Table Of Content

JOURNAL OF PROPULSION AND POWER Volume 20, No. 6, November—December 2004 2004 Journal of Propulsion and Power Index How to Use the Index In the Subject Index, pages 1136—1140, 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, page 1141-1142, lists all authors associated with a given technical paper. The locating numbers are identical to those in the Subject Index. The Chronological Index, pages 1143-1149, 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. Comments, Replies, and Errata are listed direct- ly beneath the paper to which they refer. If the paper to which they refer was published prior to 2004, 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, Noise Rotating Machinery CONVENTIONAL, STOL/VTOL B04-059 Acoustic Characteristics of Supersonic B04-018 Experimental Study on Linear Com- Jets from Grooved Nozzles pressor Cascade with Three-Dimensional Blade Aerodynamics B04-026 Engine Cycle and Exhaust Configura- Oscillation tion for Quiet Supersonic Propulsion B04-059 Acoustic Characteristics of Supersonic Solar Power Jets from Grooved Nozzles Performance B04-102 Oscillation Frequency in Wake of a Vee B04-106 Maximum Power Tracking and Pulse B04-003 Concorde and the Future of Supersonic Width-Modulated Shunt for Satellite Power Sys- Gutter Transport tems B04-112 Scramjet Inlet Flow Control Using Combined Magnetohydrodynamics and Glow- Powerplant Integration FLUID DYNAMICS Discharge-Plasma Effect B04-064 Advanced Coal Power Cycle with a Stand-Alone Magnetohydrodynamic Generator Aeroacoustics Aeroelasticity and Aeroservoelasticity B04-059 Acoustic Characteristics of Supersonic Simulation B04-018 Experimenta! Study on Linear Com- Jets from Grooved Nozzles B04-035 Parametric Design of Turbomachinery pressor Cascade with Three-Dimensional Blade B04-026 Engine Cycle and Exhaust Configura- Airfoils Using Highly Differentiable Splines Oscillation tion for Quiet Supersonic Propulsion ENERGY Aerospace Plane Computational Fluid Dynamics B04-091 Analysis of the Magnetohydrodynamic Alternate Fuels B04-015 Internal Degrees of Freedom of an Actuator Disc Model Energy Bypass Engine for High-Speed Air- B04-128 Oxidation Processes and Phase B04-063 Three-Dimensional Multi-Objective breathing Propulsion Changes in Metastable Al-Mg Alloys Design Optimization of a Transonic Compressor Rotor Air Transportation Magnetohydrodynamic Power B04-058 Numerical Simulation of Separated Generation B04-003 Concorde and the Future of Supersonic Cold Gas Nozzle Flows Transport B04-064 Advanced Coal Power Cycle with a B04-069 Transonic Axial-Flow Blade Optimiza- Stand-Alone Magnetohydrodynamic Generator tion: Evolutionary Algorithms/Three-Dimen- Fuels and Fuel Systems sional Navier-Stokes Solver Photovoltaic Power B04-037 Compressible Subsonic Particle-Laden B04-047 Ignition Delays of Heptane/O,/Ar Mix- B04-106 Maximum Power Tracking and Pulse- Flow over a Square Cylinder tures in the 1300-1600 K Temperature Width-Modulated Shunt for Satellite Power Sys- B04-130 Large-Eddy Simulation of Pollutant Range tems Emission in a DOE-HAT Combustor 1136 JOURNAL OF PROPULSION AND POWER Volume 20, No. 6, November—December 2004 2004 Journal of Propulsion and Power Index How to Use the Index In the Subject Index, pages 1136—1140, 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, page 1141-1142, lists all authors associated with a given technical paper. The locating numbers are identical to those in the Subject Index. The Chronological Index, pages 1143-1149, 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. Comments, Replies, and Errata are listed direct- ly beneath the paper to which they refer. If the paper to which they refer was published prior to 2004, 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, Noise Rotating Machinery CONVENTIONAL, STOL/VTOL B04-059 Acoustic Characteristics of Supersonic B04-018 Experimental Study on Linear Com- Jets from Grooved Nozzles pressor Cascade with Three-Dimensional Blade Aerodynamics B04-026 Engine Cycle and Exhaust Configura- Oscillation tion for Quiet Supersonic Propulsion B04-059 Acoustic Characteristics of Supersonic Solar Power Jets from Grooved Nozzles Performance B04-102 Oscillation Frequency in Wake of a Vee B04-106 Maximum Power Tracking and Pulse B04-003 Concorde and the Future of Supersonic Width-Modulated Shunt for Satellite Power Sys- Gutter Transport tems B04-112 Scramjet Inlet Flow Control Using Combined Magnetohydrodynamics and Glow- Powerplant Integration FLUID DYNAMICS Discharge-Plasma Effect B04-064 Advanced Coal Power Cycle with a Stand-Alone Magnetohydrodynamic Generator Aeroacoustics Aeroelasticity and Aeroservoelasticity B04-059 Acoustic Characteristics of Supersonic Simulation B04-018 Experimenta! Study on Linear Com- Jets from Grooved Nozzles B04-035 Parametric Design of Turbomachinery pressor Cascade with Three-Dimensional Blade B04-026 Engine Cycle and Exhaust Configura- Airfoils Using Highly Differentiable Splines Oscillation tion for Quiet Supersonic Propulsion ENERGY Aerospace Plane Computational Fluid Dynamics B04-091 Analysis of the Magnetohydrodynamic Alternate Fuels B04-015 Internal Degrees of Freedom of an Actuator Disc Model Energy Bypass Engine for High-Speed Air- B04-128 Oxidation Processes and Phase B04-063 Three-Dimensional Multi-Objective breathing Propulsion Changes in Metastable Al-Mg Alloys Design Optimization of a Transonic Compressor Rotor Air Transportation Magnetohydrodynamic Power B04-058 Numerical Simulation of Separated Generation B04-003 Concorde and the Future of Supersonic Cold Gas Nozzle Flows Transport B04-064 Advanced Coal Power Cycle with a B04-069 Transonic Axial-Flow Blade Optimiza- Stand-Alone Magnetohydrodynamic Generator tion: Evolutionary Algorithms/Three-Dimen- Fuels and Fuel Systems sional Navier-Stokes Solver Photovoltaic Power B04-037 Compressible Subsonic Particle-Laden B04-047 Ignition Delays of Heptane/O,/Ar Mix- B04-106 Maximum Power Tracking and Pulse- Flow over a Square Cylinder tures in the 1300-1600 K Temperature Width-Modulated Shunt for Satellite Power Sys- B04-130 Large-Eddy Simulation of Pollutant Range tems Emission in a DOE-HAT Combustor 1136 B04-108 Simu ym and Prediction of Ma B04-024 Unsteady Flows Propellant Reorientation in Reduced Grav Plun B04-018 Experimental Study on Linear Com- B04-103 Nu al Simulation of Ho B04-083 ide with Three-Dimensional Blade Nozzle Fl ] netohydrody B04-070 M ( ctive Shape Opti Study for c Submerged Inlet B04-119 GUIDANCE, CONTROL, AND DYNAMICS TECHNOLOGY Hypersonic Flow Reacting Flows and Combustion B04-042 | ital Evaluation Control Theory njet Inlets B04-109 Combustion Instability Con H ocity Fuel/Air Mix IX ration: Theory and validation Fuel B04-040 Inlet, Nozzle, Diffuser, and Channel Flows B04-010 ing of Surge in Free-Spool Cen- ssors: Experimental Validation B04-042 | tal Evaluation So amyjet Inlets B04-124 nization Techniques Multistage Compre Dp et-Compressor | Dimensional Multi-Objective S ons of Normal n of a Transonic Compressor Interactior Separated Flows B04-070 M Objective Shape Opt B04-036 INTERDISCIPLINARY TOPICS udy fo S ic Submerged Inlet B04-060 | ental Investigation « (nalytical and Numerical Methods ed Noz B04-058 Dimensional Model for Prelimi- Cold G \blative Pulsed Plasma Teflon Jets, Wakes, and Viscid-Inviscid Flow B04-078 Interactions | B04-060 Vultidisciplinary Design Optimization B04-061 Eff f Delta Tabs on Axis Sw ed No yf a Coaxial ire Jet B04-069 Transonic Axial-Flow Blade Optimiza- B04-103 N B04-102 Oscillation Frequency in Wake of tionary Algorithms/Three-Dimen- t Stokes Solver B04-029 Sx Injection into a Macl ticriteria Design Optimization of a Shock Waves and Detonations Freestream Through Diamond Orifices let Based upon Global Missile Per B04-039 New Particle-Image-Velocimetry Method B04-095 to Measure Flowfields in Luminous Spray Flames gation B04-036 S Research Facilities and Instrumentation Multiphase Flows B04-076 e-Resolved Fuel-Grain Port Diam- B04-037 Compressible Subsonic Particle-Lad rementin Hybrid Rockets Flow over a Square Cylinder Supersonic Flow B04-068 Simulatios Cavitating FI Sensor Systems Turbopumy B04-078 Side-Load Phenor B04-085 | Circuit Sensor Array for Surface B04-043 Nucleation Mechanism for the Freez expande |1 K2 OCK >t Dp ssure Measurements ing of Alumina in Solid Propellant Rocket Motor B04-058 Nu Nozzles Cold Gas N¢ LAUNCH VEHICLE AND MIS- B04-095 Heterogeneous Effects in the Prop B04-087 Dual-Mode Operations SILE (LV/M) TECHNOLOGY tion and Quenching of Spray Detonations Combusto! Missile Systems Plasmadynamics and MHD Transonic Flow B04-062 Multicriteria Design Optimization of a B04-118 Propellant Charring in Pulsed Plasma B04-085 Flex Circuit Sensor Art Supersonic Inlet Based upon Global Missile Per- Thrusters Unsteady Pressure Measurements B04-116 Electromagnetic Effects in the Near B04-084 High Spatial Resolutio B04-002 A Century of Ramjet Propulsion Tech- Field Plume Exhaust of a Micro-Pulsed-Plasma Forced Response in a Transonic Evolution Thruster SOI Propulsion and Propellant Systems B04-112 Scramjet Inlet Flow Control Using B04-134 Mach Number/Surface Combined Magnetohydrodynamics and Glow Effects on Symmetric Transonic Turb B04-040 Reaction Rates for Hypergolic Propel- Discharge-Plasma Effect \erody namic Losses its Using Chemical Delay Times 1138 J. PROPULSION, VOL. 20, NO. 6: 2004 INDEX B04-041 Propulsion System Instability for Con- B04-027 Hypervelocity Fuel/Air Mixing in a B04-076 Time-Resolved Fuel-Grain Port Diam- centric Tank-Type Launch Vehicle Shcramjet Inlet eter Measurementin Hybrid Rockets B04-104 Combined H,O/CO, Solid Oxide Elec- B04-017 Three-Dimensional Time-Resolved trolysis for Mars In Situ Resource Utilization Inlet Guide VanefRotor Potential Field Interac- Detonation B04-008 Development of Laboratory-Scale Gel tion B04-047 Ignition Delays of Heptane/O,/Ar Propulsion Technology B04-038 Methane Dissociation in Pulsed dec Mixtures in the 1300-1600 K Temperature B04-043 Nucleation Mechanism for the Freez- Discharges at High Reduced Electric Field Range ing of Alumina in Solid Propellant Rocket Motor B04-096 Gas-Turbine Performance Improve- B04-110 Performance Evaluation Method for Nozzles ments Through the Use of Multiple Turbine Ideal Airbreathing Pulse Detonation Engines B04-129 Decomposition of Hydrogen Peroxide Interstage Burners B04-124 Deflagration to Detonation Transition on MnO,/TiO, Catalysts B04-101 Frequency Veering Effects on Mis- Processes by Turbulence-Generating Obstacles B04-054 Pressure Control Analysis of Cryo- tuned Bladed Disk Forced Response in Pulse Detonation Engines genic Storage Systems B04-030 Mach 4 Performance of Hypersonic B04-007 Chemical Kinetic Model for Inlet with Rectangular-to-Elliptical Shape Tran- Monomethylhydrazine/Nitrogen Tetroxide Gas Simulation sition Phase Combustion and Hypergolic Ignition B04-124 Deflagration to Detonation Transition B04-116 Electromagnetic Effects in the Near B04-111 Impulse Correlation for Partially Filled Processes by Turbulence-Generating Obstacles Field Plume Exhaust of a Micro-Pulsed-Plasma Detonation Tubes in Pulse Detonation Engines Thruster B04-095 Heterogeneous Effects in the Propaga- B04-110 Performance Evaluation Method for tion and Quenching of Spray Detonations Ideal Airbreathing Pulse Detonation Engines Thermal Protection Systems B04-028 Experimental Study on Restart Control Droplet and Spray Characterization B04-044 Asymmetric Base-Bleed Effect on of a Supersonic Air-Breathing Engine Aerospike Plume-Induced Base-Heating Envi- B04-056 Model for Multistage Compressors to B04-082 Characterization of a Six-Emitter Col- ronment Predict Unsteady Inlet-Compressor Interactions loid Thruster Using a Torsional Balance B04-062 Multicriteria Design Optimization of a B04-005 Characteristics of Sprays Formed by PROPULSION Supersonic Inlet Based upon Global Missile Per- Impingement of a Pair of Liquid Jets formance B04-004 Orifice Diameter Ratio Effect on the Advanced Space Propulsion Mixing Performances for Split Triplet Injectors B04-083 Performance Theory of Diagonal Con- Combustion and Combustor Designs B04-039 New Particle-Image-Velocimetry Me- thod to Measure Flowfields in Luminous Spray ducting Wall Magnetohydrodynamic Accelera- B04-046 Kinetic Modeling of Heptane Combus- Flames tors tion and PAH Formation B04-088 Electric Sail for Spacecraft Propulsion B04-075 Interaction of Capillary Plasma with Ducted Rocket Engines B04-011 Novel High Nitrogen Propellant Use in Double-Base and Composite Propellants Solid Fuel Micropropulsion B04-130 Large-Eddy Simulation of Pollutant B04-109 Performance Prediction of a Ducted B04-121 Micropropulsion Using a Laser Abla- Emission in a DOE-HAT Combustor Rocket Combustor Using a Simulated Solid Fuel tion Jet B04-122 Effect of Paramagnetism and Diamag- B04-120 Characterization of Cathode Keeper netism on Theoretical Rocket Performance Electric Propulsion Wear by Surface Layer Activation B04-125 Scale-Up Tests of High Regression B04-119 Plasma Properties in the Plume of a Rate Paraffin-Based Hybrid Rocket Fuels Hall Thruster Cluster Airbreathing Propulsion B04-109 Performance Prediction of a Ducted B04-083 Performance Theory of Diagonal Con- B04-090 Mixing and Combustion Studies Using Rocket Combustor Using a Simulated Solid ducting Wall Magnetohydrodynamic Accelera- Cavity-Based Flameholders in a Supersonic Fuel tors Flow B04-040 Reaction Rates for Hypergolic Propel- B04-020 A Critical History of Electric Propul- B04-094 Effect of Porous Thrust Surfaces on ants Using Chemical Delay Times sion: The First 50 Years (1906-1956) Detonation Transition and Detonation Tube B04-010 Ultrasonic Measurement of the Pres- B04-022 Indium Field Emission Electric Propul- Impulse sure-Coupled Response Function for Composite sion Microthruster Experimental Characteriza- B04-091 Analysis of the Magnetohydrodynamic Solid Propellants ton Energy Bypass Engine for High-Speed Air- B04-005 Characteristics of Sprays Formed by B04-023 2000-Hour Endurance Test of Indium breathing Propulsion Impingement of a Pair of Liquid Jets Field Emission Electric Propulsion B04-111 Impulse Correlation for Partially Filled B04-011 Novel High Nitrogen Propellant Use in Microthruster Cluster Detonation Tubes Solid Fuel Micropropulsion B04-024 lIon-Energy Diagnostics in an SPT-100 B04-003 Concorde and the Future of Supersonic Plume from Thrust Axis to Backflow Transport Combustion Instability B04-117 Zero-Dimensional Model for Prelimi- B04-001 Ideas and Methods of Turbomachinery B04-126 Mathematical Modeling of the Devel- nary Design of Ablative Pulsed Plasma Teflon Aerodynamics: A Historical View opment of Anomalous Processes in High-Load- Thrusters B04-092 Assessment of Solid Hydrogen Slurry ing-Density Solid Propulsion Systems B04-116 Electromagnetic Effects in the Near Fueling for an Airbreathing Supersonic Combus- B04-012 Unsteady Stolid Propellant Pressure Field Plume Exhaust of a Micro-Pulsed-Plasma tor Combustion Responses Using a Piston Burner Thruster B04-087 Dual-Mode Operations in a Scramjet B04-131 Adaptive Combustion Instability Con- B04-136 Vacuum Chamber Pressure Maps of a Combustor trol with Saturation: Theory and validation Hall Thruster Cold-Flow Expansion J. PROPULSION, VOL. 20, NO. 6: 2064 INDE) 1139 B04-082 Characterization of a Six-Emitter Col- B04-007 Chemical Kinetic Model B04-028 Experimental Study on Restart Control loid Thruster Using a Torsional Balance Monomethylhydrazine/Nitrogen Tetroxide of a Supersonic Air-Breathing Engine B04-118 Propellant Charring in Pulsed Plasma Phase Combustion and Hypergolic Ignition B04-029 Sonic Injection into a Mach 5.0 hrusters B04-008 Development of Laboratory-Scale Freestream Through Diamond Orifices B04-105 A Power Conversion Concept for the Propulsion Technology B04-030 Mach 4 Performance of Hypersonic Jupiter Icy Moons Orbiter B04-127 Using Aluminum for Space P1 Inlet with Rectangular-to-Elliptical Shape Tran- B04-120 Characterization of Cathode Keeper B04-129 Decomposition of Hydrog Wear by Surface Layer Activation on MnO,/TiO, Catalysts B04-108 Simulation and Prediction of Magr Ignition Emissions and Noises Propellant Reorientation in Reduced G B04-075 Interaction of Capillary Plasma with B04-128 Oxidation Processes B04-130 Large-Eddy Simulation of Pollutant Double-Base and Composite Propellants Changes in Metastable Al-Mg Alloy Emission in a DOE-HAT Combustor B04-031 Supersonic Flow Ignition by Plasma B04-006 Propulsive Performance of H Torch and H,/O, Torch H,0,/Kerosene Bipropellant Engine Control Integration and Health B04-007 Chemical Kinetic Model for Monitoring Monomethylhydrazine/Nitrogen Tetroxide Gas Gas Turbine Engines Phase Combustion and Hypergolic Ignition B04-032 High-Pressure-Turbine Clearance Con- B04-001 Ideas and Methods of Turbomac B04-127_ Using Aluminum for Space Propulsion trol Systems: Current Practices and Future Aerodynamics: A Historical View B04-006 Propulsive Performance of Hypergolic Directions B04-134 Mach Number/Surface R H,O./Kerosene Bipropellant Effectso n Symmetric Transonic Turbine Airf B04-126 Mathematical Modeling of the Devel- Engine Cooling and Heat Transfer Aerodynamic Losses ypment of Anomalous Processes in High-Load- B04-044 Asymmetric Base-Bleed Effect on B04-017 Three-Dimensional Time-Resol\ ng-Density Solid Propulsion Systems Aerospike Plume-Induced Base-Heating Envi Inlet Guide VanenRotor Potential Field Int ronment tion Liquid Rocket Engines B04-133 Vane-Endwall Junction Optimization B04-096 Gas-Turbine Performance I B04-006 Propulsive Performance of Hypergolic to Reduce Turbine Vane Passage Adiabatic Wall ments Through the Use of Multipl H,O./Kerosene Bipropellant Temperatures Interstage Burners B04-055 Full- and Partial-Admission Perfor- B04-132 Rotor-Bearing Analysis for T nce of a Simplex Turbine Engine Materials chinery Single- and Dual-Rotor Syst B04-005 Characteristics of Sprays Formed by B04-135 Compatibility of Injector Materials B04-133 Vane-Endwall Junction Opt ngement of a Pair of Liquid Jets with Hydrogen Peroxide Propellant to Reduce Turbine Vane Passage Adiat B04-103 Numerical Simulation of Hot Gas Noz- Temperatures Engine Performance B04-110 Performance Evaluation M B04-014 Designing and Testing a Lighter, Ideal Airbreathing Pulse Detonation Eng B04-122 Effect of Paramagnetism and Diamag Simpler, Less-Expensive Liquid-Propellant netism on Theoretical Rocket Performance B04-033 High-Speed, High-Temperatur es Seal Test Results B04-096 Gas-Turbine Performance Improve B04-008 Development of Laboratory-Scale Gel B04-032 High-Pressure-Turbine Clearan ments Through the Use of Multiple Turbine Propulsion Technology trol Systems: Current Practices at Interstage Burners B04-122 Effect of Paramagnetism and Diamag- Directions B04-032 High-Pressure-Turbine Clearance Con on Theoretical Rocket Performance B04-102 Oscillation Frequency in Wak trol Systems: Current Practices and Future B04-078 Side-Load Phenomena in Highly Over- Gutter Directions ded Rocket Nozzles B04-033 High-Speed, High-Temperature Finger B04-035 Parametric Design of Turb B04-068 Simulations of Cavitating Flows in ery Airfoils Using Highly Diff nps Seal Test Results Splines B04-002 A Century of Ramjet Propulsion Tech nology Evolution Propulsion Hazards Hybrid Rocket Engines B04-135 Compatibility of Injector Materials Fuels and Propellants, Properties of B04-076 Time-Resolved Fuel-Grain P lrogen Peroxide Propellant eter Measurementin Hybrid Rockets B04-047 Ignition Delays of Heptane/O,/Ar Mix B04-125 Scale-Up Tests of High R Ramjets and Scramjets tures in the 1300-1600 K Temperature Range Rate Paraffin-Based Hybrid Rocket Fue B04-046 Kinetic Modeling of Heptane Combus B04-087 Dual-Mode Operations in a Scramjet tion and PAH Formation B04-127 Using Aluminum for Space Pr — B04-039 New Particle-Image-Velocimetry Me B04-129 Decomposition of Hydrogen P B04-042 Experimental Evaluation for Mass on MnO,/TiO, Catalysts thod to Measure Flowfields in Luminous Spray Capture Ratio of Scramjet Inlets Flames B04-031 Supersonic Flow Ignition by Plasma B04-048 Combustion Characteristics of Alu Hypersonic Propulsion Torch and H,/O; Torch minum Hydride at Elevated Pressure and Tem- B04-038 Methane Dissociation in P B04-028 Experimental Study on Restart Control perature Discharges al High Reduced Electric | »f a Supersonic Air-Breathing Engine B04-135 Compatibility of Injector Materials B04-027 Hypervelocity Fuel/Air Mixing B04-038 Methane Dissociation in Pulsed dec with Hydrogen Peroxide Propellant Shcramjet Inlet Discharges at High Reduced Electric Field 1140 J. PROPULSION, VOL. 20, NO. 6: 2004 INDEX B04-091 Analysis of the Magnetohydrodynamic B04-069 Transonic Axial-Flow Blade Optimiza- B04-136 Vacuum Chamber Pressure Maps of Energy Bypass Engine for High-Speed Air- tion: Evolutionary Algorithms/Three-Dimen- Hall Thruster Cold-Flow Expansion breathing Propulsion sional Navier-Stokes Solver B04-119 Plasma Properties in the Plume of B04-092 Assessment of Solid Hydrogen Slurry B04-068 Simulations of Cavitating Flows in Hall Thruster Cluster Fueling for an Airbreathing Supersonic Combustor Turbopumps B04-112 Scramjet Inlet Flow Contro! Using B04-085 Flex Circuit Sensor Array for Surface Spacecraft Test and Evaluation Combined Magnetohydrodynamics and Glow- Unsteady Pressure Measurements B04-136 Vacuum Chamber Pressure Maps of Discharge-Plasma Effect B04-099 Modeling of Surge in Free-Spool Cen- Hall Thruster Cold-Flow Expansion trifugal Compressors: Experimental Validation Solid Rocket Motors B04-084 High Spatial Resolution Upstream STRUCTURAL MECHANICS Forced Response in a Transonic Compressor B04-113 Studies on Advanced CL-20-Based AND MATERIALS B04-063 Three-Dimensional Multi-Objective Composite Modified Double-Base Propellants Design Optimization of a Transonic Compressor B04-126 Mathematical Modeling of the Devel- Structural Durability (Including Fatigue, Rotor opment of Anomalous Processes in High-Load- Fracture, and Environmental B04-101 Frequency Veering Effects on Mis- ing-Density Solid Propulsion Systems Degradation) tuned Bladed Disk Forced Response B04-011 Novel High Nitrogen Propellant Use in B04-101 Frequency Veering Effects on Mis B04-132 Rotor-Bearing Analysis tor Turboma- Solid Fuel Micropropulsion tuned Bladed Disk Forced Response chinery Single- and Dual-Rotor Systems B04-043 Nucleation Mechanism for the Freez- B04-133 Vane-Endwall Junction Optimization ing of Alumina in Solid Propellant Rocket Motor Structural Dynamics and to Reduce Turbine Vane Passage Adiabatic Wall Nozzles Characterization Temperatures B04-012 Unsteady Stolid Propellant Pressure B04-015 Internal Degrees of Freedom of an B04-041 Propulsion System Instability for Con- Combustion Responses Using a Piston Burner Actuator Disc Model centric Tank-Type Launch Vehicle B04-048 Combustion Characteristics of Alu- B04-016 Approach to High-Performance Tran- minum Hydride at Elevated Pressure and Tem- sonic Compressor Design Structural Optimization perature B04-017 | Three-Dimensional Time-Resolved Inlet B04-100 Preliminary Fan-Blade Design Using Guide Vane—Rotor Potential Field Interaction Supersonic Combustion Intermediate Response Approximations B04-031 Supersonic Flow Ignition by Plasma SPACE TECHNOLOGY Torch and H,/O, Torch THERMOPHYSICS AND HEAT B04-090 Mixing and Combustion Studies Using TRANSFER Humans in Space/Life Support Systems, Cavity-Based Flameholders in a Supersonic EVA Flow Aerothermodynamics/Thermal Protection B04-104 Combined H,O/CO, Solid Oxide B04-092 Assessment of Solid Hydrogen Slurry B04-044 Asymmetric Base-Bleed Effect on Electrolysis for Mars In Situ Resource Utiliza- Fueling for an Airbreathing Supersonic Combus- Aerospike Plume-Induced Base-Heating Envi- tion tor ronment Space Systems Turbomachinery Cryogenics B04-104 Combined H,O/CO, Solid Oxide B04-055 Full- and Partial-Admission Perfor- B04-054 Pressure Control Analysis of Cryo- Electrolysis for Mars In Situ Resource Utiliza- mance of a Simplex Turbine genic Storage Systems tion B04-001 Ideas and Methods of Turbomachinery B04-108 Simulation and Prediction of Magnetic Aerodynamics: A Historical View Propellant Reorientation in Reduced Gravity Nonintrusive Diagnostics B04-134 Mach Number/Surface Roughness B04-010 Ultrasonic Measurement of the Pres- Effects on Symmetric Transonic Turbine Airfoil Spacecraft Power sure-Coupled Response Function for Composite Aerodynamic Losses B04-014 Designing and Testing a Lighter, Sim- B04-105 A Power Conversion Concept for the Solid Propellants pler, Less-Expensive Liquid-Propellant Pump Jupiter Icy Moons Orbiter B04-035 Parametric Design of Turbomachinery Thermal Modeling and Analysis \irfoils Using Highly Differentiable Splines Spacecraft Propulsion System B04-106 Maximum Power Tracking and Pulse- Integration B04-056 Model for Multistage Compressors to Width-Modulated Shunt for Satellite Power Systems Predict Unsteady Inlet-Compressor Interac- B04-105 A Power Conversion Concept for the B04-064 Advanced Coal Power Cycle with a tons Jupiter ley Moons Orbiter Stand-Alone Magnetohydrodynamic Generator J. PROPULSION, VOL 20, NO. ¢ Author Index Ahuja, V., B04-068 Cooper, M., B04-094, B04-111 Gupta, A.K B04-039. B04-107 Knowlen, C., B04-093 Akiyama, 1 B04-107 Corral, Roque, B04-035 Haas, James M B04-119 Kobayashi, Kan, B04-031 Ali, A. N., B04-011 Cumpsty, N. A., B04-001 Hafenrichter, Thomas J . B04-010 Koff, Bernard L., B04-066 Aliev, Ali V., B04-126 D’ Agostino, Mark, B04-044 Hampton, Casey S., B04-040 Kohga, Makota, B04-013 Anderson, William R., B04-050 Damgaard, Tomas, B04-078 Hargus, W B04-119 Kojima, Takayuki, B04-028 Annaswamy, A. M., B04-131 Davis, Roger L., B04-096 Harris, P B04-109 Kolasinski, Robert D., B04-120 Anthoine, J., B003-002 deChamplain, Alain, B04-109 Hartfield, R BO04-077 Komatsu, Keiji, B04-041 Antonsen, Erik, B04-116 de Jager, Bram, B04-099 Hasan. Dx B04-008 Konishi, N., B04-107 Antonsen, Erik L., B04-118 le la Mora, Juan Fernandez, Hasan, Mol mad M B04-054 Kopriva, D. A., B04-037 Arai, N., B04-107 B04-081 Hauer, Mar B04-121 Krier, H., B04-048 Archer, S., B04-039 Delgado, Irebert R., B04-033 Heiser, William H B03-002 Krier, Herman, B04-010 Asthana, S. N., B04-086 De Zilwa, Shane, B04-076, B04-125 Heister, St B04-053 Kudo, Kenji, B04-073, B04-087 Asthana, Srinandan N., B04-113 Divekar, C. N., B04-113 He, | B04-018 Kumar, Arun, B04-033 Austin, J. M., BO3-002 Donbar, J. M., B04-090 Hiraiwa, 1 B04-042. BO4-073 Kuninaka, Hitoshi, B04-080 Babushok, V. I., B04-046 Dorney, Daniel J., B04-055 lI iskey, M. A BO04-011 Kuno, Naoki, B04-067 Bagnasco, Giovanni, B04-129 Dougal, Roger A., B04-106 Hochste B04-108 acas, F., B04-072 Baker John, B04-122 Dowling, A. P., B04-131 Hoffman, My1 \.. B04-096 attime, Scott B., B04-032 Bates, Stephen C., B04-092 Dreizin, Edward L., B04-128 Hosangadi, A B04-068 aw, Chung K., B04-095 Bazyn, T., B04-048 Droege, Alan, B04-044 Hsu, Chih-N BO4-132 awless, Patrick B., B04-097 Beal, Brian E., B04-119 Dubois, Charles, B04-109 Hsu, K.-¥ B04-090 awless, Patrick B., B04-098 Benini, Ernesto, B04-063 Dutton, J. C., B04-036 Huang, R B04-102 ear, W. E., B04-123 Bernier, D., B04-072 Edmunds, T. M., B04-100 Hunter, Craig A., B04-060 ee, Changjin, B04-049 Bhatewara, R. G., B04-086 Egeland, Olav, B04-099 Hutton, Timot M... B04-084 ee, Daina, B04-029 Bocanegra, Rodrigo, B04-081 Eggenspieler, G., B04-130 lacomini, Chi e S.. B04-104 ee, Jae-Woo, B04-049 Bowersox, Rodney D. W., B04-029 Elaskar, Sergio A., B04-117 Imbert, B1 B04-047 ee, Seong-Woong, B04-004 Boyd, lain, B04-118 Ertas, Bugra H., B04-071 Ingenito i, BO4-127 ee, Seong- Young, B04-124 Boyd, lain D., B04-116, B04-136 Ervin, Jamie S., B04-045 Isihara, At B04-051 ee, Young-Ching, B04-044 Brewster, M. Q., B04-012 Evesque, Stephanie, B04-131 Itoh, S., B04-107 eger, Timothy J., B04-084 Brito, Claude M., B04-117 Eyer, R., B04-048 Izumikawa, Mu B04-042 ger, T. J., B04-085 Brito, Hector H., B04-117 Fan, Huaiguo, B04-029 Jacobs. G. B.. B04-037 ethander, Andrew T., B04-133 Bruckner \. P., BO4-093 Farmer, Mark J., B04-040 Jackson, S. B03-002 iang, Dongbai, B04-006 Bruno, Claudio, B04-127 Finn, John E., B04-104 Jaiman., R. K.. B04-036 igrani, Phillip M., B04-134 Buchlin, J M.., BO2-042 Fleeter, Sanford, B04-017, B04-097, Janhunen, P B04-088 i, Jianquan, B04-075 Buldrini, N B04-023 B04-098 Jenkins Rhor 1 M.. BO4-077 i, Meilin, B04-034 Bundy, C., B04-093 rederick, Robert A., B04-013 Johnston, D \.. BO4-084 in, Chin S., B04-054 Burkhalter John E., B04-077 Frey, Manuel, B04-078 B04-085 inck, M., B04-039 Cai, Chunpei, B04-136 Fry, Ronald S., B04-002 Johnston, R B04-017 in, Feng, B04-034 ‘andel, S., B04-072 Fulayter, Roy D., B04-098 Jung, Ho-( B04-049 in, Liwu, B04-006i0u, Meng-Sing, ( ‘andel, Sebastien, B04-003 Funaki, [kkoh, B04-080 Kalitan, D M.. B04-074 B04-069 C ‘antwell, Brian J., B04-125 Furushima, S., B04-107 Kamhaw B04-025 ipanov, Alexey M., B04-126 ( ‘arter, ¢ D.., B04-090 Gaiddon, A., B04-062 Kanda, l B04-042, B04-073, ippert, Thomas, B04-121 Castellucci, Paul, B04-125 Gallimore, Alec D B04-024, B04-087 i, Tao, BO4-006 ( ‘atoire, Laurent, B04-007, B04-047 B04-119, BO4-136 Kandil, S itchford, Ron J., B04-083 ( ‘hakravarthy, Satyanarayanan Gamero-CastaOo, Manuel, Karabeyog B04-076 itzinger, Thomas A., B04-075 R., B04-009 B04-081, B04-082 B04-125 iu, Shengyi, B04-106 Chang, Kuo T., B04-102 Ganguly, Biswa N., B04-038 Kawamoto, O., B04-016 oth, E., B04-036 Chaumeix, Nabiha, B04-007, Gatsonis, Nikolaos A., B04-025 Kayukawa, N iki. BO4-064 ourenco, L., B04-039 B04-047 Genovese, A., B04-022, B04-023 Keane, A. J., B04-100 uke, James R., B04-121 Chen, Gordon, B04-096 Glumac, N., B04-048 Keidar, Michae B04-116, BO4-118 ukin, Alexander N., B04-126 Chen, Jingyi, B04-034 Gore, G. M., B04-086, B04-113 Kenyon, J. A B04-101 Lu, Tianfeng, B04-095 Cherny shenko, Sergei 1., BO4-015 Gostowski, Rudy, B04-135 Key, Nicole I B04-097 Ma, Lei, B04-006 Chiang, Hsiao-Wei D., B04-132 Gravdahl, Jan Tommy, B04-099 Kim, Byoung-Do, B04-053 Marchetta, Jeffrey G., B04-108 Chinzei, Nobuo, B04-073, B04-087 Greitzer, E. M., B04-001 Kim, N. E., B04-101 Marcum, S. Douglas, B04-038 Choueiri, E. Y., B04-020 Griffin, J. H., BO4-101 King, Lyon B., B04-024 Mashayek, F., B04-037 Cho, Yong-Ho, B04-004 Griffin, Lisa W., B04-055 Kitagawa, K B04-107 Mason, Lee S., B04-105 Chua, L. P., B04-061 Gross, A., B04-058, B04-103 Knight, Andrew, B04-014 Mayer, Alfons E. H. J., Bo4-109 Cong, Yu, B04-006 Gruber, M. R., B04-090 Knight, D. D B04-062 Mays, Lynette O., 804-040 Conrad, Chris, B04-124 Gulczinski III, Frank S., B04-118 Knight, Doyle D., B04-070 Menon, S., B04-130 1142 J. PROPULSION, VOL. 20, NO. 6: 2004 INDEX Mikellides, Pavlos G., B04-021 Pilone, Giuseppe, B04-129 Sigman, Robert K., B04-009 Vaidyanathan, Rajkumar, B04-079 Miller, Martin S., B04-050 Polk, James E., B04-120 Singh, Haridwar, B04-113 Vance, John M., B04-071 Mitani, Tohru, B04-031, B04-042 Poloni, C., B04-062 Sislian, Jean P., B04-027 Van Dresar, Neil T., B04-054 Morgan, Orenthral T., B04-122 Pratt, David T., B03-002 Sivabalan, R., B04-113 Vishnu, Jayant, B04-059 Moser, Marlow D., B04-013 Price, Edward W., B04-009 Smart, Michael K., B04-030 Wagner, Joel, B04-133 Murakami, Atsuo, B04-073, B04-087 Privalov, Aleksei V., B04-015 Smith Jr., James E., B04-040 Walker, Mitchell L. R., B04-136 Murphy, Jeffrey J., B04-010 Proctor, Margaret P., B04-033 Solodovnik, Eugene V., B04-106 Wang, Ten-See, B04-044 Nair, U. R., B04-113 Rahimi, Shai, B04-008 Sondak, Douglas L., B04-055 Wang, Xiaodong, B04-006 Nandakumar, K., B04-005 Ramamurthi, K., B04-005 Sonoda, Toyotaka, B04-067 Wang, X. K., B04-061 Naud, D. L., B04-011 Rathakrishnan, E., B04-059 Son, S. F., B04-011 Wang, Yongming, B04-064 Nazare, A. N., B04-086 Reinath, Michael, B04-076 Soukhomlinov, V., B04-112 Ward, Thomas, B04-045 Nikolayev, Olexiy, B04-041 Rickard, Matthew J. A., B04-074 Spanjers, Gregory G., B04-116, Watts, Jonathan, B04-124 Oana, M., B04-016 Riggins, David W., B04-091 B04-118 Weiland, C., B04-058, B04-103 Obayashi, Shigeru, B04-069 Riley, A. J., B04-131 Sridhar, K. R., B04-104 Wheelock, Adrian, B04-025 Ohkubo, Y., B04-107 Ringuette, Sophie, B04-109 Steiger, W., B04-022, B04-023 Willems, Frank, B04-099 Ohtani, H., B04-016 Rosner, Daniel E., B04-043 Steinetz, Bruce M., B04-032 Williams, Robert, B04-044 Ostlund, Jan, B04-078 Russo Sorge, Annamaria, B04-129 Stowe, Robert A., B04-109 Wintenberger, E., B03-002 Otugen, M. V., BO4-112 Saarloos, B., B04-012 Striebich, Richard C., B04-045 Witt, Jay, B04-077 Oyama, Akira, B04-069 Sajben, Miklos, B04-056 Sung, Hong-Gye, B04-057 Wokaun, Alexander, B04-121 Pack-Melton, LaTunia, B04-065 Santoro, Rovert, B04-124 Sun, Jiwen, B04-006 Wolff, J. M., B04-085 Paillard, Claude, B04-007, B04-047 Saretto, Silvano, B04-124 Tajmar, M., B04-022, B04-023 Wolff, J. Mitchell, B04-084 Pal, Sibtosh, B04-124 Sato, Tetsuya, B04-028 Tanatsugu, Nobuhiro, B04-028 Woodward, Roger, B04-124 Paoletti, Nora R., B04-117 Sawai, Shujiro, B04-028 Taskinoglu, Ezgi S., B04-070 Worgan, J. F., B04-100 Papamoschou, Dimitri, B04-026 Schauer, F., B04-111 Terabayashi, T., B04-107 Yamamoto, Y., B04-016 Papila, Nilay, B04-079 Schluter, J. U., B04-052 Thole, Karen A., B04-133 Yang, H., B04-018 Parent, Bernard, B04-027 Schoenitz, Mirko, B04-128 Thynell, Stefan T., B04-075 Yong-Seok Hwang, B04-057 Parish, John W., B04-038 Seifert, Avi, B04-065 Tipare, K. R., B04-086 Yoon, Woong-Sup, B04-004 Park, S., B04-131 Seitzman, Jerry M., B04-009 Toki, Kyoichiro, B04-080 Yu, S. C. M., B04-061 Pastor, Guillermo, B04-035 Sheikin, E. G., B04-112 Tomioka, Sadatake, B04-031 Zabarnick, Steven, B04-045 Patnaik, R. K., B04-005 Shepherd, J. E., B04-094, B04-111, Trexler, Carl A., B04-630 Zess, Gary, B04-133 Paxson, Daniel E., B04-110 B03-002 Tsang, W., B04-046 Zhang, Qiang, B04-134 Pencil, Eric J., B04-025 Sherif, S. A., B04-123 Tucker, P. Kevin, B04-079 Zhang, Tao, B04-006 Peretz, Arie, B04-008 Sheverev, V., B04-112 Turco, Maria, B04-129 Zilliac, Greg, B04-125 Petersen, Eric L., B04-074 Shimada, T., B04-107 Tu, Shun-Hsu, B04-132 Zilliac, Gregory, B04-076 Phipps, C., B04-121 Shyy, Wei, B04-079 Ungewitter, R. J., B04-068 Zwahlen, Jurg, B04-025 J. PROPULSION, VOI 20, NO. 6: 2 Chronological Index B03-002 Comment on “Analytical Model for the Impulse of B04-007 Chemical Kinetic Model for Monomethylhydrazine/ Single-Cycle Pulse Detonation Tube.”’ William H. Heiser, U.S. Ai Nitrogen Tetroxide Gas Phase Combustion and Hypergolic Force Ac« demy, and David T. Pratt, University of Washingtoi (20. Ignition. Laurent Catoir , Nabiha Chaumeix, and Claude Paillard, 1, p. 189) Technical Comment L] aboratoire nbustion t Systems Reactifs-CNRS and University of Orleans e (20. 1. p 87) Article B03-002 Erratum for “Analytical Model for the Impulse of Single-Cycle Pulse Detonation Tube.’ E. M Wintenberger, B04-008 Development of Laboratory-Scale Gel Propulsion California Institute of Technology, J. M. Austin, Un rsit oF Technology. Shai Rahimi, Dov Hasan, and Arie Peretz, RAFAEL, Illinois, M Cooper, S. Jackson, and J. | Shepherd, California Armament Development Authority, Ltd., Israel (20, 1, p. 93) Institute of Technology (20, 4, p. 765) Erratum Article B03-002 Comment on “Analytical Model for the Impulse of B04-009 Intermittent Burning of Ammonium Perchlorate- Single-Cycle Pulse Detonation Tube.” Matei | Radulescu and Hydrocarbon Binder Monomodal Matrixes, Sandwiches, and Ronald K Hanson, Stanford University (20, 5, p 956) Technical Propellants. Satyanarayanan R. Chakravarthy, Jerry M. Seitzman, Comment Edward W. Price, and Robert K. Sigman, Georgia Institute of Te chnolog 20, 1. p. 101) Article B03-002 Reply to Comment on “Analytical Model for the Impulse of Single-Cycle Pulse Detonation Tube.’ by M. I. B04-010 Ultrasonic Measurement of the Pressure-Coupled Radulescu and R. K. Hanson. E. Wintenberger, M. Cooper, F Response Function for Composite Solid Propellants. Thomas J. Pintgena,nd J. I Shepherd, Callifornia Institute of Technol (20, Hafenrichter, Jeffrey J. Murphy. and Herman Krier, University of 5, p. 957) Reply Illinois at | hamp 1 (20, 1, p. 110) Article B04-001 ideas and Methods of Turbomachinery B04-011 Novel High Nitrogen Propellant Use in Solid Fuel Aerodynamics: A Historical View. N. A. Cumpsty, Rolls-Royce Micropropulsion. A. N. Ali S. F. Son, M. A. Hiskey, and D. L. pplicc.., Great Britain; and E. M. Greitzer, Massachusetts Institute of Naud, Los A Nation Laboratory (20, 1, p. 120) Article Technology (20, 1, p. 15) Article B04-012 Unsteady Stolid Propellant Pressure Combustion B04-002 A Century of Ramjet Propulsion Technology Responses Using a Piston Burner. M.Q. Brewster and B. Saarloos, Evolution. Ronald S. Fry, Johns Hopkins University (20, 1, p. 27) Universit / Urbana—Champaign (20, 1, p. 127) Article Article B04-003 Concorde and the Future of Supersonic Transport. B04-013 Ultrasonic Properties of Propellant Ingredients. Sebastien Candel, Ecole Centrale Paris and Centre National de la Makota Kohga, National Defense Academy; Robert A. Frederick, Recherche Scientifique, France (20, 1, p. 59) Article University of Alabama in Huntsville: and Marlow D. Moser, (20, 1, p. 135) Article B04-004 Orifice Diameter Ratio Effect on the Mixing Performances for Split Triplet Injectors. Yong-Ho Cho and B04-014 Designing and Testing a Lighter, Simpler, Less- Seong-Woong Lee, Hyundai MOBIS, South Korea; and Expensive Liquid-Propellant Pump. Andrew Knight, Andrew Woong-Sup Yoon, Yonsei University, South Korea (20, 1, p. 69) Knight Space Propulsion (20, 1, p. 141) Article Article B04-015 Internal Degrees of Freedom of an Actuator Disc B04-005 Characteristics of Sprays Formed by Impingement of Model. Sergei I. Chernyshenko and Aleksei V. Privalov, University a Pair of Liquid Jets. K. Ramamurthi, K. Nandakumar, and R. K. of Southhampton, Great Britain (20, 1, p. 155) Article Patnaik, Liquid Propulsion Systems Center, India (20, 1, p. 76) Article B04-016 Approach to High-Performance Transonic Compressor Design. M. Oana, H. Ohtani, O. Kawamoto, and Y. B04-006 Propulsive Performance of Hypergolic H,0,/ Yamamoto, Honda R&D Company, Ltd., Japan (20, 1, p. 164) Kerosene Bipropellant. Tao Zhang, Chinese Academy of Sciences, Article China (PRC); Yu Cong, Tao Li, Jiwen Sun, Xiaodong Wang, and Lei Ma, Dalian Institute of Chemical Physics, China (PRC); B04-017 Three-Dimensional Time-Resolved Inlet Guide Dongbai Liang and Liwu Lin, Dalian Institute of Chemical Physics Vane—Rotor Potential Field Interaction. Robert T. Johnston and (20, 1, p. 83) Article Sanford Fleeter, Purdue University (20, 1, p. 171) Article 1144 J. PROPULSION, VOL. 20, NO. 6: 2004 INDEX B04-018 Experimental Study on Linear Compressor Cascade and Carl A. Trexler, NASA Langley Research Center (20, 2, p. 288) with Three-Dimensional Blade Oscillation. H. Yang and L. He, Article based on AIAA Paper 2003-0012 University of Durham, Great Britain (20, 1, p. 180) Article B04-030 Supersonic Flow Ignition by Plasma Torch and H,/O, B04-019 A Critical History of Electric Propulsion: The First 50 Torch. Kan Kobayashi, Sadatake Tomioka, and Tohru Mitani, Years (1906-1956). E. Y. Choueiri, Princeton University (20, 2, p. Japan Aerospace Exploration Agency, Kakuda Space Propulsion 193) Article Center, Japan (20, 2, p. 294) Article based on AIAA Paper 2001 1763 B04-020 Modeling and Analysis of a Megawatt-Class Magnetoplasmadynamic Thruster. Pavlos G. Mikellides, Arizona B04-031 High-Pressure-Turbine Clearance Control Systems: State University (20, 2, p. 204) Article Current Practices and Future Directions. Scott B. Lattime, Ohio Aerospace Institute; and Bruce M. Steinetz, NASA John H. Glenn Research Center at Lewis Field (20, 2, p. 302) Article B04-021 Indium Field Emission Electric Propulsion Microthruster Experimental Characterization. M. Tajmar, A. Genovese, and W. Steiger, ARC Seibersdorf Research, Austria (20, B04-032 High-Speed, High-Temperature Finger Seal Test 2, p. 211) Article Results. Margaret P. Proctor, NASA John H. Glenn Research Center at Lewis Field; Arun Kumar, Honeywell Engines, Systems and Services; and Irebert R. Delgado, U.S Army Reseach Laboratory B04-022 2000-Hour Endurance Test of Indium Field Emission (20, 2, p. 312) Article Electric Propulsion Microthruster Cluster. A. Genovese, M. Tajmar, N. Buldrini, and W. Steiger, ARC Seibersdorf Research, Austria (20, 2, p. 219) Article B04-033 Wavelet Analysis of Rotor-Tip Disturbances in an Axial-Flow Compressor. Feng Lin, I/ndiana Institute Technology; Jingyi Chen and Meilin Li, Chinese Academ) B04-023 Ion-Energy Diagnostics in an SPT-100 Plume from Sciences, China (PRC) (20, 2, p. 319) Article Thrust Axis to Backflow. Lyon B. King, Michigan Technological University; and Alec D. Gallimore, University of Michigan (20, 2, p. 228) Article based on AIAA Paper 98-3641 B04-034 Parametric Design of Turbomachinery Airfoils Using Highly Differentiable Splines. Roque Corral and Guillermo Pastor, Industria de Turbopropulsores S.A., Spain (20, 2, p. 335) B04-024 Pulsed Plasma Thruster Plume Investigation Using a Article Current-Mode Quadruple Probe Method. Nikolaos A. Gatsonis, Jurg Zwahlen, and Adrian Wheelock, Worcester Polytechnic Institute; Eric J. Pencil and Hani Kamhawi, NASA Glenn Research B04-035 Simulations of Normal Shock-Wave/Boundary- Center (20, 2, p. 243) Article based on AIAA Paper 2002-4123 Layer Interaction Control Using Mesoflaps. R. K. Jaiman, I Loth, and J. C. Dutton, University of Illinois (20, 2, p. 344) Article B04-025 Engine Cycle and Exhaust Configuration for Quiet Supersonic Propulsion. Dimitri Papamoschou, University of California, Irvine (20, 2, p. 255) Article B04-036 Compressible Subsonic Particle-Laden Flow over a Square Cylinder. G. B. Jacobs, University of Illinois at Chicago; D. A. Kopriva, Florida State University; and F. Mashayek, B04-026 Hypervelocity Fuel/Air Mixing in a Shcramjet Inlet. University of Illinois at Chicago (20, 2, p. 353) Article Jean P. Sislian and Bernard Parent, University of Toronto Institute for Aerospace Studies, Canada (20, 2, p. 263) Article B04-037 Methane Dissociation in Pulsed de Discharges at High B04-027 Experimental Study on Restart Control of a Reduced Electric Field. S. Douglas Marcum, Miami University: Supersonic Air-Breathing Engine. Takayuki Kojima, National John W. Parish and Biswa N. Ganguly, Air Force Research Aerospace Laboratory of Japan, Japan, Tetsuya Sato, Shujiro Laboratory (20, 2, p. 360) Article Sawai, and Nobuhiro Tanatsugu, I/nstitute of Space and Astronautical Science, Japan (20, 2, p. 273) Article B04-038 New Particle-Image-Velocimetry Method to Measure Flowfields in Luminous Spray Flames. A. K. Gupta, L. Lourenco, B04-028 Sonic Injection into a Mach 5.0 Freestream Through M. Linck, and S. Archer, University of Maryland (20, 2, p. 369) Diamond Orifices. Rodney D. W. Bowersox, Texas A&M Technical Note University, Huaiguo Fan and Daina Lee, University of Alabama (20, 2, p. 280) Article B04-039 Reaction Rates for Hypergolic Propellants Using Chemical Delay Times. Mark J. Farmer, Lynette O. Mays, Casey B04-029 Mach 4 Performance of Hypersonic Inlet with S. Hampton, and James E. Smith Jr., University of Alabama in Rectangular-to-Elliptical Shape Transition. Michael K. Smart Huntsville (20, 2, p. 372) Technical Note