Table Of Content

J. PROPULSION, VOL. 24, NO. 6: 2008 INDEX 1425 B08-054 Aerodynamics of Fan Flow Deflectors B08-084 Experimental Study of a Scramjet B08-143 Survey of Aerodynamic Drag Reduction for Jet Noise Suppression Nozzle Flow Using the Pressure-Sensitive-Paint at High Speed by Energy Deposition B08-088 Passive Control Techniques to Alleviate Method B08-144 Near-Surface Electrical Discharge in Supersonic Cavity Flow Oscillation Supersonic Airflow: Properties and Flow Control Inlet, Nozzle, Diffuser, and Channel B08-113 |H ypersonic Flow Control Using Surface Boundary Layers and Heat Transfer: Flows Plasma Actuator Laminar B08-083 Analytical Computation of Leading- B08-112| Numerical Simulation of Direct Current B08-062 Prediction of the Efficiency of Acoustic Edge Truncation Effects on Inviscid Busemann- Glow Discharges for High-Speed Flow Control Damping Cavities Inlet Performance B08-146 Repetitively Pulsed Nonequilibrium B08-030 Preliminary Study of Shock Train in a Plasmas for Magnetohydrodynamic Flow Control Boundary Layers and Heat Transfer: Curved Variable-Section Diffuser and Plasma-Assisted Combustion Turbulent B08-035 Real-Gas Effects in Organic Rankine B08-107 Wear Mechanisms in Electron Sources Cycle Turbine Nozzles for Ion Propulsion, 2: Discharge Hollow Cathode B08-049 Low-Heat-Load-Vane Profile Optimi- B08-038 Examination of a Collision-Limiter B08-106 Wear Mechanisms in Electron Sources zation, Part 2: Short-Duration Shock-Tunnel Direct Simulation Monte Carlo Method for for lon Propulsion, 1: Neutralizer Hollow Cathode Experiments Micropropulsion Applications B08-114 Single-Dielectric Barrier Discharge B08-123 Experimental Investigation of a Two- Plasma Enhanced Aerodynamics: Concepts, Boundary-Layer Stability and Transition Dimensional and a Three-Dimensional Scramjet Optimization, and Applications B08-152. Spanwise Wake and Discrete Jet Inlet at Mach 7 Disturbances on a Separating Turbine Blade B08-079 A Starting Procedure of Supersonic Rarefied Flows B08-028 Boundary-Layer Effects on Internal Ejector to Minimize Primary Pressure Load B08-121 Performance Modeling of a Coaxial Flow Choking in Dual-Thrust Solid Rocket B08-055 Investigation of Two-Dimensional Radio-Frequency Gas-Discharge Microthruster Motors Scramjet Inlet Flowfield at Mach 7 B08-038 Examination of a Collision-Limiter B08-052 Experimental Investigation of Unsteady B08-090 Computational Study on the Critical Direct Simulation Monte Carlo Method for Transition Processes on High-Lift T106A Turbine Nozzle Flow of High-Pressure Hydrogen Gas Micropropulsion Applications Blades B08-125 Limiting Contractions for Starting Simple Ramp-Type Scramjet Intakes with Over- Reacting Flows and Combustion Computational Fluid Dynamics board Spillage B08-058 Internal Flow Dynamics in a Valveless B08-035 Real-Gas Effects in Organic Rankine B08-084 Experimental Study of a Scramjet Airbreathing Pulse Detonation Engine Cycle Turbine Nozzles Nozzle Flow Using the Pressure-Sensitive-Paint B08-003 Computational Study of the Propulsive B08-038 Examination of a Collision-Limiter Method Characteristics of a Shcramjet Engine Direct Simulation Monte Carlo Method for B08-006 Concentration Distribution in Super- Micropropulsion Applications Jets, Wakes, and Viscid-Inviscid Flow sonic Flow Recirculation Region B08-115 High-Speed Magnetohydrodynamic Interactions B08-065 Outlet-Boundary-Condition Influence Flow Control Analyses with Three-Dimensional B08-032 Flush-Wall, Diamond-Shaped Fuel In- for Large Eddy Simulation of Combustion Simulations jector for High Mach Number Scramjets Instabilities in Gas Turbines B08-048 Low-Heat-Load-Vane Profile Optimi- B08-052 Experimental Investigation of Unsteady B08-146 Repetitively Pulsed Nonequilibrium zation, Part 1: Code Validation and Airfoil Transition Processes on High-Lift T106A Turbine Plasmas for Magnetohydrodynamic Flow Control Redesign Blades and Plasma-Assisted Combustion B08-001 Turbulence Models Assessment for B08-085 Complex Wall Injector Array for High- B08-099 Experimental and Numerical Investiga- Large-Scale Tip Vortices in an Axial Compressor Speed Combustors tion of n-Heptane/Air Counterflow Nonpremixed Rotor B08-152 Spanwise Wake and Discrete Jet Flame Structure B08-037 Multiple Surrogate Modeling for Axial Disturbances on a Separating Turbine Blade B08-087 Flame Characteristics in Supersonic Compressor Blade Shape Optimization B08-004 Numerical Simulation of Transverse Combustor with Hydrogen Injection Upstream B08-092. Leakage Assessment of Pressure-Ex- Injection of Circular Jets into Turbulent Super- of Cavity Flameholder change Wave Rotors sonic Streams Separated Flows B08-065 Outlet-Boundary-Condition — Influence Multiphase Flows B08-114 Single-Dielectric Barrier Discharge for Large Eddy Simulation of Combustion Instabilities in Gas Turbines B08-118 Molecular Dynamics Simulation of Ion Plasma Enhanced Aerodynamics: Concepts, Emission from Nanodroplets of Ionic Liquids Optimization, and Applications B08-134 Flow Study of a Redesigned High- B08-156 Simulation of Icing on a Cascade of B08-004 Numerical Simulation of Transverse Pressure-Ratio Centrifugal Compressor Stator Blades Injection of Circular Jets into Turbulent Super- B08-136 Detached-Eddy Simulation of a Louver- B08-161 Inert Particles for Axial-Combustion- sonic Streams Cooling Scheme for Turbine Blades Instability Suppression in a Solid Rocket Motor B08-131 Multiple Objective Optimization and B08-086 Effect of Liquid Injection on Acoustic Shock Waves and Detonations Inverse Design of Axial Turbomachinery Blades Field Induced from Supersonic Flow Past Cavities B08-103 Ablative Impulse Characteristics of B08-153 Detached-Eddy Simulation Procedure B08-031 Breakup of Aerated Liquid Jets in Polyacetal with Repetitive CO, Laser Pulses Targeted for Design Subsonic Crossflow B08-058 Internal Flow Dynamics in a Valveless Airbreathing Pulse Detonation Engine Hypersonic Flow Plasmadynamics and MHD B08-041 Multicyclic-Detonation-Initiation Stud- B08-123_ Experimental Investigation of a Two- B08-115 High-Speed Magnetohydrodynamic ies in Valveless Pulsed Detonation Combustors Dimensional and a Three-Dimensional Scramjet Flow Control Analyses with Three-Dimensional Inlet at Mach 7 Simulations Subsonic Flow B08-083 Analytical Computation of Leading- B08-039 Time-Resolved Measurements of Im- B08-139 Ducted Wind/Water Turbines and Edge Truncation Effects on Inviscid Busemann- pulse Generation in Pulsed Laser-Ablative Propellers Revisited Inlet Performance Propulsion B08-111 Virtual Shapes in Supersonic Flow B08-111 Virtual Shapes in Supersonic Flow Supersonic Flow Control with Energy Addition Control with Energy Addition B08-088 Passive Control Techniques to Alleviate B08-113 |H ypersonic Flow Control Using Surface B08-116 Microwave Discharges and Possible Supersonic Cavity Flow Oscillation Plasma Actuator Applications in Aerospace Technologies B08-087 Flame Characteristics in Supersonic B08-003 Computational Study of the Propulsive B08-145 Nanosecond-Pulsed Discharges _ for Combustor with Hydrogen Injection Upstream Characteristics of a Shcramjet Engine Plasma-Assisted Combustion and Aerodynamics of Cavity Flameholder 1426 J. PROPULSION, VOL. 24, NO. 6: 2008 INDEX B08-112 Numerical Simulation of Direct Current INTERDISCIPLINARY TOPICS PROPULSION Glow Discharges for High-Speed Flow Control B08-079 A Starting Procedure of Supersonic Aerospace Technology Utilization Advanced Space Propulsion Ejector to Minimize Primary Pressure Load B08-164 Geosynchronous-Earth-Orbit Commu- B08-118 Molecular Dynamics Simulation of Ion nication Satellite Deliveries with Integrated Emission from Nanodroplets of Ionic Liquids Transonic Flow Electric Propulsion B08-036 Strongly Swirling Turbulent Sink Flow B08-091 Unsteady Strong Shock Interactions in a B08-077 Implications of Day Temperature for a Between Two Stationary Disks Transonic Turbine: Experimental and Numerical High-Pressure-Turbine Blade’s Low-Cycle-Fa- B08-138 Moderate-Acceleration Launch Using Analysis tigue Life Consumption Repetitive-Pulse Laser Ablation in a Tube B08-117. Measurement of 30-Centimeter Ion Unsteady Flows Analytical and Numerical Methods Thruster Discharge Cathode Erosion B08-133 Desensitization of the Flowfield from B08-046 Investigation of Active Flow Control on B08-163 Dormant Cathode Erosion in a Multiple- Rotor Tip-Gap Height by Casing-Air Injection Diesel Engine Aftertreatment Cathode Gridded Ion Thruster B08-052 Experimental Investigation of Unsteady B08-022 Use of Condensed-Phase Reaction B08-061 Testing and Characterization of a Transition Processes on High-Lift T106A Turbine Models in Combustion Simulation of Energetic Hydrogen Peroxide Monopropellant Thruster Blades Materials B08-019 Silanes/H,O,: A High-Performance B08-021 Multidimensional Numerical Simula- Synthetic Bipropellant for Chemical Space Lasers and Laser Applications tion of Ammonium-Perchlorate-Based Propellant Propulsion Combustion with Fine/Ultrafine Aluminum B08-146 Repetitively Pulsed Nonequilibrium B08-047 Metal-CO, Propulsion for Mars Mis- B08-002 Effects of Tip Clearance on Aerody- Plasmas for Magnetohydrodynamic Flow Control sions: Current Status and Opportunities namic Damping in a Linear Turbine Cascade and Plasma-Assisted Combustion B08-120 Numerical Analyses of Exhaust and B08-027 Analysis of Injecting Wall Inclination on Multidisciplinary Design Optimization Refill Processes of a Laser Pulse Jet Segmented Solid Rocket Motor Instability B08-165 Thrust Stand Micromass Balance for the B08-037 Multiple Surrogate Modeling for Axial B08-092 Leakage Assessment of Pressure-Ex- Direct Measurement of Specific Impulse Compressor Blade Shape Optimization change Wave Rotors B08-162 Laser-Assisted Combustion of Solid B08-059 Optimal Design of Hybrid Rocket B08-065 Outlet-Boundary-Condition — Influence Propellants at Low Pressures Motors for Microgravity Platform for Large Eddy Simulation of Combustion B08-105 Role of Superconducting Shields in B08-094 Exploring the Effects of Removing Instabilities in Gas Turbines Electrodynamic Propulsion Process-Intrinsic Constraints on Gas Turbine B08-169 Exact Navier-Stokes Solution for the B08-017 Charged Nanoparticle Source for High Design Pulsatory Viscous Channel Flow with Arbitrary Thrust Level Colloid Thruster Pressure Gradient Airbreathing Propulsion B08-153 Detached-Eddy Simulation Procedure LAUNCH VEHICLE AND Targeted for Design MISSILE (LV/M) TECHNOLOGY B08-083 Analytical Computation of Leading- B08-091 Unsteady Strong Shock Interactions in a Edge Truncation Effects on Inviscid Busemann- Transonic Turbine: Experimental and Numerical Aerodynamics Inlet Performance Analysis B08-051 Loss Mechanisms of High-Turning B08-929 Experimental Study of Chin Intakes for B08-136 Detached-Eddy Simulation of aL ouver- Airbreathing Missiles with High Agility Supercritical Compressor Cascades Cooling Scheme for Turbine Blades B08-082 Plasma-Assisted Ignition in Scramjets B08-158 Study on the Operation of Pulse- Configuration Design B08-089 Extraction of One-Dimensional Flow Detonation Engine-Driven Ejectors B08-028 Boundary-Layer Effects on Internal Properties from Multidimensional Data Sets B08-157 Performance Studies of Pulse Detona- Flow Choking in Dual-Thrust Solid Rocket B08-030 Preliminary Study of Shock Train in a tion Engine Ejectors Motors Curved Variable-Section Diffuser B08-041 Multicyclic-Detonation-Initiation Stud- B08-138 Moderate-Acceleration Launch Using Viscous Non-Boundary-Layer Flows Repetitive-Pulse Laser Ablation in a Tube ies in Valveless Pulsed Detonation Combustors B08-033 Dual-Mode Combustion Experiments B08-011 Microgravity Geyser and Flowfield Prediction Launch Vehicle and Sounding Rocket with an Integrated Aeroramp-Injector/Plasma- Systems Torch Igniter B08-031 Breakup of Aerated Liquid Jets in Vortices B08-059 Optimal Design of Hybrid Rocket Subsonic Crossflow B08-133 Desensitization of the Flowfield from Motors for Microgravity Platform B08-008 Single-Cycle Impulse from Detonation Rotor Tip-Gap Height by Casing-Air Injection Propulsion and Propellant Systems Tubes with Nozzles B08-027 Analyofs Injiecstin g Wall Inclination on Segmented Solid Rocket Motor Instability B08-026 Laboratory-Scale Thermal Stability Ex- B08-135 Characterization ofa Prefilming Airblast B08-001 Turbulence Models Assessment for periments on RP-1 and RP-2 Atomizer in a Strong Swirl Flowfield Large-Scale Tip Vortices in an Axial Compressor B08-160 Opportunities for a Liquid Rocket Feed B08-139 Ducted Wind/Water Turbines and Rotor System Based on Electric Pumps Propellers Revisited B08-036 Strongly Swirling Turbulent Sink Flow B08-102 Chemical Erosion of Carbon-Carbon/ B08-032 Flush-Wall, Diamond-Shaped Fuel In- Between Two Stationary Disks Graphite Nozzles in Solid-Propellant Rocket jector for High Mach Number Scramjets Motors B08-084 Experimental Study of a Scramjet Wave Motion and Sloshing B08-015 Testing a Helicon Double Layer Nozzle Flow Using the Pressure-Sensitive-Paint Thruster Immersed in a Space-Simulation Method B08-169 Exact Navier-Stokes Solution for the Chamber B08-120 Numerical Analyses of Exhaust and Pulsatory Viscous Channel Flow with Arbitrary B08-029 Experimental Study of Chin Intakes for Refill Processes of a Laser Pulse Jet Pressure Gradient Airbreathing Missiles with High Agility B08-095 Adaptive Estimation Algorithm for Aircraft Engine Performance Monitoring Simulation B08-056 Experimental Studies of Pylon-Aided GUIDANCE, CONTROL, AND B08-042 Wave Reverberations in Multitube Pulse Fuel Injection into a Supersonic Crossflow DYNAMICS TECHNOLOGY Detonation Engines B08-098 Hydrocarbon Fuel Flash Vaporization for Pulsed Detonation Combustion Engine Control Testing, Flight and Ground B08-057 Matched Pressure Injections into a B08-124 Shock Train Leading-Edge Detection in B08-029 Experimental Study of Chin Intakes for Supersonic Crossflow Through Diamond-Shaped a Dual-Mode Scramjet Airbreathing Missiles with High Agility Orifices J. PROPULSION, VOL. 24, NO. 6: 2008 INDEX 1427 B08-150 Investigation of Supersonic Combustion B08-022 Use of Condensed-Phase Reaction B08-110 Inexpensive Optically Isolated Nano- with Angled Injection in a Cavity-Based Models in Combustion Simulation of Energetic ammeter for Use with Micro-Newton Electric Combustor Materials Propulsion Technology B08-168 Combustion of Decane-Based Slurries B08-062 Prediction of the Efficiency of Acoustic B08-117 Measurement of 30-Centimeter Ion with Metallic Fuel Additives Damping Cavities Thruster Discharge Cathode Erosion B08-034 Liquid-Fueled Strut-Based Scramjet B08-167 Dynamics of Laminar Premixed Flames B08-069 Relationship Between Anode Spots and Combustor Design: A Computational Fluid Forced by Harmonic Velocity Disturbances Onset Voltage Hash in Magnetoplasmadynamic Dynamics Approach B08-018 Magnetic Flowmeter Burner Measure- Thrusters B08-158 Study on the Operation of Pulse- ment of a Solid Propellant Pressure-Coupled B08-012 Plume Expansion and Ionization in a Detonation Engine-Driven Ejectors Imaginary Response Microlaser Plasma Thruster B08-157 Performance Studies of Pulse Detona- B08-064 Laboratory Scale Survey of Pentad B08-015 Testing a Helicon Double Layer tion Engine Ejectors Injector Stability Characteristics Thruster Immersed in a_ Space-Simulation B08-085 Complex Wall Injector Array for High- B08-109 Observation of Unsteady Cryogenic Chamber Speed Combustors Flows from a Characteristic Coaxial Rocket B08-016 Bismuth Hollow Cathode for Hall Injector Thrusters Combined-Cycle Engines B08-060 Burning Rate Characteristics of Ammo- B08-040 Testing of a 250-Kilowatt Fault- B08-151 Contrarotating Turbine Aerodesign for nium Perchlorate-Based Composite Propellant Tolerant Permanent Magnet Power Generation an Advanced Hypersonic Propulsion System Using Bimodal Ammonium Perchlorate System for Large Civil Aeroengines B08-063 Resonance Frequencies and Damping of B08-081 Corruption of Pulsed Electric Thruster a Combustor Acoustically Coupled to an Voltage Fluctuation Measurements by Trans- Combustion and Combustor Designs Absorber mission Line Resonances B08-147 Characteristics of Gliding Arc and its B08-078 Nonlinear Interactions Between Forced B08-068 Numerical and Experimental Investiga- Application in Combustion Enhancement and _ Self-Excited Acoustic Oscillations in tions of Crossover Ion Impingement for Subscale B08-100 Ignition of Iron-Coated and Nickel- Premixed Combustor Ion Optics Coated Aluminum Particles Under Normal- and B08-096 Combustion Instability Problems Anal- B08-163 |D ormant Cathode Erosion in a Multiple- Reduced-Gravity Conditions ysis for High-Pressure Jet Engine Cores Cathode Gridded Ion Thruster B08-097 Computational Methodology for Car- B08-127 Analytical Solution — for Pressure- B08-013 Magnetic Sensing of Azimuthal Current bon Monoxide Emission for Aeroengine Com- Coupled Combustion Response Functions of in Hall Thrusters: In-Flight Diagnostic Potential bustor Design Composite Solid Propellants B08-105 Role of Superconducting Shields in B08-129 Chemi-lon-Current-Induced Dissocia- B08-166 Characterization of an Acoustically Electrodynamic Propulsion tive Recombination in Premixed Hydrocarbon/ Self-Excited Combustor for Spray Evaporation B08-017 Charged Nanoparticle Source for High Air Flames B08-161 Inert Particles for Axial-Combustion- Thrust Level Colloid Thruster B08-062 Prediction of the Efficiency of Acoustic Instability Suppression in a Solid Rocket Motor B08-014 Near Exit Plane Velocity Field of a 200- Damping Cavities Watt Hall Thruster B08-082 Plasma-Assisted Ignition in Scramjets Detonation B08-121 Performance Modeling of a Coaxial B08-033 Dual-Mode Combustion Experiments B98-008 Single-Cycle Impulse from Detonation Radio-Frequency Gas-Discharge Microthruster with an Integrated Aeroramp-Injector/Plasma- Tubes with Nozzles B08-137 Electromagnetic Flow Sensor for Liquid Torch Igniter B08-009 Effect of High-Voltage Pulsed Dis- Metal-Fed Electric Propulsion B08-063 Resonance Frequencies and Damping of charges on Deflagration to Detonation Transition B08-164 Geosynchronous-Earth-Orbit Commu- a Combustor Acoustically Coupled to an B08-041 Multicyclic-Detonation-Initiation Stud- nication Satellite Deliveries with Integrated Absorber ies in Valveless Pulsed Detonation Combustors Electric Propulsion B08-023, Combustion of Boron-Titanium Nano- B08-158 Study on the Operation of Pulse- B08-108 [on-Collision Emission Excitation Cross composite Powders in Different Environments Detonation Engine-Driven Ejectors Sections for Xenon Electric Thruster Plasmas B08-096 Combustion Instability Problems Anal- B08-157 Performance Studies of Pulse Detona- B08-107 Wear Mechanisms in Electron Sources ysis for High-Pressure Jet Engine Cores tion Engine Ejectors for lon Propulsion, 2: Discharge Hollow Cathode B08-045 Sight-Premixing Effects on Oxidation/ B08-098 Hydrocarbon Fuel Flash Vaporization B08-106 Wear Mechanisms in Electron Sources Formation of Polycyclic Aromatic Hydrocarbon for Pulsed Detonation Combustion for lon Propulsion, 1: Neutralizer Hollow Cathode in Counterflow Flames Droplet and Spray Characterization B08-060 Burning Rate Characteristics of Ammo- B08-159 Spray Characteristics of Recessed Gas- Emissions and Noises nium Perchlorate-Based Composite Propellant Using Bimodal Ammonium Perchlorate Liquid Coaxial Swirl Injector B08-045 Sight-Premixing Effects on Oxidation/ B08-056 Experimental Studies of Pylon-Aided B08-031 Breakup of Aerated Liquid Jets in Formation of Polycyclic Aromatic Hydrocarbon Fuel Injection into a Supersonic Crossflow Subsonic Crossflow in Counterflow Flames B08-047 Metal-CO, Propulsion for Mars Mis- B08-110 Inexpensive Optically Isolated Nano- B08-072 Microphysical Modeling of Ground- sions: Current Status and Opportunities ammeter for Use with Micro-Newton Electric Level Aircraft-Emitted Aerosol Formation: Roles B08-078 Nonlinear Interactions Between Forced Propulsion Technology of Sulfur-Containing Species and = Self-Excited Acoustic Oscillations in B08-168 Combustion of Decane-Based Slurries B08-097 Computational Methodology for Car- Premixed Combustor with Metallic Fuel Additives bon Monoxide Emission for Aeroengine Com- B08-162 Laser-Assisted Combustion of Solid B08-007 Studies on Spray Behavior of a Pressure bustor Design Propellants at Low Pressures Swirl Atomizer in Transition Regime B08-078 Nonlinear Interactions Between Forced B08-099 Experimental and Numerical Investiga- B08-135 Characterization ofa Prefilming Airblast and Self-Excited Acoustic Oscillations in tion of n-Heptane/Air Counterflow Nonpremixed Atomizer in a Strong Swirl Flowfield Premixed Combustor Flame Structure Electric Propulsion B08-096 Combustion Instability Problems Anal- B08-130 Elevated Pressure Thermal Experiments ysis for High-Pressure Jet Engine Cores B08-119 Hybrid Particle-in-Cell Erosion Model- and Modeling Studies on the Water-Gas Shift B08-046 Investigation of Active Flow Control on ing of Two Hall Thrusters Reaction B08-104 Electron Dynamics After Exit Plane of Diesel Engine Aftertreatment Stationary Plasma Thruster Discharge Chamber Combustion Instability B08-118 Molecular Dynamics Simulation of lon Engine Control Integration and Health B08-129 Chemi-lon-Current-Induced Dissocia- Emission from Nanodroplets of lonic Liquids Monitoring tive Recombination in Premixed Hydrocarbon/ B08-067 Particle Simulation of Plume Flows B08-095 Adaptive Estimation Algorithm for Air Flames from an Anode-Layer Hall Thruster Aircraft Engine Performance Monitoring 1428 J. PROPULSION, VOL. 24, NO. 6: 2008 INDEX B08-013 Magnetic Sensing of Azimuthal Current Gas Turbine Engines B08-165 Thrust Stand Micromass Balance for the in Hall Thrusters: In-Flight Diagnostic Potential B08-093 Increasing Gas Turbine Blade Damping Direct Measurement of Specific Impulse Through Cavities Filled with Viscoelastic Liquid Rocket Engines Engine Cooling and Heat Transfer Materials B08-053 Rotordynamic Analysis of a Turbopump B08-048 Low-Heat-Load-Vane Profile Optimi- B08-054 Aerodynamics of Fan Flow Deflectors with the Casing Structural Flexibility zation, Part 1: Code Validation and Airfoil for Jet Noise Suppression B08-160 Opportunities for a Liquid Rocket Feed Redesign B08-094 Exploring the Effects of Removing System Based on Electric Pumps B08-055 Investigation of Two-Dimensional Process-Intrinsic Constraints on Gas Turbine B08-010 Study of Heat Transfer Correlations for Scramjet Inlet Flowfield at Mach 7 Design Supercritical Hydrogen in Regenerative Cooling B08-050 Experimental Evaluation of a Turbine B08-135 Characterization ofa Prefilming Airblast Channels Blade with Potassium Evaporative Cooling Atomizer in a Strong Swirl Flowfield B08-064 Laboratory Scale Survey of Pentad B08-136 Detached-Eddy Simulation of aL ouver- B08-049 Low-Heat-Load-Vane Profile Optimi- Injector Stability Characteristics Cooling Scheme for Turbine Blades zation, Part 2: Short-Duration Shock-Tunnel B08-061 Testing and Characterization of a B08-010 Study of Heat Transfer Correlations for Experiments Hydrogen Peroxide Monopropellant Thruster Supercritical Hydrogen in Regenerative Cooling B08-092 Leakage Assessment of Pressure-Ex- B08-109 Observation of Unsteady Cryogenic Channels change Wave Rotors Flows from a Characteristic Coaxial Rocket B08-075 Infrared Signature Suppression of B08-077 Implications of Day Temperature for a Injector Helicopter Engine Duct Based on “Conceal and High-Pressure-Turbine Blade’s Low-Cycle-Fa- B08-154 Tip*Clearance Effect on the Performance Camouflage” tigue Life Consumption of a Shrouded Supersonic Impulse Turbine Hybrid Rocket Engines B08-159 Spray Characteristics of Recessed Gas- Engine Performance Liquid Coaxial Swirl Injector B08-059 Optimal Design of Hybrid Rocket B08-089 Extraction of One-Dimensional Flow Motors for Microgravity Platform Micro Propulsion and Power Properties from Multidimensional Data Sets B08-008 Single-Cycle Impulse from Detonation Hypersonic Propulsion B08-110 Inexpensive Optically Isolated Nano- Tubes with Nozzles ammeter for Use with Micro-Newton Electric B08-126 Experimental Study of a Dual-Mode B08-046 Investigation of Active Flow Control on Propulsion Technology Scramjet Isolator Diesel Engine Aftertreatment B08-012 Plume Expansion and Ionization in a B08-124 Shock Train Leading-Edge Detection in B08-058 Internal Flow Dynamics in a Valveless Microlaser Plasma Thruster a Dual-Mode Scramjet Airbreathing Pulse Detonation Engine B08-066 Ultrasonic Propulsion B08-032 Flush-Wall, Diamond-Shaped Fuel In- B08-007 Studies on Spray Behavior of a Pressure B08-165 Thrust Stand Micromass Balance for the jector for High Mach Number Scramjets Swirl Atomizer in Transition Regime Direct Measurement of Specific Impulse B08-005 Additives to Improve Fuel Heat Sink B08-121 Performance Modeling of a Coaxial Capacity in Air/Fuel Heat Exchangers Radio-Frequency Gas-Discharge Microthruster Engine Power Cycles B08-055 Investigation of Two-Dimensional B08-017 Charged Nanoparticle Source for High B08-160 Opportunities for a Liquid Rocket Feed Scramjet Inlet Flowfield at Mach 7 Thrust Level Colloid Thruster System Based on Electric Pumps B08-034 Liquid-Fueled Strut-Based Scramjet Combustor Design: A Computational Fluid Microwaves Fuel Cells Dynamics Approach B08-116 Microwave Discharges and Possible B08-090 Computational Study on the Critical B08-086 Effect of Liquid Injection on Acoustic Applications in Aerospace Technologies Field Induced from Supersonic Flow Past Cavities Nozzle Flow of High-Pressure Hydrogen Gas B08-123 Experimental Investigation of a Two- Nuclear Propulsion and Power Dimensional and a Three-Dimensional Scramjet B08-074 Carbon-Carbon Recuperators in Closed- Fuels and Propellants, Properties of Inlet at Mach 7 Brayton-Cycle Space Power Systems B08-023 Combustion of Boron-Titanium Nano- B08-125 Limiting Contractions for Starting composite Powders in Different Environments Simple Ramp-Type Scramjet Intakes with Over- Ramjets and Scramjets B08-026 Laboratory-Scale Thermal Stability Ex- board Spillage B08-089 Extraction of One-Dimensional Flow periments on RP-| and RP-2 B08-003 Computational Study of the Propulsive Properties from Multidimensional Data Sets B08-100 Ignition of Iron-Coated and Nickel- Characteristics of a Shcramjet Engine B08-126 Experimental Study of a Dual-Mode Coated Aluminum Particles Under Normal- and B08-006 Concentration Distribution in Super- Scramjet Isolator Reduced-Gravity Conditions sonic Flow Recirculation Region B08-124 Shock Train Leading-Edge Detection in B08-019 Silanes/H,O,: A High-Performance a Dual-Mode Scramjet Synthetic Bipropellant for Chemical Space Ignition B08-086 Effect of Liquid Injection on Acoustic Propulsion B08-082 Plasma-Assisted Ignition in Scramjets Field Induced from Supersonic Flow Past Cavities B08-024 Aluminum-Rich Al-MoO, Nanocom- B08-147 Characteristics of Gliding Arc and its B08-057 Matched Pressure Injections into a posite Powders Prepared by Arrested Reactive Application in Combustion Enhancement Supersonic Crossflow Through Diamond-Shaped Milling B08-145 Nanosecond-Pulsed Discharges _ for Orifices B08-128 Combustion Mechanism of Ammo- Plasma-Assisted Combustion and Aerodynamics B08-033 Dual-Mode Combustion Experiments nium-Nitrate-Based Propellants B08-025 Heating and Ignition of Metallic with an Integrated Aeroramp-Injector/Plasma- B08-060 Burning Rate Characteristics of Ammo- Particles by a CO, Laser Torch Igniter nium Perchlorate-Based Composite Propellant B08-109 Observation of Unsteady Cryogenic B08-005 Additives to Improve Fuel Heat Sink Using Bimodal Ammonium Perchlorate Flows from a Characteristic Coaxial Rocket Capacity in Air/Fuel Heat Exchangers B08-018 Magnetic Flowmeter Burner Measure- Injector B08-150 Investigation of Supersonic Combustion ment of a Solid Propellant Pressure-Coupled with Angled Injection in a Cavity-Based Imaginary Response Laser Integration/Systems Combustor B08-099 Experimental and Numerical Investiga- B08-039 Time-Resolved Measurements of Im- B08-004 Numerical Simulation of Transverse tion of n-Heptane/Air Counterflow Nonpremixed pulse Generation in Pulsed Laser-Ablative Injection of Circular Jets into Turbuient Super- Flame Structure Propulsion sonic Streams B08-168 Combustion of Decane-Based Slurries B08-138 Moderate-Acceleration Launch Using B08-056 Experimental Studies of Pylon-Aided with Metallic Fuel Additives Repetitive-Pulse Laser Ablation in a Tube Fuel Injection into a Supersonic Crossflow B08-047. Metal-CO, Propulsion for Mars Mis- B08-103 Ablative Impulse Characteristics of B08-085 Complex Wall Injector Array for High- sions: Current Status and Opportunities Polyacetal with Repetitive CO, Laser Pulses Speed Combustors J. PROPULSION, VOL. 24, NO. 6: 2008 INDEX 1429 B08-149 Radical-Farm Ignition Processes in B08-001 Turbulence Models Assessment for THERMOPHYSICS AND HEAT Two-Dimensional Supersonic Combustion Large-Scale Tip Vortices in an Axial Compressor TRANSFER B08-125 Limiting Contractions for Starting Rotor Simple Ramp-Type Scramjet Intakes with Over- B08-037 Multiple Surrogate Modeling for Axial Ablation, Pyrolysis, Thermal board Spillage Compressor Blade Shape Optimization B08-002 Effects of Tip Clearance on Aerody- Decomposition and Degradation Rotating Machinery namic Damping in a Linear Turbine Cascade B08-102 Chemical Erosion of Carbon-Carbon/ B08-132 Parametric Study of Injection Angle B08-053 Rotordynamic Analofy a sTuribospum p Graphite Nozzles in Solid-Propellant Rocket Effects on Stability Enhancement of Transonic with the Casing Structural Flexibility Motors Axial Compressors B08-134 Flow Study of a Redesigned High- B08-101 Effects of Propellant Gases on Thermal Solid Rocket Motors Pressure-Ratio Centrifugal Compressor Response of Solid Rocket Nozzle Liners B08-154 Tip Clearance Effect on the Performance B08-026 Laboratory-Scale Thermal Stability Ex- B08-020 Microstructure of Composite Propel- of a Shrouded Supersonic Impulse Turbine periments on RP-1 and RP-2 lants Using Simulated Packings and X-Ray B08-153 Detached-Eddy Simulation Procedure Tomography Targeted for Design Aerothermodynamics/Thermal Protection B08-100 Ignition of Iron-Coated and Nickel- B08-151 Contrarotating Turbine Aerodesign for B08-049 Low-Heat-Load-Vane Profile Optimi- Coated Aluminum Particles Under Normal- and an Advanced Hypersonic Propulsion System zation, Part 2: Short-Duration Shock-Tunnel Reduced-Gravity Conditions B08-152. Spanwise Wake and Discrete Jet Experiments B08-018 Magnetic Flowmeter Burner Measure- Disturbances on a Separating Turbine Blade ment of a Solid Propellant Pressure-Coupled B08-131 Multiple Objective Optimization and Boiling/Condensation Imaginary Response Inverse Design of Axial Turbomachinery Blades B08-050 Experimental Evaluation of a Turbine B08-028 Boundary-Layer Effects on Internal B08-091 Unsteady Strong Shock Interactions in a Blade with Potassium Evaporative Cooling Flow Choking in Dual-Thrust Solid Rocket Transonic Turbine: Experimental and Numerical Motors Analysis Computational Heat Transfer B08-021 Multidimensional Numerical Simula- tion of Ammonium-Perchlorate-Based Propellant B08-155 Flow Structure of Short-Length-Scale B08-048 Low-Heat-Load-Vane Profile Optimi- Combustion with Fine/Ultrafine Aluminum Disturbance in an Axial-Flow Compressor zation, Part 1: Code Validation and Airfoil B08-161 Inert Particles for Axial-Combustion- Redesign Instability Suppression in a Solid Rocket Motor SPACE TECHNOLOGY B08-025 Heating and Ignition of Metallic B08-027 Analysis of Injecting Wall Inclination on Space Processing Particles by a CO, Laser Segmented Solid Rocket Motor Instability B08-070 Compact Reverse Water-Gas-Shift Re- Forced Convection B08-101 Effects of Propellant Gases on Thermal actor for Extraterrestrial In Situ. Resource Response of Solid Rocket Nozzle Liners B08-010 Study of Heat Transfer Correlations for Utilization B08-162 Laser-Assisted Combustion of Solid Supercritical Hydrogen in Regenerative Cooling B08-011 Microgravity Geyser and Flowfield Propellants at Low Pressures Channels Prediction B08-102, Chemical Erosion of Carbon-Carbon/ B08-074 Carbon-Carbon Recuperators in Closed- Graphite Nozzles in Solid-Propellant Rocket Space Systems Brayton-Cycle Space Power Systems Motors B08-015 Testing a Helicon Double Layer Laser Interaction B08-127 Analytical Solution for Pressure- Thruster Immersed in a Space-Simulation Coupled Combustion Response Functions of Chamber B08-025 Heating and Ignition of Metallic Composite Solid Propellants B08-105 Role of Superconducting Shields in Particles by a CO, Laser Electrodynamic Propulsion B08-039 Time-Resolved Measurements of Im- Supersonic Combustion pulse Generation in Pulsed Laser-Ablative B08-034 Liquid-Fueled Strut-Based Scramjet Spacecraft Power Propulsion Combustor Design: A Computational Fluid B08-122 Solar Cell Modeling and Parameter Dynamics Approach Optimization Using Simulated Annealing Nonintrusive Diagnostics B08-080 Performance of Aft-Ramp Cavities for B08-074 Carbon-Carbon Recuperators in Closed- B08-108 Ton-Collision Emission Excitation Cross Flame Stabilization in Supersonic Flows Brayton-Cycle Space Power Systems Sections for Xenon Electric Thruster Plasmas B08-126 Experimental Study of a Dual-Mode Spacecraft Propulsion System Integration Scramjet Isolator Radiation in Participating Media B08-149 Radical-Farm Ignition Processes in B08-164 Geosynchronous-Earth-Orbit Commu- B08-021 Multidimensional Numerical Simula- Two-Dimensional Supersonic Combustion nication Satellite Deliveries with Integrated tion of Ammonium-Perchlorate-Based Propellant B08-150 Investigation of Supersonic Combustion Electric Propulsion Combustion with Fine/Ultrafine Aluminum with Angled Injection in a Cavity-Based STRUCTURAL MECHANICS Combustor Thermochemistry and Chemical Kinetics B08-006 Concentration Distribution in Super- AND MATERIALS B08-024 Aluminum-Rich Al-MoO, Nanocom- sonic Flow Recirculation Region Aeroelasticity and Control posite Powders Prepared by Arrested Reactive Thermoelectric Power B08-002 Effects of Tip Clearance on Aerody- Milling B08-043 Thermoelectric Properties of -Zn,Sb, namic Damping in a Linear Turbine Cascade B08-022 Use of Condensed-Phase Reaction Synthesized by Mechanical Alloying and Pulse Models in Combustion Simulation of Energetic Discharge Sintering Structural Durability (Including Fatigue, Materials B08-044 Thermoelectric Properties of Iron-and Fracture, and Environmental B08-129 Chemi-Ion-Current-Induced Dissocia- Lanthanum-Doped CoSb3 Compounds by Pulse Degradation) tive Recombination in Premixed Hydrocarbon/ Discharge Sintering B08-093 Increasing Gas Turbine Blade Damping Air Flames Through Cavities Filled with Viscoelastic B08-149 Radical-Farm Ignition Processes in Turbomachinery Materials Two-Dimensional Supersonic Combustion B08-051 Loss Mechanisms of High-Turning B08-128 Combustion Mechanism of Ammo- Supercritical Compressor Cascades Structural Dynamics and nium-Nitrate-Based Propellants B08-132 Parametric Study of Injection Angle Characterization B08-045 Sight-Premixing Effects on Oxidation/ Effects on Stability Enhancement of Transonic B08-053 Rotordynamic Analysis of a Turbopump Formation of Polycyclic Aromatic Hydrocarbon Axial Compressors with the Casing Structural Flexibility in Counterflow Flames J. PROPULSION, VOL. 24, NO. 6: 2008 INDEX Author Index Abhari, Reza S., B08-133 Chen, Jingyi, BO8-155 Glaser, Aaron J., B08-158 Jeon, Seong Min, B08-053 Adamovich, Igor V., B08-146 Cheng, Shannon, B08-119 Goebel, Dan M., B08-107 Jeong, Eunhwan, B08-154 Aggarwal, Suresh K., B08-099 Cheuret, Francois, B08-063 Goel, Tushar, B08-037 Jeong, Eunju, B08-150 Akbari, Pezhman, B08-092 Chiu, Yu-Hui, B08-108 Goyne, Christopher P., B08-033, Jeung, In-Seuck, B08-150 Alexander, Derrick C., B08-003 Choi, Jeong-Yeol, B08-058 B08-124, BO8-126 Jewell, G. W., B08-040 Alexander, Matthew S., B08-110 Choi, Yongjun, B08-067 Granata, Silvia, B08-099 Johnson, Jamie J., B08-048, Alexeenko, Alina, B08-121 Choueiri, Edgar Y., B08-069, Greatrix, David R., B08-161 B08-049 Ali, M. C. Mohamed, B08-080 B08-081 Grossman, Peter M., B08-032 Johnson, Paul K., B08-074, Allgood, Daniel, B08-157 Clark, John P., B08-048, B08-049 Gruber, Mark R., B08-056 B08-074E Allison, Eric M., B08-066 Clarkson, P John, B08-094 Guardone, Alberto, B08-035 Ju, Yiguang, B08-147 Andrzejak, Timothy A., B08-100 Cohen, Norman S., B08-127 Guelman, Moshe, B08-013 Kafafy, Raed, B08-068 Anikin, Nikolai B., B08-145 Colonna, Piero, B08-035 Giilhan, Ali, B08-029, Bd8-055, Kakami, Akira, B08-162 Anju, Kohei, B08-039 Colville, Jesse R., B08-083 B08-084, BO8-123 Kalfas, Anestis I., B08-133 Aplin, Karen L., BO8-110 Cooper, Marcia A., B08-008 Gupta, Ashwani K., B08-109 Kang, Minsung, B08-088 Arai, Masataka, B08-073 Corke, Thomas C., B08-114 Gutmark, Ephraim, B08-157, Kapulkin, Alexander, B08-013 Arakawa, Yoshihiro, B08-120 Coton, Thomas, B08-091 B08-158 Kasahara, Jiro, BO7-127R Arima, Toshiyuki, B08-051 Culbertson, Brad, B08-1306 Gutsol, Alexander, B08-147 Kato, Hiromasa, B08-151 Asif, Samina, B08-122 Culick, Fred E. C., B08-127 Hiberle, Jiirgen, B08-055, BO8-123 Katsurayama, Hiroshi, B08-120 Balachandran, R., BO8-166 Cullen, J. J. A., BO8-040 Habiballah, Mohammed, B08-062 Katz, Ira, BO8-106, BO8-107 Barnett, Jack, B08-082 d’ Agostino, Luca, B08-061 Haftka, Raphael T., B08-037 Kawakami, T., B08-028 Barrett, Michael J., B08-074, Daily, John W., BO8-118 Hansel, Jason, B08-093 Keidar, Michael, B08-067 B08-074E Dankanich, John W., B08-164 Hargus, William A., B08-012, Kent, Barry J., BO8-110 Baurle, Robert A., B08-082, Dannenhoffer, III, John F., BO8-153 BO8-014 Kerrebrock, Jack L., B08-050 BO8-089 Davis, Roger L., BO8-153 Harinck, John, B08-035 Ketsdever, Andrew D., B08-165 Bazarov, Vladimir G., B08-064 DeHoyos, Amado, B08-137 Hassan, Ibrahim, B08-136 Khaleghi, Hossein, B08-132 Beck, Walter, B08-084 de la Loma, Adres, B08-091 Hattori, Eiji, BO8-044 Khodataev, Kirill V., BO8-116 Behera, Ramesh, B08-034 DeLuca, Luigi T., BO8-128 Haubelt, Lane C., B08-056 Kim, Heuy-dong, B08-028, Behr, Thomas, B08-133 Desai, Umesh C., B08-093 He, Li, B08-002 B08-088, B08-090 Bell, David L., B08-002 Dewallef, Pierre, B08-095 Heiser, W. H., B07-043TC, B07-127 Kim, Jae-hyung, B08-090 Bell, Theo A., B08-094 Doan, Son K., B08-027 TC Kim, Jinhan, B08-053, BO8-154 Bellows, Ben, B08-078 Dodson, Chris, B08-137 Heister, Stephen D., B08-041 Kim, Kwang-Yong, B08-037 Beloni, E., B08-168 Donovan, Eric S., B08-092 Hemchandra, Santosh, B08-167 Kim, Sehoon, B08-079 Berta, Paolo, B08-099 Dreizin, Edward L., B08-023, Henderson, John P., B08-093 Kimmel, Roger L., B08-113 Bingabr, Mohamed G., B08-031 B08-024, B08-025, B08-168 Henne, Ulrich, B08-084 King, Lyon B., B08-016, BO8-108 Bivolaru, Daniel, B08-082 Dressler, Rainer A., B08-108 Herrmann, Dirk, B08-029 King, Paul I., B08-048, B08-049, Bloxham, M., B08-152 D’ Souza, Brian C., B08-165 Hidding, Bernhard, B08-019 B08-056, B08-098 Bonanos, Aristides M., B08-033 Ebrahimi, Houshang B., B08-042 Hiernard, Fabrice, B08-020 Kitagawa, Kuniyuki, B08-043, Bons, J., BO8-152 Ede, J. D., B08-040 Hirano, Kohshi, B08-057 B08-044 Borguet, Sébastien, B08-095 Egorshev, Viacheslav Y, B08-128 Hirooka, Yasuro, B08-120 Knight, Doyle D., B08-143 Boroomand, Masoud, B08-132 Endo, Takuma, B07-127R Hirschen, Christian, B08-084 Kohga, Makoto, B08-060 Boswell, Rod W., B08-015 Engel, Jeffrey R., BO8-005 Hitch, Bradley D., B08-005 Komurasaki, Kimiya, B08-120 Boyce, R. R., B08-149 Farago, Zoltan, B08-063 Hiyamizu, Ryoma, B08-162 Korabelnikov, Alexey, B08-148 Boyd, lain D., B08-067 Faravelli, Tiziano, B08-099 Hochstein, John 1., BO8-011 Kosarev, Ilya N., B08-145 Bradley, Royce, BO8-157, BO8-158 Fayed, Mohamed, B08-036 Hodson, Howard Peter, B08-052 Kouchi, Toshinori, B08-057 Brezinsky, Kenneth, B08-130 Firth, John G., BO8-110 Hoffmann, Bettina, B08-134 Kozlov, Vyacheslav L., B08-104 Brooks, Kriston P., B08-070 Flanagan, Michael J., B08-049 Hoffmann, Vern K., B08-023, Krain, Hartmut, B08-134 Brown, Sarah P., B08-026 Frederick, Robert A., B08-026, B08-024, BO8-168 Krauss, Roland H., B08-124, Bruno, Claudio, B08-019 B08-064 Hoke, John, B08-157, B0O8-158 B08-126 Bruno, Thomas J., B08-076 Frenillot, Jean Philippe, B08-097 Holcomb, Frank, B08-071 Kumara Gurubaran, Ramaswamy, Burton, Rodney L., B08-071 Fridman, Alexander, B08-147 Holladay, Jamelyn D., B08-070 B08-135 Byers, David C., B08-164 Fu, Qing-fei, BO8-159 Houwing, A. F. P., B08-150 Kuo, Spencer, B08-082 Cai, Guo-biao, B08-159 Furuhata, Tomohiko, B08-073 Hrbud, Ivana, BO8-121 Kuranov, Alexander, B08-148 Caldwell, Nicholas, B08-158 Gaffney, Richard L., B08-089 Hreiz, Alex, B08-078 Kurian, Job, B08-080 Cao, Yong, B08-068 Gaitonde, Datta V., BO8-115 Hsu, Kaung-Yu, B08-056 Kwak, Hyun Duck, B08-053 Carter, Campbell D., B08-031, Gallagher-Rogers, A., B08-038 Hu, Jianli, B0O8-070 Kwon, Sejin, B08-079 B08-056, BO8-082 Gallier, Stany, BO8-020 Huang, Xiuquan, BO8-002 Landrum, D. Brian, B08-010 Casalino, Lorenzo, B08-059 Gallimore, Alec D., BO8-117, Humble, Pau! H., B08-070 Larocca, Francesco, B08-131 Castillon, Lionel, B08-091 B08-163 Hwang, Ki-Young, B08-101 Laroche, Emmanuel, B08-062 Cavitt, Ryan C., B08-064 Ganesh Anavaradham, T. K.., Inaba, Kazuaki, B07-127R Le, Daniel B., B08-124, B08-126 Cazalens, Michel, B08-065, B08-086 Ishii, Daisuke, B08-045 Lee, Hang-Gi, B08-154 B08-096, BO8-097 Gangoli, Shailesh, B08-147 Itoh, Takashi, B08-043, B08-044 Lee, Riki H., B08-165 Cervone, Angelo, B08-061 Ganguly, Biswa N., B08-129 Izumikawa, Muneo, B08-057 Lee, Sang, B08-156 Chakraborty, Debasis, B08-034 Gautam, Vivek, B08-109 Jackson, Thomas A., B08-082 Lee, Youngki, B08-088 Chakravarthy, Satyanarayanan R., Ge, Ming-he, B08-159 Jackson, Thomas L., B08-021 Lemaire, Ryan P., B08-049 B08-086, B08-135, BO8-166 Geng, Hui, B08-087 Jacobsen, Lance S., B08-082 Lempert, Walter R., B08-146 Charles, Christine, B08-015 Gimlin, Richard J., B08-071 Jameson, Kristina K., B08-107 Lentini, D., B08-160 Charles, Christopher S., B08-014 Girgis, Ihab, BO8-111 Jarrett, Jerome P., B08-094 Léonard, Olivier, B08-095 J. PROPULSION, VOI .. 24, NO. 6: 2008 INDEX Leonov, Sergey B., BO8-144 Nie, Chaoqun, B08-155 Schauer, Frederick R., B08-098, Tan, Hui-jun, BO8-030 Levin, Deborah A., B08-038 Nishihara, Munetake, B08-146 B08-157, BO8-158 Teixeira, Joao A., BO8-132 Li, Yun, B08-122 Nudnova, Maria M., B08-145 Schetz, Joseph A., B08-032, Thakre, Piyush, BO8-102 Liang, Jian-Han, B08-087 O’Brien, Timothy F., B08-083 B08-033, B08-085 Thakur, Amit, B08-006 Lieuwen, Tim, B08-078, BO8-167 O’Brien, Walter F., B08-033 Schoenitz, Mirko, B08-023, BO8-024 Thornton, Randall J., BO8-011 Lin, Feng, B08-155 O'Byrne, Sean, B08-150 Searby, Geoffrey, B08-062, B08-063 Throckmorton, Ryan, B08-085 Lin, Kuo-Cheng, B08-031 Ombrello, Timothy, B08-147 Segal, Corin, B08-006 Timko, Michael T., B08-072 Linck, Martin B., B08-109 Onasch, Timothy B., B08-072 Sensiau, Claude, B08-096 Timofeev, Evgeny, B08-125 Liu, Baojie, B08-001 Opoka, Maciej Marcin, B08-052 Seshadri, Soumitri, B08-024 Titov, Evgeny V., B08-038 Liu, Feng, B08-054 Orlov, Dmitriy M., B08-114 Setoguchi, Toshiaki, B08-028, Tomasi, Derek, BO8-128 Liu, Yangwei, B08-001 Oschwald, Michael, B08-063 B08-088, B08-090 Tomioka, Sadatake, B08-057 Locke, Justin M., B08-010 Paniagua, Guillermo, B08-091, Shafirovich, Evgeny, B08-047, Torre, Lucio, B08-061 Lorenzini, Enrico C., B08-105 BO8-151 B08-100 Torvik, Peter J., BO8-093 Loth, Eric, B08-156 Panneerselvam, S., B08-086 Shan, Jiayi, B08-043 Tousi, Abolghasem M., B08-132 Luo, Nie, B08-071 Papamoschou, Dimitri, B08-054 Shang, Joseph S., B08-113 Townsend, Jessica L., B08-050 Ma, Fuhua, B08-058 Park, Geunhong, B08-079 Shepherd, Joseph E., B08-008 Triesch, Klaus, B08-029 Macheret, Sergey O., BO8-111 Park, Pyun-Goo, B08-154 Shimo, Masayoshi, B08-041 Trunov, Mikhaylo A., B08-023, Maddalena, Luca, B08-032, B08-085 Pasini, Angelo, B08-061 Shimono, Masaya, B08-138 B08-025 Mahulikar, Shripad P., B08-075 Pastrone, Dario, B08-059 Shneider, Mikhail N., BO8-111 Tucker, Kelly Colin, B08-098 Majdalani, Joe, BO8-169 Pfitzner, Michael, B08-019 Shreenivasan, O. J., B08-086 Umbrajkar, Swati M., B08-024 Makela, Jason M., B08-016 Plourde, Frédéric, B08-027 Shumlak, Uri, B08-017 Uribarri, Luke, B08-069, B08-081 Manna, P., B08-034 Pluim, J., BO8-152 Shusser, Michael, B08-127 Utkin, Yurii G., BO8-146 Manzini, Giovanni, B08-151 Poggie, Jonathan, BO8-112 Shuzenji, Kiyotaka, B08-162 Van Dam, Jacques, B08-066 Marchetta, Jeffrey G., BO8-011 Poinsot, Thierry, B08-065, Shyy, Wei, B08-037 Varma, Arvind, B08-047, BO8-100 Marcum, Steven D., B08-129 B08-096 Simon, Thomas M., B08-070 Varvill, Richard, BO8-151 Markusic, Thomas E., B08-137 Polk, James E., B08-107 Simone, Domenico, B08-019 Vastistas, Georgios H., B08-036 Martinez, Rafael, B08-068 Polzin, Kurt A., B08-137 Sinditskii, Valery P., BO8-128 Veillard, Xavier, BO8-125 Martinez-Sanchez, Manuel, Post, Martiqua L., B0O8-114 Sislian, Jean P., BO8-003 Waitz, lan A., BO8-072 B08-119 Potnuru, Santosh K., B08-075 Sivaramakrishnan, Raghu, B08-130 Wang, Jiabin, B08-040 Massa, Luca, B08-021 Prasad, Subramanya, B08-075 Smith, Beverly L., B08-076 Wang, Joseph J., BO8-068 Massey, Dean R., B08-016 Preetham, B08-167 Smith, Katharine L., B08-110 Wang, Jun, BO8-022 Masuya, Goro, B08-057 Presz, Walter M., B08-139 Smith, Timothy B., B08-117 Wang, Meiping, B08-046 Mathew, Joseph, B08-004 Puri, Ishwar K., B08-099 Snyder, Philip H., B08-092 Wang, Zhen-Guo, B08-087 Matsuo, Akiko, B07-127R, B08-057 Raghunandan, B. N., B08-028 Solda, N., B08-160 Werle, Michael J., B08-139 Matsuo, Sigeru, B08-090 Raghunathan, S., B08-028 Sommerville, Jason D., BO8-108 West, Michael D., B08-015 McDaniel, James C., BO8-126 Rakitin, Aleksandr E., B08-009, Song, Bo, B08-051 Wickham, David T., B08-005 McGuire, J. R., BO8-149 B08-145 Song, Weidong, B08-017 Wight, Charles A., B08-022 Menart, James A., BO8-113 Ranzi, Eliseo, B08-099 Sonoda, Toyotaka, B08-051 Williams, George J., BO8-117 Merkle, Charles L., B08-042 Reader, Graham T., B08-046 Soroardy, Jomir U., B08-036 Williams, John, B08-068 Miake-Lye, Richard C., B08-072 Rebay, Stefano, B08-035 Springer, George S., B08-066 Williams, Skip, B08-082 Micci, Michael Matthew, B08-018 Reddy, K. U., B08-007 Sriram, A. T., B08-004 Wilson, Jack, B07-043R Mikellides, loannis G., B08-106, Reed, B., B0O8-038 Stanojev, Boris J., BO8-137 Wisman, David L., B08-129 BO8-107 Reilly, Michael P., B08-012 Starikovskaia, Svetlana M.., Wong, Hsi-Wu, B08-072 Miles, Richard B., B08-111 Reimann, D., BO8-152 B08-145 Yamashita, Hiroshi, B08-045 Miley, George H., B08-012, Rich, J. William, B08-146 Starikovskii, Andrei Y., B08-009, Yang, Li-jun, BO8-159 BO08-071 Romeo, Luca, B08-061 B08-145 Yang, Vigor, B08-058, BO8-102 Miller, Brian, B08-031 Rooney, Sean, B08-005 Stark, John P. W., BO8-110 Yarantsev, Dmitry, BO8-144 Mintoussov, Eugeny I., BO8-145 Roupassov, Dmitry V., B08-145 Stein, William, B08-121 Yasa, Tolga, BO8-091 Mishra, D. P., B08-007 Roux, Sébastien, B08-065, B08-096 Stickler, David M., B08-050 Yatsufusa, Tomoaki, B07-127R Mitcham, A. J., B08-040 Rovey, Joshua L., B08-163 Sujith, Raman I., B08-086, BO8-135, Yelvington, Paul E., BO8-072 Mohan, Salil, B08-025 Rubin, Binyamin, B08-013 B08-166 Yim, Yoo-Jin, BO8-101 Molder, Sannu, B08-125 Rullaud, Matthieu, B08-097 Sun, Ming-Bo, B08-087 Yoon, Suk Hwan, B08-053 Montes, Daniel R., B08-056 Rusek, John, B08-071 Sun, Shu, B08-030 Yu, Xianjun, BO8-001 Mori, Koichi, B08-039, BO8-120 Saito, Takayuki, B08-073 Sun, Z., B08-040 Zaidi, Sohail H., BO8-111 Mudford, N. R., BO8-149 Sallam, Khaled A., B08-031 Surzhikov, Sergey T., BO8-113 Zaretsky, Eugene, BO8-039 Naeem, Muhammad, B08-077 Samad, Abdus, B08-037 Suzuki, Koji, B08-103 Zhang, Jianye, BO8-072 Nakamura, Yuji, B08-045 Sanal Kumar, V. R., B08-028 Suzuki, Shingo, B08-138 Zhang, Jingxuan, BO8-155 Nalim, Razi, B08-092 Sanmartin, Juan R., BO8-105 Szokol, Szabolcs, B08-151 Zhang, Meng-zheng, B08-159 Nashif, Ahid, B08-093 Sasoh, Akihiro, B08-039, B08-103, Tachibana, Takeshi, B08-162 Zheng, Ming, B08-046 Neel, Reece, B08-085 B08-138 Tahir, Rabi, B08-125 Zhukov, Victor P., BO8-009, Ng, Wing, B08-051 Satake, Shingo, B08-045 Takaya, Ryota, BO8-103 B08-145 Nguyen, Chi Cong, B08-027 Sawada, Keisuke, B08-039, Taki, Shiro, BO7-127R Nicole, Aurélie, B08-062 B08-103, BO8-138 Tam, Chung-Jen, B08-082 J. PROPULSION, VOL. 24, NO. 6: 2008 INDEX Chronological Index B07-043 Effect of Pulse Length and Ejector Radius on Unsteady B08-012 Plume Expansion and Ionization in a Microlaser Plasma Ejector Performance. Jack Wilson, QSS Group, Inc. (23, 2, p. 345) Article Thruster. Michael P. Reilly and George H. Miley, University of Illinois at based on AIAA Paper 2005-3829 Urbana-Champaign; and William A. Hargus Jr., U.S. Air Force Research Technical Comment by W. H. Heiser, U.S. Air Force Academy (24, 1, Laboratory (24, 1, p. 111) Article based on AIAA Paper 2005-4072 p. 158) Technical Reply by Jack Wilson, WingCo, Ltd. (24, 1, p. 158) B08-013 Magnetic Sensing of Azimuthal Current in Hall Thrusters: In-Flight Diagnostic Potential. Binyamin Rubin, Alexander Kapulkin, and B07-127 Homogenous-Dilution Model of Partially Fueled Simplified Moshe Guelman, Technion-Israel Institute of Technology, Israel (24, 1, p. Pulse Detonation Engines. Takuma Endo, Tomoaki Yatsufusa, and Shiro 118) Article Taki, Hiroshima University, Japan, Akiko Matsuo, Keio University, Japan; Kazuaki Inaba, Tokyo University of Science, Japan; and Jiro Kasahara, B08-014 Near Exit Plane Velocity Field of a2 00-Watt Hall Thruster. University of Tsukuba, Japan (23, 5, p. 1033) Article based on AIAA Paper William A. Hargus Jr. and Christopher S. Charles, U.S. Air Force Research 2004-1214 Laboratory (24, 1, p. 127) Article Technical Comment by W. H. Heiser, U.S. Air Force Academy; and D. T. Pratt, University of Washington (24, 5, p. 1151) B08-015 Testing a Helicon Double Layer Thruster Immersed in a Technical Reply by Takuma Endo, Tomoaki Yatsufusa, and Shiro Taki, Space-Simulation Chamber. Michael D. West, Christine Charles, and Rod Hiroshima University, Japan, Akiko Matsuo, Keio University, Japan; W. Boswell, Australian National University, Australia (24, 1, p. 134) Article Kazuaki Inaba, Tokyo University of Science, Japan, and Jiro Kasahara, University of Tsukuba, Japan (24, 5, p. 1152) B08-016 Bismuth Hollow Cathode for Hall Thrusters. Jason M. Makela, Dean R. Massey, and Lyon B. King, Michigan Technological B08-001 Turbulence Models Assessment for Large-Scale Tip University (24, 1, p. 142) Technical Note based on AIAA Paper 2006-4634 Vortices in an Axial Compressor Rotor. Yangwei Liu, Xianjun Yu, and Baojie Liu, Beijing University of Aeronautics and Astronautics, China (ROC) B08-017 Charged Nanoparticle Source for High Thrust Level (24, 1, p. 15) Article Colloid Thruster. W. Song and U. Shumlak, University of Washington (24, |, p. 146) Technical Note B08-002 Effects of Tip Clearance on Aerodynamic Damping in a Linear Turbine Cascade. Xiuquan Huang and Li He, University of Durham, B08-018 Magnetic Flowmeter Burner Measurement of a Solid United Kingdom: and David L. Bell, ALSTOM Power, Ltd, United Kingdom Propellant Pressure-Coupled Imaginary Response. Michael M. Micci, (24, 1, p. 26) Article Pennsylvania State University (24, 1, p. 149) Technical Note B08-003 Computational Study of the Propulsive Characteristics of a B08-019 Silanes/H,O,: A High-Performance Synthetic Bipropellant Shcramjet Engine. Derrick C. Alexander and Jean P. Sislian, University of for Chemical Space Propulsion. B. Hidding, Heinrich-Heine-University Toronto, Canada (24, |, p. 34) Article Germany; M. Pfitzner, Universitaet der Bundeswehr Muenchen, Germany; C. Bruno and D. Simone, Universoif tRoym e “La Sapienza,” Italy (24, 1, p. 150) B08-004 Numerical Simulation of Transverse Injection of Circular Technical Note Jets into Turbulent Supersonic Streams. A. T. Sriram and Joseph Mathew, Indian Institute of Science, India (24, 1, p. 45) Article B08-020 Microstructure of Composite Propellants Using Simulated Packings and X-Ray Tomography. Stany Gallier and Fabrice Hiernard, SNPE Matériaux Energétiques, France (24, 1, p. 154) Technical Note B08-005 Additives to Improve Fuel Heat Sink Capacity in Air/Fuel Heat Exchangers. David T. Wickham, Jeffrey R. Engel, and Sean Rooney, TDA Research, Inc.; and Bradley D. Hitch, Reaction Systems, LLC (24, 1, p. B08-021 Multidimensional Numerical Simulation of Ammonium- 55) Article based on AIAA Paper 2005-3916 Perchlorate-Based Propellant Combustion with Fine/Ultrafine Alumi- num. L. Massa and T. L. Jackson, University of Illinois at Urbana- Champaign (24, 2, p. 161) Article B08-006 Concentration Distribution in Supersonic Flow Recircula- tion Region. Amit Thakur and Corin Segal, University of Florida (24, 1, p. 64) B08-022 Use of Condensed-Phase Reaction Models in Combustion Article Simulation of Energetic Materials. Jun Wang and Charles A. Wight, University of Utah (24, 2, p. 175) Article B08-007 Studies on Spray Behavior of a Pressure Swirl Atomizer in Transition Regime. K. U. Reddy and D P. Mishra, Indian Institute of B08-023 Combustion of Boron-Titanium Nanocomposite Powders Technology Kanpur, India (24, |, p. 74) Article in Different Environments. Mikhaylo A. Trunov, Vern K. Hoffmann, Mirko Schoenitz, and Edward L. Dreizin, New Jersey Institute of Technology (24, 2. B08-008 Single-Cycle Impulse from Detonation Tubes with Nozzles. p. 184) Article based on AIAA Paper 2006-4809 M. Cooper, Sandia National Laboratories; and J. E. Shepherd, California Institute of Technology (24, |, p. 81) Article B08-024 Aluminum-Rich Al-MoO, Nanocomposite Powders Pre- pared by Arrested Reactive Milling. Swati M. Umbrajkar, Soumitri B08-009 Effect of High-Voltage Pulsed Discharges on Deflagration to Seshadri, Mirko Schoenitz, Vern K. Hoffmann, and Edward L. Dreizin, New Detonation Transition. V. P. Zhukov, A. E. Rakitin, and A. Yu. Starikovskii, Jersey Institute of Technoiogy (24, 2, p. 192) Article based on AIAA Paper Moscow Institute of Physics and Technology, Russia (24, 1, p. 88) Article 2007-294 B08-010 Study of Heat Transfer Correlations for Supercritical B08-025 Heating and Ignition of Metallic Particles by a CO, Laser. Hydrogen in Regenerative Cooling Channels. Justin M. Locke and D. Brian Salil Mohan, Mikhaylo A. Trunov, and Edward L. Dreizin, New Jersey Landrum, University of Alabama in Huntsville (24, 1, p. 94) Article Institute of Technology (24, 2, p. 199) Article B08-011 Microgravity Geyser and Flowfield Prediction. J. I. B08-026 Laboratory-Scale Thermal Stability Experiments on RP-1 Hochstein and J. G. Marchetta, University of Memphis; and R. J. Thornton, and RP-2. Sarah P. Brown and Robert A. Frederick Jr., UAH Propulsion NASA Marshall Space Flight Center (24, 1, p. 104) Article Research Center (24, 2, p. 206) Article based on AIAA Paper 2005-3850 J. PROPULSION, VOI .. 24, NO. 6: 2008 INDEX 1433 B08-027 Analysis of Injecting Wall Inclination on Segmented Solid B08-041 Multicyclic-Detonation-Initiation Studies in Valveless Rocket Motor Instability. Chi Cong Nguyen, Frédéric Plourde, and Son Kim Pulsed Detonation Combustors. Masayoshi Shimo and Stephen D. Heister, Doan, Ecole Nationale Superieurede Mecanique et d'Aerotechnique, France Purdue University (24, 2, p. 336) Article based on AIAA Paper 2006-4308 (24, 2, p. 213) Article B08-042 Wave Reverberations in Multitube Pulse Detonation B08-028 Boundary-Layer Effects on Internal Flow Choking in Dual- Engines. Houshang B. Ebrahimi, Aerospace Testing Alliance; and Charles Thrust Solid Rocket Motors. V. R. Sanal Kumar, Vikram Sarabhai Space L. Merkle, Purdue University (24, 2, p. 345) Article Centre, India, B. N. Raghunandan, Indian Institute of Science, India; T. Kawakami, Hosei University, Japan; H. D. Kim, Andong National University, B08-043 Thermoelectric Properties of {-Zn,Sb, Synthesized by Republic of Korea, T. Setoguchi, Saga University, Japan, and S. Mechanical Alloying and Pulse Discharge Sintering. Takashi Itoh, Jiayi Raghunathan, Queens University Belfast, United Kingdom (24, 2, p. 224) Shan, and Kuniyuki Kitagawa, Nagoya University, Japan (24, 2, p. 353) Article based on AIAA Paper 2006-4432 Article based on AIAA Paper 2004-5564 B08-029 Experimental Study of Chin Intakes for Airbreathing B08-044 Thermoelectric Properties of lron-and Lanthanum-Doped Missiles with High Agility. Dirk Herrmann, Klaus Triesch, and Ali Giilhan, CoSb3 Compounds by Pulse Discharge Sintering. Takashi Itoh, Eiji DLR, German Aerospace Center, Germany (24, 2, p. 236) Article Hattori, and Kuniyuki Kitagawa. Nagoya University, Japan (24, 2, p. 359) B08-030 Preliminary Study of Shock Train in a Curved Variable- Article Section Diffuser. Hui-jun Tan and Shu Sun, Nanjing University of Aeronautics and Astronautics, China (ROC) (24, 2, p. 245) Article B08-045 Sight-Premixing Effects on Oxidation/Formation of Polycyclic Aromatic Hydrocarbon in Counterflow Flames. Yuji B08-031 Breakup of Aerated Liquid Jets in Subsonic Crossflow. B. Nakamura, Hokkaido University, Japan: Daisuke Ishii, Shingo Satake, and Miller and K. A. Sallam, Oklahoma State University; M. Bingabr, University Hiroshi Yamashita, Nagoya University, Japan (24, 2, p. 365) Article of Central Oklahoma: K.-C, Lin, Taitech, Inc.; and C. Carter, U.S. Air Force Research Laboratory (24, 2, p. 253) Article based on AIAA Paper 2007-1342 B08-046 Investigation of Active Flow Control on Diesel Engine Aftertreatment. Ming Zheng, Graham T. Reader, and Meiping Wang, B08-032 Flush-Wall, Diamond-Shaped Fuel Injector for High Mach University of Windsor, Canada (24, 2, p. 376) Article based on AIAA Paper Number Scramjets. Peter M. Grossman, Luca Maddalena, and Joseph A. OS2-2-3 Schetz, Virginia Polytechnic Institute and State University (24, 2, p. 259) Article B08-047 Metal-CO, Propulsion for Mars Missions: Current Status and Opportunities. Evgeny Shafirovich and Arvind Varma, Purdue B08-033 Dual-Mode Combustion Experiments with an Integrated University (24, 3, p. 385) Survey Paper based on AIAA Paper 2007-5126 Aeroramp-Injector/Plasma-Torch Igniter. Aristides M. Bonanos, Joseph A. Schetz. and Walter F. O’Brien, Virginia Polytechnic Institute and State B08-048 Low-Heat-Load-Vane Profile Optimization, Part 1: Code University; and Christopher P. Goyne, University of Virginia (24, 2, p. 267) Validation and Airfoil Redesign. Jamie J. Johnson and Paul I. King, Air Article Force Institute of Technology: and John P. Clark, U.S. Air Force Research Laboratory (24, 3, p. 395) Article based on AIAA Paper 2006-3386 B08-034 Liquid-Fueled Strut-Based Scramjet Combustor Design: A Computational Fluid Dynamics Approach. P. Manna, Ramesh Behera, and B08-049 Low-Heat-Load-Vane Profile Optimization, Part 2: Short- Debasis Chakraborty, Defense Research and Development Laboratory, India (24, 2, p. 274) Article Duration Shock-Tunnel Experiments. Jamie J. Johnson, Paul I. King, John P. Clark, Michael J. Flanagan, and Ryan P. Lemaire, Air Force Institute of B08-035 Real-Gas Effects in Organic Rankine Cycle Turbine Technology (24, 3, p. 403) Article based on AIAA Paper 2006-3386 Nozzles. P. Colonna and J. Harinck, Delft University of Technology, The Netherlands, S. Rebay, Universita Degli Studi di Brescia, Italy; and A. B08-050 Experimental Evaluation of a Turbine Blade with Guardone, Politecnico di Milano, Italy (24, 2, p. 282) Article Potassium Evaporative Cooling. Jessica L. Townsend, Franklin W. Olin College of Engineering: Jack Kerrebrock, Massachusetts Institute of B08-036 Strongly Swirling Turbulent Sink Flow Between Two Technology; and David Stickler, Aerodyne Research, Inc. (24, 3, p. 410) Stationary Disks. G. H. Vatistas, M. Fayed, and J. U. Soroardy, Concordia Article based on AIAA Paper 2004-3571 University, Canada (24, 2, p. 295) Article B08-051 Loss Mechanisms of High-Turning Supercritical Compres- B08-037 Multiple Surrogate Modeling for Axial Compressor Blade sor Cascades. Bo Song. Gardner Denver, Inc.. Wing Ng, Virginia Shape Optimization. Abdus Samad and Kwang-Yong Kim, /nha University, Polytechnic Institute and State University: Toyotaka Sonoda and Toshiyuki Republico f Korea; Tushar Goel and Raphael T. Haftka, University of Florida; Arima, Honda R&D Co., Ltd., Japan (24, 3, p. 416) Article and Wei Shyy, University of Michigan (24, 2, p. 302) Article B08-052 Experimental Investigation of Unsteady Transition B08-038 Examination of a Collision-Limiter Direct Simulation Processes on High-Lift T106A Turbine Blades. M. M. Opoka and H. P. Monte Carlo Method for Micropropulsion Applications. E. Titov, A. Hodson, Cambridge University, United Kingdom (24, 3, p. 424) Articie based Gallagher-Rogers, and D. Levin, Pennsylvania State University, and Brian on AIAA Paper 2005-1227 Reed, NASA John H. Glenn Research Center at Lewis Field (24, 2, p. 311) Article B08-053 Rotordynamic Analysis of a Turbopump with the Casing B08-039 Time-Resolved Measurements of Impulse Generation in Structural Flexibility. Seong Min Jeon, Hyun Duck Kwak, Suk Hwan Yoon, Pulsed Laser-Ablative Propulsion. Kohei Anju and Keisuke Sawada, and Jinhan Kim, Korea Aerospace Research Institute, Republic of Korea (24, Tohoku University, Japan; Akihiro Sasoh and Koichi Mori, Nagoya 3, p. 433) Article based on AIAA Paper 2007-5543 University, Japan; and Eugene Zaretsky, Ben-Gurion Universityo f the Negev, Israel (24, 2, p. 322) Article based on AIAA Paper 2007-4389 B08-054 Aerodynamics of Fan Flow Deflectors for Jet Noise Suppression. Dimitri Papamoschou and Feng Liu, University of California, B08-040 Testing of a 250-Kilowatt Fault-Tolerant Permanent Irvine (24, 3, p. 437) Article based on AIAA Paper 2005-0994 Magnet Power Generation System for Aeroengines. Z. Sun, J. D. Ede, J. Wang, and G. W. Jewell, University of Sheffield, United Kingdom, J. J. A. B08-055 Investigation of Two-Dimensional Scramjet Inlet Flowfield Cullen, and A. J. Mitcham, Rolls-Royce plc, United Kingdom (24, 2, p. 330) at Mach 7. Jiirgen Hiiberle and Ali Giilhan, DLR, German Aerospace Center, Article based on AIAA Paper 2007-4829 Germany (24, 3, p. 446) Article based on AIAA Paper 2007-5068 1434 J. PROPULSION, VOL. 24, NO. 6: 2008 INDEX B08-056 Experimental Studies of Pylon-Aided Fuel Injection into a B08-070 Compact Reverse Water-Gas-Shift Reactor for Extra- Supersonic Crossflow. Mark R. Gruber and Campbell D. Carter, U.S. Air terrestrial In Situ Resource Utilization. J. D. Holladay, K. P. Brooks, P. Force Research Laboratory, Daniel R. Montes, Lane C. Haubelt, and Paul I. Humble, and J. Hu, Pacific Northwest National Laboratory; and T. M. Simon, King, Air Force Institute of Technology, and Kaung-Yu Hsu, Innovative NASA Johnson Space Center (24, 3, p. 578) Article Scientific Solutions, Inc. (24, 3, p. 460) Article B08-071 Hydrogen-Peroxide-Based Fuel Cells for Space Power B08-057 Matched Pressure Injections into a Supersonic Crossflow Systems. Nie Luo, George H. Miley, Richard J. Gimlin, and Rodney L. Through Diamond-Shaped Orifices. Sadatake Tomioka and Muneo Burton, University ofI llinois; John Rusek, Swift Enterprises, Ltd.; and Frank Izumikawa, Japan Aerospace Exploration Agency, Japan; Toshinori Kouchi Holcomb, U.S. Army Engineer Research and Development Center (24, 3, p. and Goro Masuya, Tohoku University, Japan; Kohshi Hirano and Akiko 583) Article based on AIAA Paper 2005-5755 Matsuo, Keio University, Japan (24, 3, p. 471) Article based on AIAA Paper 2007-5402 B08-072 Microphysical Modeling of Ground-Level Aircraft-Emitted Aerosol Formation: Roles of Sulfur-Containing Species. Hsi-Wu Wong, B08-058 Internal Flow Dynamics in a Valveless Airbreathing Pulse Paul E. Yelvington, Michael T. Timko, Timothy B. Onasch, and Richard C. Detonation Engine. Fuhua Ma, Jeong-Yeol Choi, and Vigor Yang, Miake-Lye, Aerodyne Research, Inc.; Jianye Zhang and Ian A. Waitz, Pennsylvania State University (24, 3, p. 479) Article based on AIAA Paper Massachusetts Institute of Technology (24, 3, p. 590) Article 2007-1251 B08-073 Effect of Biodiesel Fuel on Direct Injection Diesel Engine B08-059 Optimal Design of Hybrid Rocket Motors for Microgravity Performance. M. Arai, T. Saito, and T. Furuhata, Gunma University, Japan Platform. Lorenzo Casalino and Dario Pastrone, Politecnico di Torino, Italy (24, 3, p. 603) Article (24, 3, p. 491) Article B08-074 Expectations of Closed-Brayton-Cycle Heat Exchangers in B08-060 Burning Rate Characteristics of Ammonium Perchlorate- Space Power Systems. Michael J. Barrett, NASA John H. Glenn Research Based Composite Propellant Using Bimodal Ammonium Perchlorate. Center at Lewis Field; and Paul K. Johnson, Analex Corporation (24, 3, p. Makoto Kohga, National Defense Academy, Japan (24, 3, p. 499) Article 609) Technical Note based on AIAA Paper 2004-5652 based on AIAA Paper 2006-4924 B08-074E Erratum on Expectations of Closed-Brayton-Cycle Heat B08-061 Testing and Characterization of a Hydrogen Peroxide Exchangers in Space Power Systems. Michael J. Barrett, NASA John H. Monopropellant Thruster. A. Pasini, L. Torre, L.R omeo, A. Cervone, and L. Glenn Research Center at Lewis Field; and Paul K. Johnson, Analex d’ Agostino, ALTA S.p.A., Italy (24, 3, p. 507) Article based on AIAA Paper Corporation (24, 4, p. 896) 2007-5465 B08-075 Infrared Signature Suppression of Helicopter Engine Duct B08-062 Prediction of the Efficiency of Acoustic Damping Cavities. Based on “Conceal and Camouflage.” S. P. Mahulikar, H. S. S. Prasad, and Geoffrey Searby, Centre National de la Recherche Scientifique and Aix- S. K. Potnuru, /ndian Institute of Technology, Bombay, India (24, 3, p. 613) Marseille University, France, Aurélie Nicole, Mohammed Habiballah, and Technical Note Emmanuel Laroche, ONERA, France (24, 3, p. 516) Article B08-076 Application of a Composition-Explicit Distillation Curve B08-063 Resonance Frequencies and Damping of a Combustor Metrology to Mixtures of Jet-A and S-8. Beverly L. Smith and Thomas J. Acoustically Coupled to an Absorber. Michael Oschwald and Zoltan Bruno, National Institute of Standards and Technology (24, 3, p. 618) Farago, DLR, German Aerospace Center, Germany, Geoff Searby and Technical Note Francois Cheuret, Centre National de la Recherche Scientifique and Aix- Marseille Université, France (24, 3, p. 524) Article B08-077 Implications of Day Temperature for a High-Pressure- Turbine Blade’s Low-Cycle-Fatigue Life Consumption. Muhammad B08-064 Laboratory Scale Survey of Pentad Injector Stability Naeem, National University of Sciences and Technology Pakistan (24, 3, p. Characteristics. Ryan C. Cavitt and Robert A. Frederick, University of 624) Technical Note Alabama in Hunstville; and Vladimir G. Bazarov, Moscow Aviation Institute (24, 3, p. 534) Article based on AIAA Paper 2007-5587 B08-078 Nonlinear Interactions Between Forced and Self-Excited Acoustic Oscillations in Premixed Combustor. Benjamin D. Bellows, Alex B08-065 Outlet-Boundary-Condition Influence for Large Eddy Hreiz, and Tim Lieuwen, Georgia Institute of Technology (24, 3, p. 628) Simulation of Combustion Instabilities in Gas Turbines. S. Roux, Centre Technical Note based on AIAA Paper 2006-0755 Europeen de Recherche et de Avancee en Calcul Scientifique, France; M. Cazalens, Societe Nationale d'Etude et de Construction de Moteurs B08-079 A Starting Procedure of Supersonic Ejector to Minimize d’Aviation, France; and T. Poinsot, Institut des Mecanique des Fluides de Primary Pressure Load. Geunhong Park, Sehoon Kim, and Sejin Kwon, Toulouse, France (24, 3, p. 541) Article Korea Advanced Institute of Science and Technology, Republic of Korea (24, 3, p. 631) Technical Note B08-066 Ultrasonic Propulsion. Eric M. Allison, George S. Springer, and Jacques Van Dam, Stanford University (24, 3, p. 547) Article B08-080 Performance of Aft-Ramp Cavities for Flame Stabilization in Supersonic Flows. M. C. Mohamed Ali, Thangu! Kunju Musaliar College B08-067 Particle Simulation of Plume Flows from an Anode-Layer of Engineering, India; and Job Kurian, Indian Institute of Technology, India Hall Thruster. Yongjun Choi, Michael Keidar, and lain D. Boyd, University (24, 3, p. 635) Technical Note of Michigan (2A, 3, p. 554) Article based on AIAA Paper 2006-5026 B08-081 Corruption of Pulsed Electric Thruster Voltage Fluctuation B08-068 Numerical and Experimental Investigations of Crossover Measurements by Transmission Line Resonances. Luke Uribarri and E. Y. Ion Impingement for Subscale Ion Optics. Joseph J. Wang, Yong Cao, and Choueiri, Princeton University (24, 3, p. 637) Technical Note based on AIAA Raed Kafafy, Virginia Polytechnic Institute and State University, Rafael Paper 2007-5295 Martinez and John Williams, Colorado State University (24, 3, p. 562) Article based on AIAA Paper 2007-5244 B08-082 Plasma-Assisted Ignition in Scramjets. Lance S. Jacobsen, Campbell D. Carter, Thomas A. Jackson, Skip Williams, and Jack Barnett, B08-069 Relationship Between Anode Spots and Onset Voltage Hash U.S. Air Force Research Laboratory, Chung-Jen Tam and Robert Baurle, in Magnetoplasmadynamic Thrusters. Luke Uribarri and Edgar Y. Tiatech, Inc.; Daniel Bivolaru and Spencer Kuo, Polytechnic University (24, 4, Choueiri, Princeton University (24, 3, p. 571) Article p. 641) Article based on AIAA Paper 2003-871