mohieldin, T. O., BO2-095 Chaffee, K. P., B02-144 Goh, Sien-Fong, B02-140 Kim, Kyu-sup, B02-073 Montanes, J., BO2-157 Chakravarthy, Satyanarayanan R.., Golafshani, Mehdi, B02-014 King, Galen B., B02-051 Montgomery, Christopher J., BO2-023 BO2-025 Golembiewski, J. M., B02-076 Kitagawa, Kuniyuki, BO2-024, Murphy, Jeffrey J., BO2-085 », W. C., BO2-010 Gollahalli, S. R., BO2-091, BO2-140 B02-050 Myrabo, Leik N., BO2-150 Chang, Yi-Ping, B02-141 Golliher, E. L., B02-153 Kiyanda, C. B., BO2-148 Nalim, M. Razi, BO2-155 Chaouat, Bruno, BO2-041 Goltsev, Valentin F., BO2-138 Knight, Doyle D., BO2-122 Neubauer, J., BO2-151 Chart. D. A., BO2-100 Gottfried, Dana, B02-063 Knopf, F. C., BO2-115 Nishiyama, K., BO2-020 Chen, Jyh-Yuan, B02-023 Gottfried, Dana A., B02-071, BO02-130 Knuth, William H., B02-081 Nusca, Michael J., BO2-004 Chen, Yen-Sen, BO2-150 Gramer, Daniel J., BO2-081 Ko, Hyun, B02-079 Oakes, William C., BO2-133 Chiaverini, Martin J., BO2-081 Gravlin, E. S., BO2-001 Kobayashi, Kan, B02-056 Ohzehi, Hiroyuki, BO2-090 Che, Y. H., B02-114 Gregory, David, B02-080 Konishi, Noriyuki, B02-024 Oksuz, Ozhan, B02-086 Choudhuri, Ahsan R., BO2-091 Griffin, Lisa, BO2-070 Korting, P. A. O. G., BO2-015, Opalski, Anthony B., B02-123 Christensen, K. L., B02-027, BO2-027 Griffin, Lisa W., BO2-067, BO2-171 B02-016 Orkwis, Paul D., BO2-052, BO2-167 Chupp, Raymond E., B02-164, Guérin, Maurice, BO2-162 Koschel. W., B02-078 Oyama, Akira, B02-072 BO2-165 Guillen, Philippe, BO2-036 Kovalev, Oleg B., BO2-158 Pan, Dartzi, BO2-132 Cizmas, Paul G. A., B02-073 Gulezinski, Frank S., B02-065 Kriebel, Mary M., BO2-098 Papalia, John, BO2-129 Clemens, N. T., BO2-152 Gupta, A. K., B02-032, B02-106 Krier, Herman, B02-085, B02-084 Papila, Nilay, BO2-070 Cohen, Norman S., BO2-143 Gupta, Ashwani K., B02-024, Kubota, Masao, B02-050 Paschereit, Christian Oliver, B02-170 Cooper, G. R., B02-046, B02-069 B02-050 Kudo, Kenji, B02-135 Patterson, Michael J., BO2-172 Cooper, Gene R., B02-045 Gupta, Vipul, B02-167 Kudva, Gautam N., B02-160 Peddieson, Jr., John, BO2-080 Cooper, M., BO2-136 Gutmark, E., BO2-115 Kuhl, Detlef, BO2-113 Pillet, Nicolas, BO2-162 Copeland, George S., B02-107 Gutmark, Ephraim, BO2-170 Kujala, R. J.. BO2-026 Pirault-Roy, Laurence, BO2-162 Coy, Edward B., BO2-054 Haeseler, Dietrich, BO2-013 Kuninaka, H., BO2-020 Prasanth, R. K., BO2-087 Cremer, Mare A., BO2-023 Hagemann, G., BO2-078 Kuo, Kenneth K., BO2-141 Pratt, David T., B02-007 Culiek, Fred E. C., BO2-143 Hagemann, Gerald, B02-013 Kuo, Tien-Chuan, B02-037 Presser, C., BO2-106 Dameodaran, M., BO2-029 Haidn, Oskar J., BO2-113 Kwon, O. C., B02-139 Price, Edward W., B02-025 Darea, Yu, BO2-038 Han, Sam, BO2-080 Lakshmanan, B. K., B02-121, Rasmussen, B., BO2-142 Dasgupta, A., BO2-022 Hanson, R. K., BO2-049 B02-128 Rat, Roger, BO2-109 Davenas, Alain, B02-109 Hanson, Ronald K., BO2-125 Lakshminarayana, B., B02-147 Rhie, Chae M., BO2-107 Dav adson, D. F., BO2-049 Hardesty, D., B02-101 Lakshmisha, K. N., BO2-043 Rhode, David L., BO2-166 Davis, Roger L., BO2-062 Hargus, Jr., W. A., BO2-019 Landrum, D. Brian, BO2-127, Rhodes, Robert, BO2-021 Deck. Sébastien, BO2-036 Hasegawa, T., B02-032 B02-124 Ribéreau, D., BO2-159 Demuroglu, Mehmet, B02-164, Hathout, J. P., BO2-053, BO2-087 Larocca, F., BO2-002 Riccius, Jérg, BO2-113 BO2-165 Hayashi, A. Koich, B02-035 Laurendeau, Normand M., B02-051 Rivir, Richard B., BO2-119 DiMaggio, S. J., B02-077 Heijden, A.E.D.M. v.d., BO2-016 Lawless, Patrick B., B02-133 Roth, Bryce, BO2-156 Dine, O. Saim, BO2-164 Heijden, A. E. D. M. van der, BO2-015 Le Breton, P., BO2-159 Rusek, J. J., BO2-144 1320 J. PROPULSION, VOL. 18, NO. 6: 2002 INDEX Rusek, John J., BO2-110 Sondak, Douglas L., B02-067, Tizon, J., BO2-157 Willems, Frank, BO2-009 Saito, Toshihito, BO2-056 B02-167, B02-171 Toffolo, Andrea, B02-074 Williams, F. A., BO2-047, Sajben, Miklos, B02-123, B02-149 Sondergaard, Rolf, BO2-119 Toki, K., BO2-020 BO2-048 Salasovich, R. M., BO2-097, BO2-101 Spanjers, G. G., B02-097, B02-102, Torgerson, S., BO2-066 Williams, George J., B02-065 Sanders, Albert J., BO2-061, BO2-129 B02-103, B02-104, BO2-105 Tseng, L. K., BO2-033 Wilson, Erich A., B02-094 Sane, S. K., BO2-121 Strakey, P. A., BO2-033 Turchi, Peter J., BO2-017, Wilson, Ken J., BO2-005 Sanghi, Vivek, BO2-121, B02-128 Sturgess, G., BO2-055 B02-018 Wintenberger, E., BO2-136 Santhanam, V., BO2-115 Stutrud, J., BO2-055 Turner, Mark G., BO2-052 Wo, A. M., BO2-010 Sauer, J. Arthur, BO2-081 Sullivan, J., BO2-066 Turnquist, Norman A., BO2-165 Won, Y. D., BO2-114 Sawyer, Scott, BO2-O11 Sun, Xiaofeng, BO2-096 Varatharajan, B., BO2-047, B02-048 Xanthos, S., BO2-169 Schilling, J. H., B02-097, BO2-103, Sunami, Tetsuji, BO2-056 Varghese, P. L., BO2-152 Xiao, X., BO2-147 B02-104, BO2-105 Swihart, Mark T., BO2-163 Vasilyev, V. A., BO2-111 Xu, Changhai, BO2-161 Schmidt, G. R., BO2-068 Tacina, Robert R., BO2-064 Vaughan, C. E., B02-099, BO2-100 Yamamoto, Takahisa, BO2-058 Schoyer, H. F. R., BO2-016, BO2-015 Taha, A. A., BO2-095 Velazquez, A., B02-157 Yang, An-Shik, BO2-037 Scott, Douglas A., BO2-051 Takahashi, Katsuyoshi, BO2-090 Verma, S. B., BO2-146 Yao, Jixian, BO2-062 Shepherd, J. E., BO2-136 Takatori, Fumio, B02-090 Vinogradov, Viacheslav A., B02-138 Yokota, Jeffrey W., BO2-012 Sherif, S. A., BO2-153 Takita, Kenichi, BO2-090 Vuillot, Frangois, B02-030 Yoon, W. S., BO02-114 Shih, T. I-P., BO2-022 Talley, Douglas G., BO2-033 Waesche, R. H. Woodward, BO2-112 Yoon, Woong-Sup, B02-079 Shimizu, Y., BO2-020 Talley, Doug, BO2-054 Wal, Mare van de, B0O2-009 York, Thomas M., BO2-018 Shneider, Mikhail N., BO2-057 Tanguay, V., BO2-148 Waltrup, P. J., BO2-001, BO2-138 Yu, Ken H., BO2-005 Shouse, D., BO2-055 Tani, Kouichiro, B02-056, BO2-135 Wang, Ten-See, BO2-150 Yu, Yi-Di, BO2-132 Shusser, Michael, BO2-143 Tarukawa, Yuichi, BO2-126 Wang, X., BO2-029 Zannetti, L., BO2-002 Shyy, Wei, B02-070 Terhardt, Michael, BO2-013 Welland-Veltmans, W.H.M., B02-016, Zarlingo, F., BO2-001 Sigman, Robert K., BO2-025 Thomas, J.-L., BO2-026 B02-015 Zedda, Marco, BO2-134 Silkowski, Peter D., BO2-107 Tidman, D. A., B02-046, BO2-069 Westbrook, Charles K., BO2-023 Zhou, Chong, BO2-093 Simonich, John, B02-011 Tidman, Derek A., BO2-044, White, D. C., B02-097 Zimmerman, J. A., BO2-101 Singh, Riti, BO2-134 B02-045 White, M. E., B02-001 Zumwalt, Glen W., BO2-003 Smith, Timothy B., BO2-065 Tiwari, S. N., BO2-095 Wight, Charles A., BO2-112 Zuoyi, Chen, BO2-040 J. PROPULSION, VOL. 18, NO. 6: 2002 INDEX Chronological Index B02-00! History of U.S. Navy Ramjet, Scramjet, and Mixed- B02-014 Effects of Grain Geometry on Pulse-Triggered Cycle Propulsion Development. P. J. Waltrup and M. E. White, Combustion Instability in Rocket Motors. Mehdi Golafshani, Johns Hopkins University; F. Zarlingo, U.S. Naval Air Warfare Mohammad Farshchi, and Hojat Ghassemi, Sharif University of Center; and E. S. Gravlin, U.S. Naval Air Warfare Center (18, 1, p. Technology, Iran (18, 1, p. 123) Article 14) SURVEY based on AIAA Paper 96-3152 B02-015 Overview of the Development of Hydrazinium B02-002 Integrated Design and Analysis of Intakes and Nozzles Nitroformate. H. F. R. Schéyer, Schéyer Consultancy B.V., The in Air-Breathing Engines. M. Ferlauto, F. Larocca, and Netherlands, W. H. M. Welland-Veltmans, Aerospace Propulsion L. Zannetti, Politecnico di Torino, Italy (18, 1, p. 28) Article Products, The Netherlands; J. Louwers, Royal Philips Electronics Optical Storage, The Netherlands; and P. A. O. G. Korting, A. E. D. M. van der Heijden, H. L. J. Keizers, and R. P. van den Berg, TNC- B02-003 Analytical Model of the Base Flow Between a Prins Maurits Laboratorium, The Netherlands (18, 1, p. 131) Subsonic and Supersonic Flow. Doo S. Baik, Kookmin University, Article Korea; and Glen W. Zumwalt, Wichita State University (18, 1, p. 35) Article B02-016 Overview of the Development of Hydrazinium Nitroformate-Based Propellants. H. F. R. Schéyer, Schdyer B02-004 Numerical Simulation of the Ram Accelerator Using a Consultancy B.V., The Netherlands; W. H. M. Welland-Veltmans, New Chemical Kinetics Mechanism. Michael J. Nusca, U.S. Army Aerospace Propulsion Products, The Netherlands; J. Louwers, Research Laboratory (18, 1, p. 44) Article Royal Philips Electronics Optical Storage, The Netherlands; and P. A. O. G. Korting, A. E. D. M. van der Heijden, H. L. J. Keizers, B02-005 Scale-Up Experiments on Liquid-Fueled Active and R. P. van den Berg, TNO-Prins Maurits Laboratorium, The Combustion Control. Ken H. Yu, University of Maryland; and Netherlands (18, 1, p. 138) Article Ken J. Wilson, U.S. Naval Air Warfare Center (18, 1, p. 53) Article based on AIAA Paper 98-3211 B02-017 Design of a Fusion Propulsion System—Part 1: Gigawatt-Level Magnetoplasmadynamic Source. Pavlos G. B02-006 Experimental Investigation of Limit-Cycle Mikellides, Ohio Aerospace Institute; Peter J. Turchi, Los Alamos Oscillations in an Unstable Gas Turbine Combustor. Tim C. National Laboratory; and loannis G. Mikellides, Science Lieuwen, Georgia Institute of Technology (18, 1, p. 61) Article Applications International Corporation (18, 1, p. 146) Article B02-007 Thermodynamic Cycle Analysis of Pulse Detonation B02-018 Design of a Fusion Propulsion System—Part 2: Engines. William H. Heiser, U.S. Air Force Academy; and David T. Numerical Simulation of Magnetic-Nozzle Flows. Ioannis G. Pratt, University of Washington (18, 1, p. 68) Article Mikellides, Science Applications International Corporation; Pavlos G. Mikellides, Ohio Aerospace Institute; Peter J. Turchi and B02-008 Fundamentals of Idealized Airbreathing Pulse- Thomas M. York, The Ohio State University (18, 1, p. 152) Article Detonation Engines. J. A. C. Kentfield, University of Calgary, based on AIAA Paper 2000-3367 Canada (18, 1, p. 77) Article based on AIAA Paper 2000-3469 B02-019 Interior and Exterior Laser-Induced Flourescence B02-009 Selection of Actuators and Sensors for Surge Control. and Plasma Measurements within a Hall Thruster. W. A. Hargus Jr., and M. A. Cappelli, Stanford University (18, 1, p. 159) Article Marc van de Wal, Frank Willems, and Bram de Jager, Eindhoven University of Technology, The Netherlands (18, 1, p. 84) Article B02-020 Verification Tests of Carbon-Carbon Composite Grids for Microwave Discharge Ion Thruster. I. Funaki, B02-010 Flow Control via Rotor Trailing Edge Blowing in a H. Kuninaka, K. Toki, Y. Shimizu, and K. Nishiyama, /nstitute of Rotor/Stator Axial Compressor. A. M. Wo, A. C. Lo, and W. C. Space and Astronautical Science, Japan; and Y. Horiuchi, NEC Chang, National Taiwan University, Taiwan, ROC (18, 1, p. 93) Aerospace Systems, Ltd., Japan (18, 1, p. 169) Article Article B02-021 Cascade Arc Studies of Hydrogen/Nitrogen Plasmas B02-611 Active Control of Discrete-Frequency Noise in Nonequilibrium. Trevor Moeller, Dennis Keefer, and Robert Generated by Rotor-Stator Interactions. Scott Sawyer and Rhodes, University of Tennessee Space Institute (18, 1, p. 176) Sanford Fleeter, Purdue University; and John Simonich, United Article Technologies Research Center (18, 1, p. 100) Article B02-022 Flow Past Stationary Spherical Particles with B02-612 Shock Fitting a Transonic Cascade Solution into an Streamwise Velocity Fluctuation. A. Dasgupta, Quest, Inc.; and Inverse Design Technique. Jeffrey W. Yokota and Adam J. Medd, T. I-P. Shih, Michigan State University (18, 1, p. 184) Article University of Alberta, Canada (18, 1, p. 107) Article B02-023 Reduced Chemical Kinetic Mechanisms for B02-013 Experimental and Analytical Design Verification of Hydrocarbon Fuels. Christopher J. Montgomery and Marc A. the Dual-Bell Concept. Gerald Hagemann, Michael Terhardt, and Cremer, Reaction Engineering International; Jyh-Yuan Chen, Dietrich Haeseler, Astrium GmbH, Germany; and Manuel Frey, University of California; Charles K. Westbrook, Lawrence DLR, German Aerospace Research Center, Germany (18, 1, p. 116) Livermore National Laboratory; and Lourdes Q. Maurice, U.S. Air Article based on AIAA Paper 2000-3778 Force Research Laboratory (18, 1, p. 192) Article 1322 J. PROPULSION, VOL. 18, NO. 6: 2002 INDEX B02-024 Two-Dimensional Spectroscopic Analysis of a Flame B02-035 Computations of Axisymmetric Plug-Nozzle Using Highly Preheated Combustion Air. Noriyuki Konishi, Flowfields: Flow Structures and Thrust Performance. Takashi Kuniyuki Kitagawa, and Norio Arai, Nagoya University, Japan; Ito, University of Tokyo, Japan; Kozo Fujii, Institute of Space and Astronautical Science, Japan, and A. Koich Hayashi, Aoyama and Ashwani K. Gupta, University of Maryland (18, 1, p. 199) Gakuin University, Japan (18, 2, p. 254) Article based on AIAA Article Paper 99-3211 B02-025 Anomalous Deflagration Behavior of Ammonium B02-036 Numerical Simulation of Side Loads in an Ideal Perchlorate at Elevated Pressures. Satyanarayanan R. Truncated Nozzle. Sébastien Deck and Philippe Guillen, ONERA, Chakravarthy, Edward W. Price, Robert K. Sigman, and Jeffrey M. France (18, 2, p. 261) Article Freeman, Georgia Institute of Technology (18, 1, p. 205) Technical Note B02-037 Design Analysis of a Satellite Hydrazine Propulsion System. An-Shik Yang, Da Yeh University, Taiwan, ROC; and Tien- B02-026 Effects of GH2/LOX Velocity and Momentum Ratios Chuan Kuo, National Space Program Office, Taiwan, ROC (18, 2. p. 270) Article on Shear Coaxial Injector Atomization. M. Ferraro, R. J. Kujala, J.-L. Thomas, M.J. Glogowski, and M. M. Micci, The Pennsylvania B62-038 Leak Fault Detection of Liquid Rocket Engine Based State University (18, 1, p. 209) Technical Note on Strong Tracking Filter. Yu Daren and Wang Jianbo, Harbin Institute of Technology, ROC (18, 2, p. 280) Article B02-027 Equation for Additive Drag Coefficient at Static Conditions. K. L. Christensen, KC Consulting Engineering B02-039 Temperature-Dependent Modal Test/Analysis (18, 1, p. 211) Technical Note Correlation of X-34 FASTRAC Composite Rocket Nozzle. Technical Comment by William H. Heiser, U.S. Air Andrew M. Brown, University of North Carolina at Charlotte (18, 2, p. 284) Article based on AIAA Paper 2000-1741 Force Academy; and Jack D. Mattingly, Seattle University (18, 4, p. 967) B02-040 Characteristic Analysis of Flow-Induced Vibrations Reply (18, 4, p. 968) on Inducer of Oxygen Pump. Liang Hengli and Chen Zuoyi, Tsinghua University, ROC (18, 2, p. 289) Article B02-028 Intercusp Electron Transport in an NSTAR- Derivative Ion Thruster. John E. Foster, NASA John H. Glenn B02-041 Numerical Predictions of Channel Flows with Fluid Research Center at Lewis Field (18, |, p. 213) Technical Note Injection Using Reynolds-Stress Model. Bruno Chaouat, ONERA, France (18, 2, p. 295) Article B02-029 Optimal Three-Dimensinal Nozzle Shape Design Using CFD and Parallel Simulated Annealing. X. Wang and M. B02-042 Effect of Nozzle Cavity on Resonance in Large SRM: Theoretical Modeling. J. Anthoine and J-M. Buchlin, von Karman Damodaran, Nanyang Technological University, Singapore (18, |, Institute for Fluid Dynamics, Belgium, and A. Hirschberg, p. 217) Technical Note Technische Universiteit Eindhoven, The Netherlands (18, 2, p. 304) Article based on AIAA Paper 2001-2102 B02-030 Propagation of Acoustic Waves in a Two-Phase Vaporizing Mixture. Joé] Dupays and Francois Vuillot, ONERA, B02-043 Dynamic Combustion of Solid Propellants: Effects of France (18, 1, p. 222) Technical Note based on AIAA Paper 98- Unsteady Condensed Phase Degradation Layer. K. R. Anil 3696 Kumar, /ndian Institute of Science, India, and K. N. Lakshmisha, Indian Institute of Science, India (18, 2, p. 312) Article B02-031 Multilevel Analysis of Pulsed Detonation Engines. Houshang B. Ebrahimi, Sverdrup Technology, Inc.; and Rajendran B02-044 Slingatron: A High Velocity Rapid Fire Sling. Derek A. Tidman, Advanced Launch Corporation (18, 2, p. 322) Article Mohanraj and Charles L. Merkle, University of Tennessee (18, 2, p. 225) Article B02-045 Sizing a Slingatron-Based Space Launcher. Mark L. Bundy, U.S. Army Research Laboratory, Derek A. Tidman, B02-032 Development of Advanced Industrial Furnace Using Advanced Launch Corporation, and Gene R. Cooper, U.S. Army Highly Preheated Combustion Air. T. Hasegawa and S. Mochida, Research Laboratory (18, 2, p. 330) Article Nippon Furnace Kogyo Kaisha Ltd., Japan; and A. K. Gupta, University of Maryland (18, 2, p. 233) Article B02-046 Numerical Simulations of the Slingatron. G. R. Cooper, U.S. Army Research Laboratory; D. A. Tidman, Advanced B02-033 Effects of Liquid-Oxygen Post Biasing on SSME Launch Corporation, and M. L. Bundy, U.S. Army Research Injector Wall Compatibility. P. A. Strakey and D. G. Talley, U.S. Laboratory (18, 2, p. 338) Article Air Force Research Laboratory; and L. K. Tseng and K. I. Miner, B02-047 Ethylene Ignition and Detonation Chemistry, Part 1: Boeing Rocketdyne Propulsion and Power (18, 2, p. 240) Detailed Modeling and Experimental Comparison. B. Article Varatharajan and F. A. Williams, University of California (18, 2, p. 344) Article B02-034 Time- and Length Scales of Combustion in Liquid Rocket Thrust Chambers. B. Ivancic and W. Mayer, DLR, B02-048 Ethylene Ignition and Detonation Chemistry, Part 2: German Aerospace Center, Germany (18, 2, p. 247) Article based Ignition Histories and Reduced Mechanisms. B. Varatharajan on AIAA Paper 99-2211 and F. A. Williams, University of California (18, 2, p. 352) Article