Table Of Content

JOURNAL OF PROPULSION AND POWER Vol. 26, No. 6, November—December 2010 2010 Journal of Propulsion and Power Index How to Use the Index In the Subject Index, pages 1331-1336, each technical paper is listed under a maximum of three appropriate headings. Note the locating number in boldface type preceding each paper title, and use that number to find the paper in the Chronological Index. The Author Index, pages 1337—1338, lists all authors associated with a given technical paper. The locating numbers are identical to those in the Subject Index. The Chronological Index, pages 1339-1344, 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 directly beneath the paper to which they refer. If the paper to which they refer was published prior to 2010, 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, B10-088 Shock-Tube Experiments and Kinetic FLUID DYNAMICS Modeling of Toluene Ignition CONVENTIONAL, STOL/VTOL {eroacoustics Manufacturing Aerodynamics B10-035 Core Noise Diagnostics of Turbofan B10-040 Ultrasonically Aided Electrospray B10-069 Direct Numerical Simulations of Transi- Source for Charged Particles Approaching Engine Noise Using Correlation and Coherence tional and Turbulent Flow on a Turbine Airfoil Monodisperse Distributions Functions B10-139 Inlet Starting of High-Contraction B10-129 Separating Direct and Indirect Turbofan Axisymmetric Scramjets Noise Engine Combustion Noise Using the Correlation B10-147 Wind Turbine Wall-Blockage Perform- B10-035 Core Noise Diagnostics of Turbofan Function ance Corrections Engine Noise Using Correlation and Coherence Boundary Layers and Heat Transfer- B10-003 Unsteady Blade Loading with Clocking Functions Laminar in Multistage Axial Compressors, Part 2 B10-142 Hybrid Reynolds-Averaged Navier Testing, Flight and Ground B10-010 Sidewall Boundary Layers of the Stokes/Kinetic-Eddy Simulation of Stall Incep- B10-028 Investigation of Rocket Exhaust Dif Bidirectional Vortex tion in Axial Compressors fusers for Altitude Simulation Boundary Layers and Heat Transfer- B10-002 Unsteady Blade Loading with Clocking Turbulent in Multistage Axial Compressors, Part | ENERGY B10-025 Simulation of Shock/Boundary-Layer Airframe-Propulsion Integration Interactions with Bleed Using Immersed-Boun- Alternate Fuels B10-122 Investigation of a Fluidic Shock Control dary Methods Method for Hypersonic Inlets B10-036 Emissions Characieristics of Military B10-095 Film Effectiveness Measurements on the Helicopter Engines with JP-8 and Fischer Pressure Surface of a Transonic Airfoil Configuration Design Tropsch Fuels B10-107 Inclined Jet in Crossflow Interacting B10-034 influence of Configuration on Materials B10-057 Simultaneous Pressure and Optical with a Vortex Generator ; Selection for Actively Cooled Combustors Measurements of Nanoaluminum Thermites Investigating the Reaction Mechanism Computational Fluid Dynamics |. Flow Control B10-133 Energy Content and Alternative Jet Fuel B10-075 Effects of Wavy Surface Roughness on B10-060 Experimental Study on Flow Transition Viability the Performance of Micronozzles in Dual Bell Nozzles B10-028 Investigation of Rocket Exhaust Dif- Batteries B10-094 Flow Control in a Compressor Cascade fusers for Altitude Simulation at High Incidence B10-074 Batteries for Venus Surface Operation B10-038 Harmonic Balance Analysis of Blade B10-093 Controlling Separation on a Simulated Fuel Economy Row Interactions in a Transonic Compressor Compressor Blade Using Vortex-Generator Jets B10-069 Direct Numerical Simulations of Transi- B10-149 Ejector Thrust Augmentation B10-121 Unstart Detection in a Simplified- tional and Turbulent Flow on a Turbine Airfoil Geometry Hypersonic Inlet-Isolator Flow Nuclear Fission B10-137 Numerical Investigation of Transverse B10-120 Effects of Magnetohydrodynamic Inter- B10-019 High-Power Brayton Rotating Unit for Jets Through Multiport Injector Arrays in a nBiste action-Zone Position on Shock-Wave/Boundary- Reactor and Solar Dynamic Power Systems Supersonic Crossflow OeeeOeEvea aeet T e, Layer Interaction B10-142 Hybrid Reynolds-Averaged Navier- B10-107 Inclined Jet in Crossflow Interacting Rotating Machinery Stokes/Kinetic-Eddy Simulation of Stall Incep- Tew with a Vortex Generator B10-037 Effects of Axial Gap on the Vane—Rotor tion in Axial Compressors Interaction in a Low Aspect Ratio Turbine Stage B10-079 Heat Flux and Pressure Profiles in an Fuels and Fuel Systems B10-048 Dynamic Simulation of a Space Reactor Oxygen/Hydrogen Multielement Rocket Com- B10-036 Emissions Characteristics of Military System with Closed Brayton Cycle Loops bustor Helicopter Engines with JP-8 and Fischer B10-008 Scalar Filtered Density Function for Tropsch Fuels Wind Power Large Eddy Simulation of a Bunsen Burner B10-133 Energy Content and Alternative Jet Fuel B10-147 Wind Turbine Wall-Blockage Perform- B10-024 Modeling of Fixed-Exit Porous Bleed Viability ance Corrections Systems for Supersonic Inlets 1331 1332 J. PROPULSION, VOL. 26, NO. 6: 2010 INDEX B10-105 Large-Eddy Simulation of Flame-Tur- Multiphase Flows Supersonic Flow bulence Interactions in a Shear Coaxial Injector B10-135 Experimental Study of Fluid Jet Mixing B10-043 Experimental and Numerical Studies of B10-132 Spray Generated by an Airblast Atom- at Supercritical Conditions Diamond-Shaped Injector in a Supersonic Flow izer Under Elevated Ambient Pressures B10-115 Thrust Augmentation of Solid Rocket B10-064 Hybrid Reynolds-Averaged and Large- B10-140 Parametric Study of the Generation of Motors Using Beamed Microwave Energy Eddy Simulation of Normal Injection into a Shocks in Near-Critical Turbofan Nozzles B10-054 Reduced-Order Model for H,O, Cata- Supersonic Crossflow B10-031 Improved Spray Model for Viscous lytic Reactor Performance Analysis B10-025 Simulation of Shock/Boundary-Layer Annular Sheets in a Swirl Injector B10-132 Spray Generated by an Airblast Atom- Interactions with Bleed Using Immersed-Boun- B10-068 Direct Numerical Simulations of Transi- izer Under Elevated Ambient Pressures dary Methods tional/ Turbulent Wake of a Flat Plate B10-031 Improved Spray Model for Viscous B10-090 Hydroxyl-Tagging-Velocimetry Meas- B10-073 Aerodynamic Heating of Reentry Body Annular Sheets in a Swirl Injector urements of a Supersonic Flow over a Cavity Equipped with Onboard-Surface Hall Magneto- B10-060 Experimental Study on Flow Transition hydrodynamic Generator Plasmadynamics and in Dual Bell Nozzles B10-123 Numerical Investigation of the Super- Magnetohydrodynamics B10-006 Feedback Combustion Control Using sonic Combustion of Kerosene in a Strut-Based B10-077 Particle-Based Plasma Simulations for Chemi-Ionization Probe in Supersonic Flow of Combustor an Ion Engine Discharge Chamber Combustion Products Hydrodynamics B10-073 Aerodynamic Heating of Reentry Body B10-099 Empirical Equation for Self-Starting Equipped with Onboard-Surface Hall Magneto- Limit of Supersonic Inlets B10-135 Experimental Study of Fluid Jet Mixing hydrodynamic Generator B10-091 Extended Quantitative Fluorescence at Supercritical Conditions B10-017 Numerical Rebuilding of SMART-1 Imaging for Multicomponent and Staged Injection Hypersonic Flow Hall Effect Thruster Plasma Plume into Supersonic Crossflows B10-120 Effects of Magnetohydrodynamic Inter- B10-005 Supersonic Boundary-Layer Combus- B10-099 Empirical Equation for Self-Starting action-Zone Position on Shock-Wave/Boundary- tion: Effects of Upstream Entropy and Shear- Limit of Supersonic Inlets Layer Interaction Layer Thickness B10-139 Inlet Starting of High-Contraction Axisymmetric Scramjets Rarefied Flows B10-065 Reduced-Order Modeling of Two- Dimensional Supersonic Flows with Applications B10-017 Numerical Rebuilding of SMART-1 Inlet, Nozzle, Diffuser, and Channel Hall Effect Thruster Plasma Plume to Scramjet Inlets Flows B10-062 Assessment of Seeder Performance for Reacting Flows and Combustion Particle Velocimetry in a Scramjet Combustor B10-028 Investigation of Rocket Exhaust Dif- fusers for Altitude Simulation B10-059 Analysis of Gas-Dynamic Effects in B10-026 Effect of Swirl on Shock Structure in B10-075 Effects of Wavy Surface Roughness on Explosively Actuated Valves Underexpanded Supersonic Airflow the Performance of Micronozzles B10-105 Large-Eddy Simulation of Flame-Tur- B10-122 Investigation of a Fluidic Shock Control bulence Interactions in a Shear Coaxial Injector Transonic Flow Method for Hypersonic Inlets B10-006 Feedback Combustion Control Using B10-095 Film Effectiveness Measurements on the B10-101 Study of Detonation Interactions Inside Chemi-Ionization Probe in Supersonic Flow of Pressure Surface of a Transonic Airfoil a Two-Dimensional Ejector Using Detonation Combustion Products B10-140 Parametric Study of the Generation of Transmission Tubing B10-123 Numerical Investigation of the Super- Shocks in Near-Critical Turbofan Nozzles B10-080 Engineering Model for Self-Pressuriz- sonic Combustion of Kerosene in a Strut-Based B10-026 Effect of Swirl on Shock Structure in ing Saturated-N,O-Propellant Feed Systems Combustor B10-145 Laser Pulsejet with Beam Concentration B10-112 Model for Melt-Layer Front in Ammo- Underexpanded Supersonic Airflow by Multiple Reflections in a Sharp-Cone Nozzle nium Perchlorate Propellant Combustion B10-085 Swirling Airflow Through a Nozzle: B10-084 Exhaust of Underexpanded Jets from B10-008 Scalar Filtered Density Function for Choking Criteria Finite Reservoirs Large Eddy Simulation of a Bunsen Burner B10-024 Modeling of Fixed-Exit Porous Bleed Separated Flows Unsteady Flows Systems for Supersonic Inlets B10-109 High-Performance Rocket Nozzle Con- B10-078 Instability Characteristics of a Gaseous- : B10-085 Swirling Airflow Through a Nozzle: Oxygen/Methane Pentad Injector cept Choking Criteria B10-089 Particle Image Velocimetry Character- B10-120 Effects of Magnetohydrodynamic Inter- B10-140 Parametric Study of the Generation of ization of High-Speed Centrifugal Compressor Shocks in Near-Critical Turbofan Nozzles aLcatyieorn -IZnotneera ctPioosni tion on Shock-Wave/Boundary- Impeller—Diffuser Interaction 9 B10-026 Effect of Swirl on Shock Structure in B10-142 Hybrid Reynolds-Averaged Navier— B10-038 Harmonic Balance Analysis of Blade Underexpanded Supersonic Airflow Stokes/Kinetic-Eddy Simulation of Stall Incep- Row Interactions in a Transonic Compressor B10-099 Empirical Equation for Self-siarting tion in Axial Compressors B10-037 Effects of Axial Gap on the Vane—Rotor Limit of Supersonic Inlets Interaction in a Low Aspect Ratio Turbine Stage Shock Waves and Detonations B10-101 Study of Detonation Interactions Inside Jets, Wakes, and Viscid-Inviscid Flow B10-025 Simulation of Shock/Boundary-Layer a Two-Dimensional Ejector Using Detonation Interactions Interactions with Bleed Using Immersed-Boun- Transmission Tubing B10-039 Rotor Wake Variability in a Multistage dary Methods B10-084 Exhaust of Underexpanded Jets from ae2aSoi tR t eh Compressor B10-084 Exhaust of Underexpanded Jets from Finite Reservoirs B10-125 Molecular Weight and Shock-Wave Finite Reservoirs B10-004 Sensitivity of Turbine Efficiency and Effects on Transverse Injection in Supersonic B10-101 Study of Detonation Interactions Inside Flow Structures to Varying Purge Flow Flow a Two-Dimensional Ejector Using Detonation B10-091 Extended Quantitative Fluorescence Transmission Tubing Imaging for Multicomponent and Staged Injection B10-032 Ignition Delay Time Measurements of Vortices into Supersonic Crossflows Normal Alkanes and Simple Oxygenates B10-004 Sensitivity of Turbine Efficiency and B10-106 Nozzle-Geometry Effects on Upwind- Flow Structures to Varying Purge Flow Surface Properties of Turbulent Liquid Jets in Subsonic Flow B10-010 Sidewall Boundary Layers of the Gaseous Crossflow B10-138 Experimental Study of Cavity-Strut Bidirectional Vortex B10-137 Numerical Investigation of Transverse Combustion in Supersonic Flow B10-141 Leading-Edge Endwall Suction and Jets Through Multiport Injector Arrays in a B10-147 Wind Turbine Wall-Blockage Perform- Midspan Blowing to Reduce Turbomachinery Supersonic Crossflow ance Corrections Losses J. PROPULSION, VOL. 26, NO. 6: 2010 INDEX 1333 GUIDANCE, CONTROL, AND B10-051 Optimal Design of Hybrid Rocket B10-092 Rotating Stall Suppression in Axial Motors for Launchers Upper Stages Compressors with Casing Plasma Actuation DYNAMICS TECHNOLOGY B10-082 Microstructure Effects in Aluminized B10-145 Laser Pulsejet with Beam Concentration Astrodynamics Solid Rocket Propellants by Multiple Reflections in a Sharp-Cone Nozzle B10-047 Three-Body Dynamics and Self-Power- B10-138 Experimental Study of Cavity-Strut Simulation ing of an Electrodynamic Tether in a Plasmasphere Combustion in Supersonic Flow B10-029 Performance Evaluation of Second- B10-061 Raman Scattering Measurements of Control System Sensors Throat Diffuser for High-Altitude-Test Facility Gaseous Ethylene Jets in a Mach 2 Supersonic B10-006 Feedback Combustion Control Using Crossflow Testing, Flight and Ground Chemi-lonization Probe in Supersonic Flow of B10-137 Numerical Investigation of Transverse Combustion Products B10-096 Influence of Intake Orientation on Jets Through Multiport Injector Arrays in a Ramjet Performance Supersonic Crossflow Engine Control B10-029 Performance Evaluation of Second- B10-021 Isolator/Combustion Chamber Interac- B10-067 Modeling, Simulation, and Controller Throat Diffuser for High-Altitude-Test Facility tions During Supersonic Combustion Design for an Air-Breathing Combustion System B10-003 Unsteady Blade Loading with Clocking Thermal Protection Systems Optimization Techniques in Multistage Axial Compressors, Part 2 B10-034 Influence of Configuration on Materials B10-005 Supersonic Boundary-Layer Combus- B10-033 Optimization of Secondary-Air Addi- Selection for Actively Cooled Combustors tion: Effects of Upstream Entropy and Shear- tion in a Continuous One-Dimensional Spray Layer Thickness Combustor PROPULSION B10-024 Modeling of Fixed-Exit Porous Bleed Remote Control Systems for Supersonic Inlets B10-023 Laser Ablation Propulsion Tractor Beam Advanced Space Propulsion B10-066 Role of Tip Clearance Flow in Rotating System B10-072 Review: Laser-Ablation Propulsion Instabilities and Nonsynchronous Vibrations B10-042 Electrostatic Plasma Brake for Deorbit- B10-097 Numerical Simulation of Supersonic INTERDISCIPLINARY TOPICS ing a Satellite Nonpremixed Turbulent Combustion in a B10-052 Film Cooling in a High-Pressure Scramjet Combustor Model Analytical and Numerical Methods Subscale Combustion Chamber B10-001 Resonant Response of Mistuned Bladed B10-008 Scalar Filtered Density Function for B10-145 Laser Pulsejet with Beam Concentration Disks Including Aerodynamic Damping Effects Large Eddy Simulation of a Bunsen Burner by Multiple Reflections in a Sharp-Cone Nozzle B10-068 Direct Numerical Simulations of Transi- B10-018 Hybrid Particle-in-Cell Simulations of B10-015 Near-Plume Laser-Induced Fluores- tional/ Turbulent Wake of a Flat Plate Magnetic Sail in Laboratory Experiment cence Velocity Measurements of a Medium Power B10-149 Ejector Thrust Augmentation B10-077 Particle-Based Plasma Simulations for Hall Thruster B10-131 Acoustic Characterization of an Ethyl- an Ion Engine Discharge Chamber B10-018 Hybrid Particle-in-Cell Simulations of ene-Fueled Scramjet Combustor with a Cavity Magnetic Sail in Laboratory Experiment Flameholder Lasers and Laser Applications B10-023 Laser Ablation Propulsion Tractor Beam B10-016 Sputter Erosion Sensor for Anode System Combustion and Combustor Designs Layer-Type Hall Thrusters Using Cavity Ring- B10-119 Magnetic lon Beam Deflection in the B10-056 Performance of Ammonium-Perchlo- Down Spectroscopy Helicon Double-Layer Thruster rate-Based Composite Propellant Containing B10-072 Review: Laser-Ablation Propulsion B10-118 Effect of Anode Temperature on Hall Nanoscale Aluminum Multidisciplinary Design Optimization Thruster Performance B10-063 Linear Response of Laminar Premixed B10-144 Asymptotic Solution for the Current Flames to Flow Oscillations: Unsteady Stretch B10-011 Optiraization of System Parameters for Profile of Passive Bare Electrodynamic Tethers Effects Liquid Rocket Engines with Gas-Generator B10-116 Influencing Factors on Propulsive B10-088 Shock-Tube Experiments and Kinetic Cycles Performances of Water Droplets for Laser Modeling of Toluene Ignition Research Facilities and Instrumentation Propulsion B10-030 Combustion Dynamics and Stability ofa B10-062 Assessment of Seeder Performance for B10-143 Torsion Pendulum Investigation of Fuel-Rich Gas Generator Particle Velocimetry in a Scramjet Combustor Electromagnetic Inertia Manipulation Thrusting B10-081 Size Distribution of Particles in Com- B10-047 Three-Body Dynamics and Self-Power- bustion Products of Aluminized Composite LAUNCH VEHICLE AND ing of an Electrodynamic Tether in a Plasmasphere Propellant B10-103 Operating Radio Frequency Antennas B10-129 Separating Direct and Indirect Turbofan MISSILE TECHNOLOGY Immersed in Vacuum: Implications for Ground- Engine Combustion Noise Using the Correlation Aerodynamics Testing Plasma Thrusters Function B10-117 Development of a Magnesium and Zinc B10-033 Optimization of Secondary-Air Addi- B10-065 Reduced-Order Modeling of Two- Hall-Effect Thruster tion in a Continuous One-Dimensional Spray Dimensional’Supersonic Flows with Applications Combustor to Scramjet Inlets Airbreathing Propulsion B10-086 Theoretical Model of the Transient B10-096 Influence of Intake Orientation on B10-126 Numerical Simulation of Gaseous Combustion of Organic-Gellant-Based Gel Fuel Ramjet Performance Hydrocarbon Fuel Injection in a Hypersonic Inlet Droplets Launch Vehicle and Sounding Rocket B10-089 Particle Image Velocimetry Character- B10-087 Semi-Empirical Model for Reaction Systems ization of High-Speed Centrifugal Compressor Progress in Nanothermite Impeller—Diffuser Interaction B10-128 Effect of a Microturbine Combustor B10-051 Optimal Design of Hybrid Rocket Motors for Launchers Upper Stages B10-127 Numerically Simulated Comparative Type on Emissions at Lean-Premixed Conditions Performance of a Scramjet and Shcramjet at Propulsion and Propellant Systems Mach 11 Combustion Instability B10-053 Comparison of Catalyst Support Be- B10-002 Unsteady Blade Loading with Clocking B10-030 Combustion Dynamics and Stability of a tween Monolith and Pellet in Hydrogen Peroxide in Multistage Axial Compressors, Part | Fuel-Rich Gas Generator Thrusters B10-020 Implications of a Military Turbofan’s B10-050 Acoustic Analysis of Hybrid Rocket B10-115 Thrust Augmentation of Solid Rocket High-Pressure Turbine Erosion for Blade’s Creep Combustion Chambers Motors Using Beamed Microwave Energy Life-Consumption B10-063 Linear Response of Laminar Premixed B10-109 High-Performance Rocket Nozzle Con- B10-067 Modeling, Simulation, and Controller Flames to Flow Oscillations: Unsteady Stretch cept Design for an Air-Breathing Combustion System Effects 1334 J. PROPULSION, VOL. 26, NO. 6: 2010 INDEX B10-078 Instability Characteristics of a Gaseous- B10-016 Sputter Erosion Sensor for Anode B10-111 Assessing the Mixedness of Composite Oxygen/Methane Pentad Injector Layer-Type Hall Thrusters Using Cavity Ring- Solid Rocket Propellants Using Fluorescent B10-007 Theoretical Analysis of Dynamic Re- Down Spectroscopy Particles sponse of a Vaporizing Droplet to Acoustic B10-013 lon Thruster Grid Design Using an B10-087 Semi-Empirical Model for Reaction Oscillations Evolutionary Algorithm Progress in Nanothermite B10-081 Size Distribution of Particles in Com- B10-017 Numerical Rebuilding of SMART-1! B10-012 Closed-Vessel and Thermal Studies on bustion Products of Aluminized Composite Hall Effect Thruster Plasma Plume Triple-Base Gun Propellants Containing CL-20 Propellant B10-076 Determining Vacuum-Arc Thruster Per- B10-044 Rheological Matching of Gel Propel- B10-130 Physical Hypothesis for the Combustion formance Using a Cathode-Spot Model lants Instability in Cryogenic Liquid Rocket Engines B10-103 Operating Radio Frequency Antennas B10-086 Theoretical Model of the Transient B10-131 Acoustic Characterization of an Ethyl- Immersed in Vacuum: Implications for Ground- Combustion of Organic-Gellant-Based Gel Fuel ene-Fueled Scramjet Combustor with a Cavity Testing Plasma Thrusters Droplets Flameholder B10-117 Development of a Magnesium and Zinc B10-058 Ultrasonic Signal Denoising for Robust B10-113 Calculating an Admittance Function Hall-Effect Thruster Measurement of Solid-Propellant Burning Rates from Pulsed Tubular Grain Motor Tests B10-040 Ultrasonically Aided Electrospray Gas Turbine Engines Source for Charged Particles Approaching Detonation Monodisperse Distributions B10-063 Linear Response of Laminar Premixed B10-100 Exergy Analysis of a Hybrid Pulse Flames to Flow Oscillations: Unsteady Stretch Detonation Power Device Emissions and Noises Effects B10-027 Chemical Nonequilibrium, Heat Trans- B10-088 Shock-Tube Experiments and Kinetic B10-035 Core Noise Diagnostics of Turbofan fer, and Friction in a Detonation Tube with Modeling of Toluene Ignition Engine Noise Using Correlation and Coherence Nozzles B10-095 Film Effectiveness Measurements on the Functions Pressure Surface of a Transonic Airfoil Droplet and Spray Characterization B10-036 Emissions Characteristics of Military B10-019 High-Power Brayton Rotating Unit for B10-033 Optimizatioiu of Secondary-Air Addi- Helicopter Engines with JP-8 and Fischer- Reactor and Solar Dynamic Power Systems tion in a Continuous One-Dimensional Spray Tropsch Fuels B10-020 Implications of a Military Turbofan’s Combustor B10-128 Effect of a Microturbine Combustor High-Pressure Turbine Erosion for Blade’s Creep B10-007 Theoretical Analysis of Dynamic Re- Type on Emissions at Lean-Premixed Conditions Life-Consumption sponse of a Vaporizing Droplet to Acoustic B10-071 Blade Bowing Effect on Aerodynamic Oscillations Energy Conservation Performance of a Highly Loaded Turbine Cascade B10-136 Linear Stability Analysis of a Non- B10-048 Dynamic Simulation of aS pace Reactor B10-092 Rotating Stall Suppression in Axial Newtonian Liquid Sheet System with Closed Brayton Cycle Loops Compressors with Casing Plasma Actuation B10-135 Experimental Study of Fluid Jet Mixing B10-094 Flow Control in a Compressor Cascade at Supercritical Conditions Engine Cooling and Heat Transfer at High Incidence B10-031 Improved Spray Model for Viscous B10-052 Film Cooling in a High-Pressure B10-102 Turboprop Cycle Optimization Using Annular Sheets in a Swirl Injector Subscale Combustion Chamber Repulsive Particle Swarm Algorithm B10-116 Influencing Factors on Propulsive B10-066 Role of Tip Clearance Flow in Rotating Performances of Water Droplets for Laser Engine Performance Instabilities and Nonsynchronous Vibrations Propulsion B10-020 Implications of a Military Turbofan’s B10-039 Rotor Wake Variability in a Multistage B10-009 Theoretical and Experimental Study of High-Pressure Turbine Erosion for Blade’s Creep Compressor the Dynamics of a Liquid Swirl Injector Life-Consumption B10-086 Theoretical Model of the Transient Hybrid Rocket Engines B10-102 Turboprop Cycle Optimization Using Combustion of Organic-Gellant-Based Gel Fuel Repulsive Particle Swarm Algorithm B10-050 Acoustic Analysis of Hybrid Rocket Droplets B10-149 Ejector Thrust Augmentation Combustion Chambers B10-108 Linear Stability Analysis of a Conical B10-148 Discharge Coefficient of Expanded Exit Liquid Sheet Engine Power Cycles Holes for Film Cooling of Turbine Blades B10-132 Spray Generated by an Airblast Atom- B10-051 Optimal Design of Hybrid Rocket B10-100 Exergy Analysis of a Hybrid Pulse izer Under Elevated Ambient Pressures Motors for Launchers Upper Stages Detonation Power Device B10-080 Engineering Model for Self-Pressuriz- Electric Propulsion B10-102 Turboprop Cycle Optimization Using ing Saturated-N,O-Propellant Feed Systems B10-077 Particle-Based Plasma Simulations for Repulsive Particle Swarm Algorithm an Ion Engine Discharge Chamber Hypersonic Propulsion B10-118 Effect of Anode Temperature on Hall Fuels and Propellants, Properties of B10-126 Numerical Simulation of Gaseous Thruster Performance B10-056 Performance of Ammonium-Perchlo- Hydrocarbon Fuel Injection in a Hypersonic Inlet B10-015 Near-Plume Laser-Induced Fluores- rate-Based Composite Propellant Containing B10-127 Numerically Simulated Comparative cence Velocity Measurements of a Medium Power Nanoscale Aluminum Performance of a Scramjet and Shcramjet at Hall Thruster B10-114 Exploring the Effects of Nanostructured Mach 11 B10-046 Thomson-Scattering Diagnostics of Particles on Liquid Nitromethane Combustion B10-138 Experimental Study of Cavity-Strut Plasmas Produced in Miniature Microwave B10-133 Energy Content and Alternative Jet Fuel Combustion in Supersonic Flow Discharge Ion Engine Viability B10-064 Hybrid Reynolds-Averaged and Large- B10-041 Barium Oxide Depletion from Hollow- B10-083 Combustion of Silicon/Teflon/Viton and Eddy Simulation of Normal Injection into a Cathode Inserts: Modeling and Comparison with Aluminun/Teflon/Viton Energetic Composites Supersonic Crossflow Experiments B10-082 Microstructure Effects in Aluminized B10-139 Inlet Starting of High-Contraction B10-070 Miniature Microwave Discharge Ion Solid Rocket Propellants Axisymmetric Scramjets Thruster Driven by | Watt Microwave Power B10-081 Size Distribution of Particles in Com- B10-061 Raman Scattering Measurements of B10-119 Magnetic lon Beam Deflection in the bustion Products of Aluminized Composite Gaseous Ethylene Jets in a Mach 2 Supersonic Helicon Double-Layer Thruster Propellant Crossflow B10-146 Energy-Loss Mechanisms of a Low- B10-045 Effect of the Combined Burning-Sur- B10-021 Isolator/Combustion Chamber Interac- Discharge-Voltage Hall Thruster face/Particle Motion on Aluminum Agglomer- tions During Supersonic Combustion B10-014 Ignition and Plume Characteristics of ation B10-125 Molecular Weight and Shock-Wave Low-Current Cerium and Lanthanum Hexaboride B10-136 Linear Stability Analysis of a Non- Effects on Transverse Injection in Supersonic Hollow Cathodes Newtonian Liquid Sheet Flow 1. PROPULSION, VOL. 26, NO. 6: 2010 INDEX B10-121 Unstart Detection in a Simplified- B10-057 Simultaneous Pressure and Optical Solid Rocket Motors Geometry Hypersonic Inlet-Isolator Flow Measurements of Nanoaluminum Thermites: B10-055 Characterization of Fine Nickel-Coated B10-124 Effects of Pylon-Aided Fuel Injection on Investigating the Reaction Mechanism Powder as Potential Fuel Additive Mixing in a Supersonic Flowfield B10-076 Determining Vacuum-Arc Thruster Per- B10-056 Performance of Ammonium-Perchlo- B10-005 Supersonic Boundary-Layer Combus- formance Using a Cathode-Spot Model rate-Based Composite Propellant Containing tion: Effects of Upstream Entropy and Shear- B10-128 Effect of a Microturbine Combustor Nanoscale Aluminum Layer Thickness Type on Emissions at Lean-Premixed Conditions B10-115 Thrust Augmentation of Solid Rocket B10-040 Ultrasonically Aided slectrospray Motors Using Beamed Microwave Energy Ignition Source for Charged Particles Approaching B10-045 Effect of the Combined Burning-Sur- B10-032 Ignition Delay Time Measurements of Monodisperse Distributions face/Particle Motion on Aluminum Agglomer- Normal Alkanes and Simple Oxygenates ation Nuclear Propulsion and Power B10-055 Characterization of Fine Nickel-Coated B10-082 Microstructure Effects in Aluminized Powder as Potential Fuel Additive B10-049 Multiphysics Computational Analysis Solid Rocket Propellants of a Solid-Core Nuclear Thermal Engine Thrust B10-110 Numerical Analysis of Quasi-Steady- Laser Integration/Systems Chamber Combustion Characteristics in a Solid Rocket B10-023 Laser Ablation Propulsion Tractor Beam B10-048 Dynamic Simulation of a Space Reactor Motor System System with Closed Brayton Cycle Loops B10-111 Assessing the Mixedness of Composite Solid Rocket Propellants Using Fluorescent Ramijets and Scramjets Liquid Rocket Engines Particles B10-030 Combustion Dynamics and Stability of a B10-127_ Numerically Simulated Comparative B10-113 Calculating an Admittance Function Fuel-Rich Gas Generator Performance of a Scramjet and Shcramjet at from Pulsed Tubular Grain Motor Tests B10-052 Film Cooling in a High-Pressure Mach 11 B10-112 Model for Melt-Layer Front in Ammo- Subscale Combustion Chamber B10-122 Investigatioofn a Fluidic Shock Control nium Perchlorate Propellant Combustion Method for Hypersonic Inlets B10-022 One- and Three-Dimensional Wall Heat B10-064 Hybrid Reynolds-Averaged and Large Flux Calculations in a O,/H, System Supersonic Combustion Eddy Simulation of Normal Injection into a B10-011 Optimization of System Parameters for Supersonic Crossflow B10-021 Isolator/Combustion Chamber Interac- Liquid Rocket Engines with Gas-Generator B10-055 Characterization of Fine Nickel-Coated tions During Supersonic Combustion Cycles Powder as Potential Fuel Additive B10-043 Experimental and Numerical Studies of B10-053 Comparison of Catalyst Support Be- B10-126 Numerical Simulation of Gaseous Diamond-Shaped Injector in a Supersonic Flow tween Monolith and Pellet in Hydrogen Peroxide Hydrocarbon Fuel Injection in a Hypersonic Inlet B10-097_ Numerical Simulation of Supersonic Thrusters B10-125 Molecular Weight and Shock-Wave Nonpremixed Turbulent Combustion in a B10-134 Comparative Study of Spray Character- Effects on Transverse Injection in Supersonic Scramjet Combustor Model istics of Gas-Centered and Liquid-Centered Swirl B10-090 Hydroxyl-Tagging-Velocimetry Meas- Flow Coaxial Injectors urements of a Supersonic Flow over a Cavity B10-043 Experimental and Numerical Studies of B10-079 Heat Flux and Pressure Profiles in an Diamond-Shaped Injector in a Supersonic Flow B10-098 Numerical Study of Supersonic Com- Oxygen/Hydrogen Multielement Rocket Com- B10-067 Modeling, Simulation, and Controller bustion Processes with Central Strut Injection bustor Design for an Air-Breathing Combustion System B10-123 Numerical Investigation of the Super- B10-060 Experimental Study on Flow Transition B10-098 Numerical Study of Supersonic Com sonic Combustion of Kerosene in a Strut-Based in Dual Bell Nozzles Combustor bustion Processes with Central Strut Injection B10-010 Sidewall Boundary Layers of the B10-096 Influence of Intake Orientation on B10-124 Effects of Pylon-Aided Fuel Injection on Bidirectional Vortex Mixing in a Supersonic Flowfield Ramjet Performance B10-105 Large-Eddy Simulation of Flame-Tur- B10-065 Reduced-Order Modeling of Two B10-091 Extended Quantitative Fluorescence bulence Interactions in a Shear Coaxial Injector Dimensional Supersonic Flows with Applications Imaging for Multicomponent and Staged Injection B10-080 Engineering Model for Self-Pressuriz- into Supersonic Crossflows to Scramjet Inlets ing Saturated-N,O-Propellant Feed Systems B10-131 Acoustic Characterization of an Ethyl B10-109 High-Performance Rocket Nozzle Con- ene-Fueled Scramjet Combustor with a Cavity Turbomachinery cept Flameholder B10-069 Direct Numerical Simulations of Transi- B10-009 Theoretical and Experimental Study of B10-097 Numerical Simulation of Supersonic tional and Turbulent Flow on a Turbine Airfoil the Dynamics of a Liquid Swirl Injector Nonpremixed Turbulent Combustion in B10-037 Effects of Axial Gap on the Vane—Rotor B10-007 Theoretical Analysis of Dynamic Re- Scramjet Combustor Model Interaction in a Low Aspect Ratio Turbine Stage sponse of a Vaporizing Droplet to Acoustic B10-061 Raman Scattering Measurements of B10-038 Harmonic Balance Analysis of Blade Oscillations Gaseous Ethylene Jets in a Mach 2 Supersonic Row Interactions in a Transonic Compressor B10-054 Reduced-Order Model for H,O, Cata- Crossflow B10-141 Leading-Edge Endwall Suction and lytic Reactor Performance Analysis B10-062 Assessment of Seeder Performance for Midspan Blowing to Reduce Turbomachinery B10-108 Linear Stability Analysis of a Conical Particle Velocimetry in a Scramjet Combustor Losses Liquid Sheet B10-121 Unstart Detection in a Simplified B10-002 Unsteady Blade Loading with Clocking B10-104_ Liquid-Propellant Rocket Engine Throt- Geometry Hypersonic Inlet-Isolator Flow in Multistage Axial Compressors, Part 1 tling: A Comprehensive Review B10-124 Effectso tP ylon-Aided Fuel Injection on B10-094 Flow Control in a Compressor Cascade Mixing in a Supersonic Flowfield at High Incidence Magnetohydrodynamic Power Generation B10-093 Controlling Separation on a Simulated B10-073 Aerodynamic Heating of Reentry Body Rotating Machinery Compressor Blade Using Vortex-Generator Jets Equipped with Onboard-Surface Hall Magneto- B10-001 Resonant Response of Mistuned Bladed B10-129 Separating Direct and Indirect Turbofan hydrodynamic Generator Disks Including Aerodynamic Damping Effects Engine Combustion Noise Using the Correlation B10-089 Particle Image Velocimetry Character Function Micropropulsion and Power ization of High-Speed Centrifugal Compressor B10-071 Blade Bowing Effect on Aerodynamic B10-075 Effects of Wavy Surface Roughness on Impeller—Diffuser Interaction Performance of a Highly Loaded Turbine Cascade the Performance of Micronozzles B10-092 Rotating Stall Suppression in Axial B10-070 Miniature Microwave Discharge lon Solar Power Compressors with Casing Plasma Actuation Thruster Driven by | Watt Microwave Power B10-019 High-Power Brayton Rotating Unit for B10-001 Resonant Response of Mistuned Bladed B10-072 Review: Laser-Ablation Propulsion Reactor and Solar Dynamic Power Systems Disks Including Aerodynamic Damping Effects 1336 J. PROPULSION, VOL. 26, NO. 6: 2010 INDEX B10-107 Inclined Jet in Crossflow Interacting Spacecraft Test and Evaluation Heat Conduction with a Vortex Generator B10-103 Operating Radio Frequency Antennas B10-079 Heat Flux and Pressure Profiles in an B10-039 Rotor Wake Variability in a Multistage Immersed in Vacuum: Implications for Ground- Oxygen/Hydrogen Multielement Rocket Com- Compressor Testing Plasma Thrusters bustor B10-004 Sensitivity of Turbine Efficiency and B10-022 One- and Three-Dimensional Wall Heat Flow Structures to Varying Purge Flow STRUCTURAL MECHANICS Flux Calculations in a O,/H, System B10-068 Direct Numerical Simulations of Transi- tional/ Turbulent Wake of a Flat Plate AND MATERIALS Nonintrusive Diagnostics B10-148 Discharge Coefficient of Expanded Exit Materials Structural Properties B10-090 Hydroxyl-Tagging-Velocimetry Meas- Holes for Film Cooling of Turbine Blades urements of a Supersonic Flow over a Cavity B10-111 Assessing the Mixedness of Composite B10-066 Role of Tip Clearance Flow in Rotating B10-016 Sputter Erosion Sensor for Anode Solid Rocket Propellants Using Fluorescent Instabilities and Nonsynchronous Vibrations Layer-Type Hall Thrusters Using Cavity Ring- Particles Down Spectroscopy REAL-TIME SYSTEMS Structural Optimization Thermal Modeling and Analysis Signal Processing B10-034 Influence of Configuration on Materials B10-049 Multiphysics Computational Analysis Selection for Actively Cooled Combustors B10-058 Ultrasonic Signal Denoising for Robust of a Solid-Core Nuclear Thermal Engine Thrust Measurement of Solid-Propellant Burning Rates Chamber THERMOPHYSICS AND HEAT SPACE TECHNOLOGY TRANSFER Thermochemistry and Chemical Kinetics B10-054 Reduced-Order Model for H,O0, Cata- Spacecraft Power Computational Heat Transfer lytic Reactor Performance Analysis B10-047 Three-Body Dynamics and Self-Power- B10-022 One- and Three-Dimensional Wall Heat B10-087 Semi-Empirical Model for Reaction ing of an Electrodynamic Tether in a Plasmasphere Flux Calculations in a O,/H, System Progress in Nanothermite B10-144 Asymptotic Solution for the Current B10-049 Multiphysics Computational Analysis B10-057 Simultaneous Pressure and Optical Profile of Passive Bare Electrodynamic Tethers of a Solid-Core Nuclear Thermal Engine Thrust Measurements of Nanoaluminum Thermites: B10-074 Batteries for Venus Surface Operation Chamber Investigating the Reaction Mechanism H HM ; i . J. PROPULSION, VOL. 26, NO. 6: 2010 INDEX Author Index Abdelhafez, A., B10-026, B10-085 Cheng, Gary, B10-049 Gottfried, Dana A., B10-001 Kirchhartz, Rainer M., B10-005 Abhari, R. S., B10-004 Cheng, Meng-Dawn, B10-036 Goyne, Christopher P., B10-062 Kleijn, Chris R., B10-075 Adamovich, Igor V., B10-006 Cho, Seongho, B10-134 Grainger, Alexander L., B10-139 Klingshirn, Christopher D., Adzic, M., B10-128 Choi, Hwan-Seok, B10-030 Greenberg, J. Barry, B10-086 B10-036 Akella, M. R., B10-121 Choi, Jung-Il, B10-025 Gruber, Mark, B10-061, B10-138 Knoetze, J. H., B10-113 Alexander, Derrick, B10-127 Choi, Yoon S., B10-001 Gu, Bin, Bi0-108, B10-136 Ko, Sun-Feel, B10-058 Aly, Yasmine, B10-055 Chrigui, Mouldi, B10-132 Giilhan, Ali, B10-096 Kobayashi, Kan, B10-043 An, Sungyong, B10-053 Chun, Jaechul, B10-098 Gupta, A. K., B10-026, B10-085 Kodzwa, Paul M., B10-095 Ananthkrishnan, Narayan, B10-067 Clemens, N., B10-121 Gupta, Nitin K., B10-067 Koizumi, Hiroyuki, B10-070 Anderson, William E., B10-079 Coletti, Michele, B10-041 Gustavsson, Jonas, B10-022 Kontis, K., B10-101 Arnold, Richard, B10-052 Colombo, G., B10-082 Habiballah, Mohammed, B10-007 Kube-McDowell, Matthew T., Austin, J. M., B10-084 Corbin, Benjamin A., B10-111 Haidn, Oskar J., B10-052 B10-140 Babu, V., B10-123 Cornella, Barry, B10-115 Hall, Kenneth C., B10-038 Kumaran, K., B10-123 Babuk, V. A., B10-082 Corporan, Edwin, B10-036 Hanson, Ronald K., B10-027, Kumaran, R. Manikanda, B10-029 Baek, Seung Wook, B10-110 Cox, Wes, B10-119 B10-032, B10-088 Kunin, Alina, B10-086 Bandera, A., B10-082 Cui, Cunyan, B10-116 Hargus, William A., B10-014, Kuninaka, Hitoshi, B10-070 Banica, Marius C., B10-098 Curreli, Davide, B10-047 B10-015 Kwon, Sejin, B10-053 Barbour, Ethan A., B10-027 d’ Agostino, Luca, B10-054 Harrison, Rachel, B10-074 Lahr, Michael D., B10-090 Barhorst, T., B10-138 Dalle, Derek J., B10-065 He, Guogiang, B10-116 Laine, Robert, B10-119 Batarseh, Feras Z., B10-132 Davidson, David F., B10-032, Heidmann, J. D., B10-107 Lam, K.-Y., B10-032 Batterson, Joshua W., B10-010 B10-088 Heiser, W. H., B10-149 Landis, Geoffrey A., B10-074 Behdadnia, Robert, B10-131 Deepak, Desh, B10-081 Herrmann, Dirk, B10-096 Lara, Martin, B10-047 Behera, Prabhat Ranjan, B10-123 DeLuca, L. T., B10-082 Hideki, Nakashima, B10-046 La Torre, Federico, B10-075 Bellini, Rafaela, B10-100 deRidder, Mauritz A., B10-079 Hileman, James I., B10-133 Lawless, Patrick B., B10-039, Bharani Chandra, Kumar P., DeWitt, Matthew J., B10-036 Hiller, Sven-Juergen, B10-093 B10-089 B10-067 Divekar, C. N., B10-012 Hirota, Mitsutomo, B10-091 Lee, Jeongsub, B10-053 Siagioni, L., B10-017 Dobson, R. T., B10-076 Hodson, Howard, B10-093, B10-094 Lee, Sung Nam, B10-110 Birkan, Mitat, B10-072 Donohoo, Pearl E., B10-133 Hong, Yanji, B10-116 Li, Cheng-Hong, B10-122 Blaisdell, Gregory A., B10-140 Douglas, Zachary W., B10-090 Hong, Z., B10-032 Li, Xiugian, B10-116 Bloxham, Matthew J., B10-141 Dreizin, Edward L., B10-055 Hopkins, Mark A., B10-117 Liaw, M., B10-032 Boccaletto, Luca, B10-109 Driscoll, James F., B10-065 Horisawa, Hideyuki, B10-072 Lieuwen, Tim, B10-063 Bohn, Willy, B10-072 Dussauge, Jean-Paul, B10-109 Howison, Jason C., B10-062 Lin, Kuo-Cheng, B10-061, B10-131 Bombardelli, Claudio, B10-047, Eaton, John K., B10-095 Hsu, K.-Y., B10-138 Lippert, Thomas, B10-072 B10-144 Eckel, Hans-Albert, B10-072 Hulka, James R., B10-104 Lorenzini, Enrico C., B10-047 Bons, Jeffrey P., B10-141 Edwards, Jack R., B10-025 Hynes, Tom, B10-093, B10-094 Lu, Frank K., B10-100 Book, Carl F., B10-118 Ekici, Kivanc, B10-038 Ikegami, Shuzo, B10-091 Lun, J., B10-076 Boswell, Rod W., B10-103, B10-119 El-Genk, Mohamed S., B10-019, Im, Ji-Hyuk, B10-134 Lyrintzis, Anastasios S., B10-140 Boulkeraa, Tayeb, B10-102 B10-048 Ishikawa, Motoo, B10-073 Ma, Fuhua, B10-131 Bowersox, Rodney D. W., B10-043 Evans, A. G., B10-034 Izard, Jean-Francois, B10-097 Maddalena, Luca, B10-125 Boyce, Russell R., B10-137, Evans, Simon, B10-093, B10-094 Jackson, Kevin, B10-131 Maggi, F., B10-082 B10-139 Fang, Jie, B10-011 Jackson, Thomas A., B10-131 Mahalingam, Sudhakar, B10-077 Brahmi, Rachid, B10-053 Farnell, Cody C., B10-013 Jacobs, Peter A., B10-005 Mailach, Ronald, B10-002, B10-003 Branam, Richard D., B10-014 Fleeter, Sanford, B10-001, B10-039, Jagadeesh, G., B10-101 Majdalani, Joseph, B10-010 Burger, Scott K., B10-125 B10-089 Janhunen, Pekka, B10-042 Makela, Jason M., B10-117 Byrd, Robert E., B10-078 Foley, Timothy J., B10-083, B10-087 Jeenu, R., B10-081 Manohar, D. Raja, B10-029 Cai, Guobiao, B10-011 Forghan, Fariborz, B10-148 Jeon, Su-Kyun, B10-058 Marini, Ricardo L., B10-143 Canabal, Francisco, B10-049 Fotev, V., B10-128 Jia, Huixia, B10-002, B10-003 Marvin, Vladimir, B10-045 Candler, Graham V., B10-064 Fotia, Matthew L., B10-065 Jung, Jung Yong, B10-058 Marvina, Liubov, B10-045 Carmicino, Carmine, B10-050 Frederick, Robert A., B10-078 Jung, Taeyong, B10-112 Masquelet, Matthieu, B10-105 Carro, Rodolphe, B10-056 Fu, Qing-Fei, B10-009, B10-108, Kajimura, Yoshihiro, B10-018 Massey, Dean R., B10-117 Carter, Campbell D., B10-043, B10-136 Kappenstein, Charles, B10-053 Masuya, Goro, B10-091 B10-061, B10-090, B10-138 Fujino, Takayasu, B10-073 Katsurayama, Hiroshi, B10-145 Matuszewski, Lionel, B10-007 Casalino, Lorenzo, B10-050, Funaki, Ikkoh, B10-018 Kenjeres, Sasa, B10-075 Mauriot, Yves, B10-007 B10-051 Gabriel, Stephen B., B10-041 Kentaro, Tomita, B10-046 Mee, David J., B10-005 iCtSaia el yleL l Te Casiano, Matthew J., B10-104 Gaetani, P., B10-037 Keshav, Saurabh, B10-006 Menart, James A., B10-077 Cervone, Angelo, B10-054 Galfetti, L., B10-082 Ketsdever, Andrew, B10-115 Menon, Suresh, B10-105, B10-142 Chakraborthy, T. K., B10-012 Galian, Eugenio S., B10-143 Key, Nicole L., B10-039 Metghalchi, Hameed, B10-148 Chan, Jonathan, B10-127 Gallier, Kirk, B10-089 Kielb, Robert E., B10-038 Michaelis, Max, B10-072 Chandler, Spencer N., B10-080 Gallo, Bruno M., B10-019, B10-048 Kiichiro, Uchino, B10-046 Miles, Jeffrey Hilton, B10-035, Chang, Xin-Yu, B10-120 Ghenaiet, Adel, B10-102 Kim, Dongjun, B10-031 B10-129 Charles, Christine, B10-103, Ghosh, Santanu, B10-025 Kim, Hak-Joon, B10-058 Milivojevic, A., B10-128 B10-119 Gier, J., B10-004 Kim, In-Chul, B10-058 Moerel, Jean-Luc P.A., B10-075 Charles, Christopher S., B10-015 Gimelshein, Natalia E., B10-115 Kim, Jingon, B10-028 Moon, Insang, B10-134 Chehroudi, Bruce, B10-130 Gimelshein, Sergey F., B10-115 Kim, Kyung Moo, B10-110 Moon, Yoonwan, B10-031 Chen, Haisheng, B10-071 Givi, P., B10-008 Kim, Seong-Jin, B10-028 Mori, Koichi, B10-145 Chen, Jun, B10-011 Gongora-Orozco, N., B10-101 Kim, Seong-Ku, B10-030 Miiller, Lutz, B10-002, B10-003 Chen, Yen-Sen, B10-049 Gonthier, Keith A., B10-059 King, Lyon B., B10-117, B10-146 Mura, Arnaud, B10-097 1338 J. PROPULSION, VOL. 26, NO. 6: 2010 INDEX Naeem, Muhammad, B10-020 Rosa Sentinella, Matteo, B10-050 Song, W., B10-040 Walker, Mitchell L. R., B10-118 Nair, U. R., B10-012 Rose, M. G., B10-004 Srikant, S., B10-121 Wang, Feng, B10-136 Nakamura, Masao, B10-018 Ross, Jerry L., B10-146 Srinivasan, Ravichandra, B10-043 Wang, Jue, B10-011 Nania, F., B10-017 Rousseau, C. W., B10-113 Stalker, Raymond J., B10-005 Wang, Ten-See, B10-049 Naoji, Yamamoto, B10-046 Roy, Arnab, B10-135 Stephens, Matthew A., B10-056, Wang, Xiang-dong, B10-009 Naoto, Yamasaki, B10-046 Rubin, Binyamin, B10-016 B10-111 Wang, Yen -W., B10-126 Narusawa, Uichiro, B10-148 Ryan, Michael D., B10-043, Steyn, W. H., B10-076 Warner, Dustin J., B10-014 Natan, Benveniste, B10-044, B10-061 Strakey, Peter A., B10-008 Washeleski, Robert L., B10-117 B10-045, B10-086 Sabourin, Justin L., B10-043, Stratton, Russell W., B10-133 Weigand, Bernhard, B10-098 Nicole, Aurélie, B10-007 B10-114 Striebich, Richard, B10-036 Wen, Ming, B10-116 Nik, M. B., B10-008 Sadiki, Amsini, B10-132 Su, Wei- Yi, B10-120 Werle, M. J., B10-147 Nunami, Masanori, B10-018 Sallam, K. A., B10-106 Sullivan, Kyle, B10-057 West, Michael D., B10-103 Niirnberger-Génin, Chloé, B10-060 Sammet, Thomas E., B10-056, Sun, Bo, B10-099 Whitmore, Stephen A., B10-080 Ogawa, Hideaki, B10-139 B10-111 Sundararajan, T., B10-029 Williams, John D., B10-013, Oh, Hyun-Taek, B10-058 Sanghavi, R. R., B10-012 Sung, Hong-Gye, B10-028 B10-016 Orescanin, M. M., B10-084 Sanjurjo, Manuel, B10-047, B10-144 Suslov, Dmitry I., B10-052 Wolf, Steven, B10-056 Osnaghi, C., B10-037 Sankar, Lakshmi N., B10-142 Takahashi, Hidemi, B10-091, Xi, Guang, B10-002, B10-003 Osta, A. R., B10-106 Santosh, H., B10-063 B10-124 Yalin, Azer P., B10-016 Parimi, Venkata Sharat, B10-114 Sasoh, Akihiro, B10-072 Tan, Chunging, B10-071 Yamakawa, Hiroshi, B10-018 Park, Ik Soo, B10-067 Saunders, John D., B10-024 Tan, Hui-Jun, B10-122 Yamamoto, Atsumasa, B10-071 Pasini, Angelo, B10-054 Schall, Wolfgang, B10-072 Tao, Lei, B10-016 Yamamoto, Naoji, B10-016 Passaro, A., B10-017 Scharring, Stefan, B10-072 Teppei, Tsuru, B10-046 Yang, Li-jun, B10-009, B10-108, Pastrone, Dario, B10-050, B10-051 Scheeres, Daniel, B10-047 Thumuluru, Sai K., B10-063 B10-136 Paul, Blaise H., B10-059 Schetz, Joseph A., B10-125 Tichenor, Nathan R., B10-043 Yang, Vigor, B10-104, B10-131 Pelaez, Jesus, B10-047, B10-144 Scheuermann, Tobias, B10-098 Tong, Xiaoyan, B10-011 Yarrington, Cole D., B10-083 Peretz, Arie, B10-044 Schoenitz, Mirko, B10-055 Torre, Lucio, B10-054 Yeom, Hyo-Won, B10-028 Perren, Matthew, B10-119 Schuepbach, P., B10-004 Tournier, Jean-Michael P., B10-048 Yetter, Richard A., B10-114 Persico, G., B10-037 Segal, Corin, B10-021, B10-022, Trebs, Adam, B10-087 Yilmaz, S. L., B10-008 Petersen, Eric L., B10-056, B10-111 B10-124, B10-135 Tropea, Cam, B10-132 Yoh, Jack J., B10-112 Peterson, David M., B10-0€ Seo, Seonghyeon, B10-030 Tu, Qiuya, B10-021, B10-124 Yoo, Ji-Chang, B10-058 Phipps, Claude, B10-072 Shinohara, Iku, B10-018 Ueno, Kazuma, B10-018 Yoon, Hyun Gull, B10-067 Pinumalla, Kiran, B10-081 Shumlak, U., B10-040 Ul-Hagq, Irfan, B10-020 Yoon, Sangkyu, B10-028 Pitz, Robert W., B10-090 Sideris, Anthanasios, B10-033 Usui, Hideyuki, B10-018 Yoon, Youngbin, B10-031, B10-134 Preetham, B10-063 Sikder, A. K., B10-012 Utkin, Yurii, B10-006 Yoshino, Tomoyuki, B10-073 Prud’ homme, Roger, B10-007 Sinditskii, V. P., B10-082 Vaidyanathan, Aravind, B10-022 Zachariah, Michael, B10-057 Pudsey, Adrian S., B10-137 Singh, Amarjii, B10-012 Valdevit, L., B10-034 Zaki, Mina, B10-142 Qu, Yuan-Yuan, B10-108, B10-136 Sinko, John E., B10-023, B10-072 Valdivia, A., B10-121 Zaman, K. B. M. Q., B10-107 Raffoul, Charbel, B10-061 Sirignano, Justin A., B10-033 Vasu, Subith S., B10-088 Zare-Behtash, H., B10-101 Rahimi, Shai, B10-044 Sirignano, William A., B10-033 Vermaak, N., B10-034 Zhang, Hualiang, B10-071 Rai, Man M., B10-068, B10-069 Sislian, Jean P., B10-126, B10-127 Vicini, A., B10-017 Zhang, Kun-yuan, B10-099, Ralf, Stark, B10-060 Slater, John W., B10-024 Vo, Huu Duc, B10-066, B10-092 B10-120 Ranganath, S. C., B10-032 Smart, Michael K., B16-005 Vogeler, Konrad, B10-002, B10-003 Zhang, Yue, B10-122 Rezunkov, Yuri, B10-072 Smith, Christopher, B10-056 Von Wolfersdorf, Jens, B10-098 Zheng, Yuntao, B10-01T Rigby, D. L., B10-107 Smith, S., B10-138 Vummidi, Shashank L., B10-055 Zivkovic, M., B10-128 Rodriquez, Luis, B10-033 Sommerville, Jason D., B10-146 Wagner, J. L., B10-121 Roisman, Ilia V., B10-132 Son, Steven F., B10-083 Wakelam, Christian, B10-093, Romeo, Luca, B10-054 Song, Sung-Jin, B10-058 B10-094 J. PROPULSION, VOL. 26, NO. 6: 2010 INDEX Chronological Index B10-001 Resonant Response of Mistuned Bladed Disks Including B10-014 Ignition and Plume Characteristics of Low-Current Cerium Aerodynamic Damping Effects. Yoon S. Choi, Dana A. Gottfried, and and Lanthanum Hexaboride Hollow Cathodes. Dustin J. Warner and Sanford Fleeter, Purdue University (26, |, p. 16) Article based on AIAA Paper Richard D. Branam, Air Force Institute of Technology; and William A. 2003-4977 Hargus, U.S. Air Force Research Laboratory (26, 1, p. 130) Article based on AIAA Paper 2008-1086 B10-002 Unsteady Blade Loading with Clocking in Multistage Axial Compressors, Part 1. Huixia Jia, Zhejiang Sci-Tech University, China (PRC); B10-015 Near-Plume Laser-Induced Fluorescence Velocity Meas- Guang Xi, Xi’an Jiaotong University, China (PRC); Lutz Miiller, Ronald urements of a Medium Power Hall Thruster. William A. Hargus and Mailach, and Konrad Vogeler, Technische Universitdt Dresden, Germany (26, Christopher S. Charles, U.S. Air Force Research Laboratory (26, 1, p. 135) 1, p. 25) Article Article based on AIAA Paper 2008-5004 B10-003 Unsteady Blade Loading with Clocking in Multistage Axial B10-016 Sputter Erosion Sensor for Anode Layer-Type Hall Compressors, Part 2. Lutz Miiller, Ronald Mailach, and Konrad Vogeler, Thrusters Using Cavity Ring-Down Spectroscopy. Naoji Yamamoto, Technische Universitit Dresden, Germany; Huixia Jia, Zhejiang Sci-Tech Kyushu University, Japan; Lei Tao, Binyamin Rubin, John D. Williams, and University, China (PRC); and Guang Xi, Xi’an Jiaotong University, China Azer P. Yalin, Colorado State University (26, 1, p. 142) Article (PRC) (26, 1, p. 36) Article B10-017 Numerical Rebuilding of SMART-1 Hall Effect Thruster B10-004 Sensitivity of Turbine Efficiency and Flow Structures to Plasma Plume. A. Passaro, A. Vicini, F. Nania, and L. Biagioni, Alta, S.p.A., Varying Purge Flow. P. Schuepbach and R. S. Abhari, ETH Zurich, Italy (26, 1, p. 149) Article Switzerland; M. G. Rose, University of Stuttgart, Germany; and J. Gier, MTU Aero Engines, GmbH, Germany (26, |, p. 46) Article B10-018 Hybrid Particle-in-Cell Simulations of Magnetic Sail in Laboratory Experiment. Yoshihiro Kajimura, Kyoto University, Japan; B10-005 Supersonic Boundary-Layer Combustion: Effects of Hideyuki Usui, Kobe University, Japan; Ikkoh Funaki, Japan Aerospace Exploration Agency, Japan; Kazuma Ueno, Graduate Univefrors Aidvtanyce d Upstream Entropy and Shear-Layer Thickness. Rainer M. Kirchhartz, David J. Mee, Raymond J. Stalker, Peter A. Jacobs, and Michael K. Smart, Studies, Japan; Masanori Nunami, National Institute for Fusion Science, University of Queensland, Australia (26, 1, p. 57) Article Japan; Iku Shinohara, Japan Aerospace Exploration Agency, Japan; Masao Nakamura, Osaka Prefecture University, Japan; and Hiroshi Yamakawa, Kyoto University, Japan (26, 1, p. 159) Article B10-006 Feedback Combustion Control Using Chemi-lonization Probe in Supersonic Flow of Combustion Products. Saurabh Keshav, Yurii B10-019 High-Power Brayton Rotating Unit for Reactor and Solar Utkin, and Igor V. Adamovich, Ohio State University (26, 1, p. 67) Article Dynamic Power Systems. Mohamed S. El-Genk and Bruno M. Gallo, based on AIAA Paper 2008-1056 University of New Mexico (26, 1, p. 167) Article B10-007 Theoretical Analysis of Dynamic Response of a Vaporizing B10-020 Implications of a Military Turbofan’s High-Pressure Droplet to Acoustic Oscillations. Roger Prudhomme, Pierre et Marie Curie Turbine Erosion for Blade’s Creep Life-Consumption. Muhammad University/Centre Nationald e la Recherche Scientifique, France; Mohammed Naeem and Irfan Ul-Hagq, Institute of Space Technology, Pakistan (26, 1, Habiballah, Lionel Matuszewski, Yves Mauriot, and Aurélie Nicole, Office p. 177) Technical Note National d’ Etudes et de Recherches Aerospatiale, France (26, |, p. 74) Article B10-021 Isolator/Combustion Chamber Interactions During Super- B10-008 Scalar Filtered Density Function for Large Eddy Simulation sonic Combustion. Qiuya Tu and Corin Segal, University of Florida (26, 1, of a Bunsen Burner. S. L. Yilmaz, National Energy Technology Laboratory; p. 182) Technical Note M. B. Nik, University of Pittsburgh; P. Givi and Peter A. Strakey, National Energy Technology Laboratory (26, 1, p. 84) Article B10-022 One- and Three-Dimensional Wall Heat Flux Calculations in a O,/H, System. Aravind Vaidyanathan, Jowa State University; Jonas B10-009 Theoretical and Experimental Study of the Dynamics of a Gustavsson and Corin Segal, University of Florida (26, 1, p. 186) Technical Liquid Swirl Injector. Qing-fei Fu, Li-Jun Yang, and Xiang-Dong Wang, Note Beijing Univeorf sAeirontauytic s and AstronaChuinta i(PcRCs) ,(26 , 1, p.9 4) Article B10-023 Laser Ablation Propulsion Tractor Beam System. John E. Sinko, Global Center of Excellence (26, 1, p. 189) Technical Note B10-010 Sidewall Boundary Layers of the Bidirectional Vortex. Joshua W. Batterson and Joseph Majdalani, University of Tennessee Space B10-024 Modeling of Fixed-Exit Porous Bleed Systems for Super- Institute (26, 1, p. 102) Article based on AIAA Paper 2007-4123 sonic Inlets. John W. Slater and John D. Saunders, NASA John H. Glenn Research Center at Lewis Field (26, 2, p. 193) Article based on AIAA Paper B10-011 Optimization of System Parameters for Liquid Rocket 2008-94 CiaTRe8n e R Engines with Gas-Generator Cycles. Guobiao Cai, Jie Fang, Yuntao Zheng, and Xiaoyan Tong, Beijing University of Aeronautics and Astronautics, China B10-025 Simulation of Shock/Boundary-Layer Interactions with (PRC); Jun Chen and Jue Wang, Beijing Aerospace Propulsion Institute, Bleed Using Immersed-Boundary Methods. Santanu Ghosh, Jung-II Choi, China (PRC) (26, 1, p. 113) Article based on AIAA Paper 2005-3743 and Jack R. Edwards, North Carolina State University (26, 2, p. 203) Article based on AIAA Paper 2009-1330 B10-012 Closed-Vessel and Thermal Studies on Triple-Base Gun Propellants Containing CL-20. C. N. Divekar, R. R. Sanghavi, U. R. Nair, T. B10-026 Effect of Swirl on Shock Structure in Underexpanded K. Chakreborthy, A. K. Sikder, and Amarjit Singh, High Energy Materials Supersonic Airflow. A. Abdelhafez and A. K. Gupta, Univerofs Miartylyan d Research Laboratory, India (26, 1, p. 120) Article (26, 2, p. 215) Article B10-013 Ion Thruster Grid Design Using an Evolutionary B10-027 Chemical Nonequilibrium, Heat Transfer, and Friction in a Algorithm. Cody C. Farnell and John D. Williams, Colorado State University Detonation Tube with Nozzles. Ethan A. Barbour and Ronald K. Hanson, (26, 1, p. 125) Article Stanford University (26, 2, p. 230) Article 1340 J. PROPULSION, VOL. 26, NO. 6: 2010 INDEX B10-028 Investigation of Rocket Exhaust Diffusers for Altitude B10-044 Rheological Matching of Gel Propellants. Shai Rahimi and Simulation. Hong-Gye Sung, Hyo-Won Yeom, Sangkyu Yoon, Seong-Jin Arie Peretz, Rafael Advanced Defense Systems, Ltd., Israel; and Benveniste Kim, and Jingon Kim, Korea Aerospace University, South Korea (26, 2, Natan, /srael Institute of Technology, Israel (26, 2, p. 376) Technical Note p. 240) Article based on AIAA Paper 2008-0855 B10-045 Effect of the Combined Burning-Surface/Particle Motion on B10-029 Performance Evaluation of Second-Throat Diffuser for Aluminum Agglomeration. Vladimir Marvin, Liubov Marvina, and High-Altitude-Test Facility. R. M. Kumaran and T. Sundararajan, Indian Benveniste Natan, Technion-Israel Institute of Technology, \srael (26, 2, Institute of Technology, India; and D. R. Manohar, Indian Space Research p. 379) Technical Note Organization, India (26, 2, p. 248) Article B10-046 Thomson-Scattering Diagnostics of Plasmas Produced in B10-030 Combustion Dynamics and Stability of a Fuel-Rich Gas Miniature Microwave Discharge lon Engine. Tomita Kentaro, Yamamoto Generator. Seonghyeon Seo, Seong-Ku Kim, and Hwan-Seok Choi, Korea Naoji, Yamasaki Naoto, Tsuru Teppei, Uchino Kiichiro, and Nakashima Aerospace Research Institute, South Korea (26, 2, p. 259) Article Hideki, Kyusyu University, Japan (26, 2, p. 381) Technical Note B10-031 Improved Spray Model for Viscous Annular Sheets in a B10-047 Three-Body Dynamics ard Self-Powering of an Electro- Swirl Injector. Yoonwan Moon, Dongjun Kim, and Youngbin Yoon, Seoul dynamic Tether in a Plasmasphere. Davide Curreli and Enrico C. Lorenzini, National University, South Korea (26, 2, p. 267) Article University of Padova, Italy; Claudio Bombardelli, Manuel Sanjurjo-Rivo, and B10-032 Ignition Delay Time Measurements of Normal Alkanes and Jesus Pelaez, Universidad Politécnica de Madrid, Spain; Daniel Scheeres, Simple Oxygenates. D. F. Davidson, S. C. Ranganath, K.-Y. Lam, M. Liaw, University of Colorado at Boulder; and Martin Lara, Real Instituto y Z. Hong, and Ronald K. Hanson, Stanford University (26, 2, p. 280) Article Observatorio de la Armada en San Fernando, Spain (26, 3, p. 385) Article B10-033 Optimization of Secondary-Air Addition in a Continuous B10-048 Dynamic Simulation of a Space Reactor System with Closed One-Dimensional Spray Combustor. Justin A. Sirignano, Princeton Brayton Cycle Loops. Mohamed S. El-Genk, Jean-Michael P. Tournier, and University, Luis Rodriquez, Anthanasios Sideris, and William A. Sirignano, Bruno M. Gallo, University of New Mexico (26, 3, p. 394) Article University of California, Irvine(26, 2, p. 288) Article B10-049 Multiphysics Computational Analysis of a Solid-Core B10-034 Influence of Configuration on Materials Selection for Nuclear Thermal Engine Thrust Chamber. Ten-See Wang and Francisco Actively Cooled Combustors. N. Vermaak, University of California, Santa Canabal, NASA Marshall Space Flight Center, Yen-Sen Chen, Engineering Barbara, L. Valdevit, University of California, Irvine; and A. G. Evans, Sciences, Inc., Taiwan (ROC); and Gary Cheng, University of Alabama at University of California, Santa Barbara (26, 2, p. 295) Article Birmingham (26, 3, p. 407) Article based on AIAA Paper 2007-4144 B10-035 Core Noise Diagnostics of Turbofan Engine Noise Using B10-050 Acoustic Analysis of Hybrid Rocket Combustion Cham- Correlation and Coherence Functions. Jeffrey H. Miles, NASA John H. bers. Dario Pastrone, Lorenzo Casalino, and Matteo Rosa Sentinella, Glenn Research Center at Lewis Field (26, 2, p. 303) Article based on AIAA Politecnico di Torino, Italy; and Carmine Carmicino, Universita di Napoli Paper 2009-1237 “Federico II,” Italy (26, 3, p. 415) Article based on AIAA Paper 2007-5368 B10-036 Emissions Characteristics of Military Helicopter Engines B10-051 Optimal Design of Hybrid Rocket Motors for Launchers with JP-8 and Fischer-Tropsch Fuels. Edwin Corporan, U.S. Air Force Upper Stages. Lorenzo Casalino and Dario Pastrone, Politecnico di Torino, Research Laboratory, Matthew J. DeWitt, Christopher D. Klingshirn, and Italy (26, 3, p. 421) Article based on AIAA Paper 2008-4541 Richard Striebich, University of Dayton Research Institute; and Meng-Dawn Cheng, Oak Ridge National Laboratory (26, 2, p. 317) Article B10-052 Film Cooling in a High-Pressure Subscale Combustion B10-037 Effects of Axial Gap on the Vane—Rotor Interaction in a Chamber. Richard Amold, DLR, German Aerospace Center; Dmitry I. Low Aspect Ratio Turbine Stage. P. Gaetani, G. Persico, and C. Osnaghi, Suslov and Oskarj .H aidn, DLR, German Aerospace Center, Germany (26, 3, Politecnico di Milano, Italy (26, 2, p. 325) Article p. 428) Article based on AIAA Paper 2009-0453 B10-038 Harmonic Balance Analysis of Blade Row Interactions in a B10-053 Comparison of Catalyst Support Between Monolith and Transonic Compressor. Kivanc Ekici, University of Tennessee; Kenneth C. Pellet in Hydrogen Peroxide Thrusters. Sungyong An and Jeongsub Lee, Hall and Robert E. Kielb, Duke University (26, 2, p. 335) Article based on Korea Advanced Institute of Science and Technology, South Korea; Rachid AIAA Paper 2009-1240 Brahmi and Charles Kappenstein, University of Poitiers, France; and Sejin Kwon, Korea Advanced Institute of Science and Technology, South Korea (26, B10-039 Rotor Wake Variability in a Multistage Compressor. Nicole 3, p. 439) Article L. Key, Patrick B. Lawless, and Sanford Fleeter, Purdue University (26, 2, p. 344) Article based on AIAA Paper 2007-19 B10-054 Reduced-Order Model for H,O, Catalytic Reactor Performance Analysis. Angelo Pasini, Lucio Torre, Luca Romeo, Angelo B10-040 Ultrasonically Aided Electrospray Source for Charged Cervone, and Luca d’ Agostino, Alta, S.p.A., Italy (26, 3, p. 446) Article based Particles Approaching Monodisperse Distributions. W Song and U on AIAA Paper 08-5025 Shumlak, University of Washington (26, 2, p. 353) Article B10-055 Characterization of Fine Nickel-Coated Powder as Potential B10-041 Barium Oxide Depletion from Hollow-Cathode Inserts: Fuel Additive. Shashank L. Vummidi, Yasmine Aly, Mirko Schoenitz, and Modeling and Comparison with Experiments. Michele Coletti and Stephen Edward L. Dreizin, New Jersey Institute of Technology (26, 3, p. 454) Article B. Gabriel, University of Southampton, Great Britain (26, 2, p. 364) Article B10-042 Electrostatic Plasma Brake for Deorbiting a Satellite. Pekka B10-056 Performance of Ammonium-Perchlorate-Based Composite Janhunen, Finnish Meteorological Institute, Finland (26, 2, p. 370) Article Propellant Containing Nanoscale Aluminum. Matthew Stephens, Thomas Sammet, and Eric Petersen, Texas A&M University; Rodolphe Carro and B10-043 Experimental and Numerical Studies of Diamond-Shaped Steven Wolf, University of Central Florida; and Christopher Smith, Space Injector in a Supersonic Flow. Kan Kobayashi, Japan Aerospace Launch Corporation (26, 3, p. 461) Article based on AIAA Paper 2005-4470 Exploration Agency, Japan; Rodney D. Bowersox, Ravichandra Srinivasan, and Nathan R. Tichenor, Texas A&M University; Campbell D. Carter, U.S. Air B10-057 Simultaneous Pressure and Optical Measurements of Force Research Laboratory; and Michael D. Ryan, Universal Technology Nanoaluminum Thermites: Investigating the Reaction Mechanism. Kyle Corporation (26, 2, p. 373) Technical Note based on AIAA Paper 2009-1420 Sullivan and Michael Zachariah, University of Marylan(2d6 , 3, p. 467) Article