JOURNAL OF PROPULSION AND POWER Vol. 28, No. 6, November—December 2012 2012 Journal of Propulsion and Power Index How to Use the Index In the Subject Index, pages 1429-1433, 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 1434—1435, lists all authors associated with a given technical paper. The locating numbers are identical to those in the Subject Index. The Chronological Index, pages 1436—1440, 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 2012, that paper also will appear in both the Subject and Chronological Indexes. Authors of Comments also are listed in the Author Index. Subject Index DOI: 10.2514/1.60630 AIRCRAFT TECHNOLOGY, Flow Control COMPUTING, INFORMATION, CONVENTIONAL, SHORT/ B12-127 Surface-Flow Visuali AND COMMUNICATION VERTICAL TAKEOFF AND sure-Sensitive Paint Measurements Scale Low-Boom Inlet Autonomous Systems LANDING B12-088 Fluidic Thrust Vector ( B12-038 Autonomous Navigation System for sonic Jet Using Coflow Injectior Spacecraft Using Low-Thrust Trajectories Aerodynamics B12-079 Separation Control B12-111 Design and Analysis of a Second-Throat Part 2: High-Speed Investigations ENERGY Exhaust Diffuser for Altitude Simulation B12-027 High-Speed and High-Reynol (Alternate Fuels B12-124 Novel Oscillatory Patterns of Hyper ber Jet Control Using Localized Ar sonic Inlet Buzz Plasma Actuators B12-087 Performance Evaluation of an lodine- B12-055 Experimental Testing and Numerical B12-099 Numerical Simulation of th Vapor Hall Thruster Simulations of Shrouded Plug-Nozzle Flowfields Mesoflaps in Controlling Shock/Boundar B12-073 Ignition and Combustion of Boron B12-075 Aerodynamic Performance of Fan-Flow Interactions Nanoparticles in Ethanol Spray Flame Deflectors for Jet-Noise Reduction B12-078 Separation Control fo Rotating Machinery B12-097 Reduction of Tip Clearance Losses in an Intakes, Part 1: Low-Speed B12-081 Detached-Eddy Simulation of Rotating Unshi led Turbine by Rotor-Casing Contouring Control Strategies Stall Inception for a Full-Annulus Transonic B12-099 Numerical Simulation of the Effects of RKoott or Mesoflaps in Controlling Shock/Boundary-Layer Fuels and Fuel Systems Intera B12-072 Effects of Flow Passage FLUID DYNAMICS B12-122 Intercooled \ero-Gas-Turbine Duct Contraction on Jet-Fuel Surface Depositior 4\ erodynamics: Core Air Delivery Duct B12-071 Compressible Modeling {eroacoustics B12-105 Exchange Inlet Design for Rocket Flow in a Gas-Centered Swirl B12-027 High-Speed and High-Reynolds-Num- Based Combined-Cycle Engines Injector ber Jet Control Using Localized Arc Filament B12-024 Large-Eddy Simulation Complex B12-131 Off-Design Condition ¢ Plasma Actuators Geometry Jets Analysis of Recooling Cycle fot B12-028 Analysis of the Near Field in a Plasma- B12-029 Pulsed-Jet Ejector Thrust Augmentotr Actuator-Controlled Supersonic Jet Noise Characteristics B12-025 Some Issues in Large-Eddy Simulations B12-065 Analysis of Thrust Characteristics of a B12-024 Large-Eddy Simulatior for Chevron Nozzle Jet Flows Magnetic Sail in a Magnetized Solar Wind Geometry Jets B12-128 Thrust Measurement Boundary Layers and Heat Transfer: Aerospace Plane Hypersonic Nozzle Using an Inclined Turbulent B12-082 Investigation of High-Pressure Turbine B12-056 Rapid Analysis of Scramjet and Linear Performance Plug Nozzles Endwall Film-Cooling Performance Under Real- B12-074 Thermodynamic Gas Model Effect « istic Inlet Conditions Gas Turbine Performance Simulatior B12-008 Experimental Effects of Nozzle Geom- Air Transportation on Flow Efficiency at Low Reynolds B12-024 Large-Eddy Simulation of Complex SHORT/VERTICAL TAKEOFF AND Numbers Geometry ts LANDING AND SHORT TAKEOFF/ B12-004 Simulation of Hypersonic Shock/Turbu- VERTICAL LANDING ent Boundary-Layer Interactions Using Shock- \irframe-Propulsion Integration B12-088 Fluidic Thrust Vector Control of Unsteadiness Model B12-078 Separation Control for Aeroengine sonic Jet Using Coflow Injectior Intakes, Part 1: Low-Speed Investigation of Computational Fluid Dynamics Control Strategies Uninhabited and Unmanned Air Vehicles B12-082 Investigation of High-Pressure Turbine B12-079 Separation Control for Aeroengine B12-115 Performance of a _ Thrust-Vectoring Endwall Film-Cooling Performance Under Real- Intakes, Part 2: High-Speed Investigations Solution for Unmanned Air Vehicles istic Inlet Conditions 1429 1430 J. PROPULSION, VOL. 28, NO. 6: 2012 INDEX B12-111 Design and Analysis of aS econd-Throat B12-055 Experimental Testing and Numerical B12-030 Experimental Study on Rocket Nozzle Exhaust Diffuser for Altitude Simulation Simulations of Shrouded Plug-Nozzle Flowfields Side Load Reduction B12-126 Shock Management in Diverging Flow B12-080 Improvements in Modeling 90-Degree B12-054 Control of Operation Mode Transition in Passages by Blowing/Suction, Part 2: Applica- Bleed Holes for Supersonic Inlets Dual-Bell Nozzles with Film Cooling tons B12-127 Surface-Flow Visualization and Pres- B12-109 Jet Oscillation at Low-Altitude Oper- B12-139 Pressure and Geometry Scaling of sure-Sensitive Paint Measurements in the Large- ation Mode in Dual-Bell Nozzle Gaseous Hydrogen/Gaseous Oxygen Shear- Scale Low-Boom Inlet Shock Waves and Detonations Coaxial Injectors Bi2-128 Thrust Measurement of a Rectangular B12-080 Improvements in Modeling 90-Degree Hypersonic Nozzle Using an Inclined Baffle Plate B12-100 Mean and Turbulent Velocity Field for Bleed Holes for Supersonic Inlets B12-070 Rate-Controlled = Constrained-Equili- Jet Injected into Supersonic Flow with Pseudosh- B12-071 Compressible Modeling of the Internal brium Modeling of H/O Reacting Nozzle Flow ock Wave Flow in a Gas-Centered Swirl-Coaxial Fuel B12-134 Gas-Density Effects on Dual-Bell B12-127 Surface-Flow Visualization and Pres- Injector Transition Behavior sure-Sensitive Paint Measurements in the Large- B12-092 Optimization of Centrifugal Impellers B12-078 Separation Control for Aeroengine Scale Low-Boom Inlet for Uniform Discharge Flow and Wide Operating Intakes, Part 1: Low-Speed Investigation of B12-110 Effect of Coolant Flow Distribution on Range Control Strategies Transient Side Load of Film-Cooled Nozzles B12-125 Shock Management in Diverging Flow B12-105 Exchange Inlet Design for Rocket- Supersonic Flow Passages by Blowing/Suction, Part |: Quasi-One- Based Combined-Cycle Engines B12-100 Mean and Turbulent Velocity Field for Dimensional Theory B12-006 Vortex Generators for a Normal Shock/ Jet Injected into Supersonic Flow with Pseudosh- B12-025 Some Issues in Large-Eddy Simulations Boundary-Layer Interaction with a Downstream ock Wave for Chevron Nozzle Jet Flows Diffuser B12-070 Rate-Controlled | Constrained-Equili- B12-084 Carbon—Carbon Nozzle Erosion and B1i2-030 Experimental Study on Rocket Nozzle brium Modeling of H/O Reacting Nozzle Flow Shape-Change Effects in Full-Scale Solid-Rocket Side Load Reduction B12-111 Design and Analysis of a Second-Throat Motors B12-109 Jet Oscillation at Low-Altitude Oper- Exhaust Diffuser for Altitude Simulation B12-085 Analysis of Multivane Radiometer ation Mode in Dual-Bell Nozzle B12-008 Experimental Effects of Nozzle Geom- Arrays in High-Altitude Propulsion Jets, Wakes, and Viscid/Inviscid Flow etry on Flow Efficiency at Low Reynolds B12-028 Analysis of the Near Field in a Plasma- Actuator-Controlled Supersonic Jet Interactions Numbers B12-006 Vortex Generators for a Normal Shock/ B12-044 Enhanced Cooling of a Liquid-Fueled B12-028 Analysis of the Near Field in a Plasma- Boundary-Layer Interaction with a Downstream Rocket Thrust Chamber by Metai Foams Actuator-Controlled Supersonic Jet Diffuser B12-099 Numerical Simulation of the Effects of B12-025 Some Issues in Large-Eddy Simulations B12-003 Numerical Investigation of Lateral Jets Mesoflaps in Controlling Shock/Boundary-Layer for Chevron Nozzle Jet Flows over Body of Revolution in Supersonic Crossflow Interactions Multiphase Flows B12-009 Mecahnd aContnrol iof sCombmusti on- Transonic Flow Mode Transition in a Scramjet Engine B12-120 Cavitation Performance and Instability B12-054 Control of Operation Mode Transition in B12-004 Simulation of Hypersonic Shock/Turbu- of a Two-Bladed Inducer Dual-Bell Nozzles with Film Cooling lent Boundary-Layer Interactions Using Shock- B12-144 Stability of Confined Gas—Liquid Shear B12-082 Investigation of High-Pressure Turbine Unsteadiness Model Flows in Recessed Shear Coaxial Injectors Endwall Film-Cooling Performance Under Real- B12-003 Numerical Investigation of Lateral Jets B12-108 Atomization and Flow Characteristics of istic Inlet Conditions over Body of Revolution in Supersonic Crossflow Liquid Sheet Produced by Jet Impingement B12-071 Compressible Modeling of the Internal Unsteady Flows Hydrodynamics Flow in a Gas-Centered Swirl-Coaxial Fuel B12-121 Combined Wake and Pulsed Jet Effects Injector on Separation on a Turbine Airfoil B12-098 Study on the Suppression of Cavitation B12-110 Effect of Coolant Flow Distribution on B12-098 Study on the Suppression of Cavitation Instability in a Two-Stage Inducer Transient Side Load of Film-Cooled Nozzles Instability in a Two-Stage Inducer Plasmadynamics and Viscous Non-Boundary-Layer Flows Hypersonic Flow Magnetohydrodynamics B12-010 Estimation of Flow Properties of Gelled B12-039 Computer Simulations of Exothermic Fuels with Regard to Propulsion Systems B12-004 Simulation of Hypersonic Shock/Turbu- Propellants in a Microlaser Ablation Plasma Vortices lent Boundary-Layer Interactions Using Shock- Thruster B12-029 Pulsed-Jet Ejector Thrust Augmentor Unsteadiness Model Rarefied Flows Characteristics B12-102 Numerical Simulation of Injection Strategies in a Cavity-Based Supersonic Combus- B12-085 Analysis of Multivane Radiometer GUIDANCE, CONTROL, AND tor Arrays in High-Altitude Propulsion DYNAMICS TECHNOLOGY B12-056 Rapid Analysis of Scramjet and Linear Reacting Flows and Combustion Plug Nozzles Astrodynamics B12-129 Simple Analysis of Flame Dynamics via Flexible Convected Disturbance Models B12-143 Utilization of Residual Helium to Inlet, Nozzle, Diffuser, and Channel B12-106 Vortex Breakdown in a Swirl-Stabilized Extend Satellite Lifetimes and Mitigate Space Flows Debris Combustor B12-135 Nozzle Design Optimization for Ax B12-139 Pressure and Geometry Scaling of Optimization Techniques isymmetric Scramjets by Using Surrogate- Gaseous Hydrogen/Gaseous Oxygen Shear- B12-092 Optimization of Centrifugal Impellers Assisted Evolutionary Algorithms Coaxial Injectors for Uniform Discharge Flow and Wide Operating B12-075 Aerodynamic Performance of Fan-Flow B12-070 Rate-Controlled © Constrained-Equili- Range Deflectors for Jet-Noise Reduction brium Modeling of H/O Reacting Nozzle Flow B12-079 Separation Control for Aeroengine INTERDISCIPLINARY TOPICS Intakes, Part 2: High-Speed Investigations Separated Flows B12-110 Effect of Coolant Flow Distribution on B12-123 Separation-Control Mechanisms of Lasers and Laser Applications Transient Side Load of Film-Cooled Nozzles Steady and Pulsed Vortex-Generator Jets B12-063 Laser-Induced Fluorescence Measure- B12-056 Rapid Analysis of Scramjet and Linear B12-121 Combined Wake and Pulsed Jet Effects ments of Product Penetration Within an Ultra- Plug Nozzles on Separation on a Turbine Airfoil compact Combustor J. PROPULSION, VOL. 28, NO. 6: 2012 INDEX B12-101 Supersonic Flow over a Ramped-Wall B12-131 Off-Design Condition Cooling Capacity Combustion Instability Cavity Flame Holder with an Upstream Strut Analysis of Recooling Cycle for a Scramjet B12-091 Spontaneous Longitudinal Combustion Safety B12-132_ Rim-Rotor Rotary Ramjet Engine, Part Instability in a Continuously Variable Resonance B12-012 Ignition of Metal Powder Layers of 1: Structural Design Combustor Different Thickness by Electrostatic Discharge B12-052 Multistability and Loops-Coupled Hys- B12-138 Combustion Dynamics of Swirl Coaxial teresis: Flight-Test Analysis on Error Detection of Injectors in Fuel-Rich Combustion LAUNCH VEHICLE AND Inlet Start/Unstart B12-136 Combustion Instability-Coupling B12-105 Exchange Inlet Design for Rocket- Mechanisms Between Liquid Oxygen/Methane MISSILE TECHNOLOGY Based Combined-Cycle Engines Spray Flames and Acoustics Propulsion and Propellant Systems Bi2-125 Shock Management in Diverging Flow B12-089 Infrared Radiation and Acoustic Char- B12-141 Experimental Investigation of High- Passages by Blowing/Suction, Part |: Quasi-One- acteristics of Combustion Instabilities in Turbu- Burning-Rate Composite Solid Propellants Dimensional Theory lent Premixed Flames B12-010 Estimation of Flow Properties of Gelled B12-126 Shock Management in Diverging Flow B12-103 Combustion Instability and Flame Fuels with Regard to Propulsion Systems Passages by Blowing/Suction, Part 2: Applica- Structure of Turbulent Swirl-Stabilized Liquid- B12-083 Side-Force Amplification on an Aero- tions Fueled Combustion dynamically Thrust-Vectored Aerospike Nozzle B12-063 Laser-Induced Fluorescence Measure- B12-060 Velocity Coupling from Pulse-Test B12-014 Magnetohydrodynamic Augmentation ments of Product Penetration Within an Ultra- Firings of Pulse Detonation Rocket Engines compact Combustor B12-106 Vortex Breakdown in a Swirl-Stabilized B12-046 Effect of Surface Roughness and B12-081 Detached-Eddy Simulation of Rotating Combustor Radiation on Graphite Nozzle Erosion in Solid B12-104 Combustion Rumble Prediction with Stall Inception for a Full-Annulus Transonic Rocket Motors Integrated Computational-Fluid-Dynamics/Low- B12-044 Enhanced Cooling of a Liquid-Fueled Rotor Order-Model Methods Rocket Thrust Chamber by Metal Foams B12-102 Numerical Simulation of Injection B12-011 Analytical and Numerical Development Strategies in a Cavity-Based Supersonic Combus- of a Baffled Liquid Rocket Combustion Stability PROPULSION tor Code B12-095 Lessons Learned from an Aggressive Advanced Space Propulsion Outlet Vane Design for Axial Compressors Detonation B12-066 Thrust Evaluation of a Magnetic Sail by B12-142 Analysis of Airbreathing Hall-Effect B12-013 Gradient Mechanism of Detonation Flux-Tube Model Thrusters Initiation Under Action of High-Voltage Nano- B12-083 Side-Force Amplification on an Aero- B12-013 Gradient Mechanism of Detonation second Discharge dynamically Thrust-Vectored Aerospike Nozzle Initiation Under Action of High-Voltage Nano- B12-114 Experimental Study of a High-Fre- B12-113 Photon Laser-Induced Fluorescence of second Discharge quency Fluidic Valve Fuel Injector Neutral Xenon in a Thin Xenon Plasma B12-029 Pulsed-Jet Ejector Thrust Augmentor Droplet and Spray Characterization B12-086 Laser Ablation Propulsion Performance Characteristics of Surface-Modified Polyoxymethylene B12-021 Discharge Coefficient of Pressure-Swirl B12-042 Investigation of Short Contact Time B12-143 Utilization of Residual Helium to Atomizers with Low Nozzle Opening Coefficients Reactors for Regeneratively Cooled Hypersonic Extend Satellite Lifetimes and Mitigate Space B12-108 Atomization and Flow Characteristics of Vehicles Debris Liquid Sheet Produced by Jet Impingement B12-067 Thrust and Attitude Evaluation of B12-049 Performance Evaluation of a Ramjet B12-144 Stability of Confined Gas—Liquid Shear Magnetic Sail by Three-Dimensional Hybrid Model in a Pulse Facility at Mach 4.5 Flows in Recessed Shear Coaxial Injectors Particle-in-Cell Code Electric Propulsion B12-134 Gas-Density Effects on Dual-Bell Combustion and Combustor Designs Transition Behavior B12-062 Scaling of Efficiency with Applied B12-107 Flame Structure Measurements of Nitric B12-087 Performance Evaluation of an lodine- Magnetic Field in Magnetoplasmadynamic Vapor Hall Thruster Oxide in Hydrocarbon—Nitrous-Oxide Flames Thrusters B12-085 Analysis of Multivane Radiometer B12-138 Combustion Dynamics of Swirl Coaxial B12-113 Photon Laser-Induced Fluorescence of Arrays in High-Altitude Propulsion Injectors in Fuel-Rich Combustion Neutral Xenon in a Thin Xenon Plasma B12-014 Magnetohydrodynamic Augmentation B12-140 Modeling the Combustion of a Solid B12-143 Utilization of Residual Helium to of Pulse Detonation Rocket Engines Fuel Containing a Liquid Oxidizer Droplet Extend Satellite Lifetimes and Mitigate Space B12-065 Analysis of Thrust Characteristics of a B12-089 Infrared Radiation and Acoustic Char Debris Magnetic Sail in a Magnetized Solar Wind acteristics of Combustion Instabilities in Turbu B12-064 NASA’s Evolutionary Xenon Thruster B12-090 Deep Regulation and Reusable Rocket lent Premixed Flames Long-Duration Test Results Propulsion Using Premixed Slurry Propellant B12-103 Combustion Instability and Flame B12-067 Thrust and Attitude Evaluation of Structure of Turbulent Swirl-Stabilized Liquid- Magnetic Sail by Three-Dimensional Hybrid Airbreathing Propulsion Fueled Combustion Particle-in-Cell Code B12-103 Combustion Instability and Flame Bi2-063 Laser-Induced Fluorescence Measure- B12-112 Plume Characterization of an lon- Structure of Turbulent Swirl-Stabilized Liquid- ments of Product Penetration Within an Ultra- Focusing Hall Thruster Fueled Combustion B12-117 Simulation of Plasma Parameters Dur- compact Combustor B12-101 Supersonic Flow over a Ramped-Wall ing Hollow Cathodes Operation B12-106 Vortex Breakdown in a Swirl-Stabilized Cavity Flame Holder with an Upstream Strut B12-061 Performance of Dimethyl Ether Arcjet Combustor B12-133 Rim-Rotor Rotary Ramjet Engine, Part Thrusters and Its Dependence on Electrode B12-139 Pressure and Geometry Scaling of 2: Quasi-One-Dimensional Aerothermodynamic Configurations Gaseous Hydrogen/Gaseous Oxygen Shear- Design B12-037 Performance Evaluation of the T6 Ion Coaxial Injectors B12-080 Improvements in Modeling 90-Degree Engine Bleed Holes for Supersonic Inlets B12-021 Discharge Coefficient of Pressure-Swirl B12-116 Comparison Between Measured and B12-073 Ignition and Combustion of Boron Atomizers with Low Nozzle Opening Coefficients Predicted Field Distributions Produced by a Nanoparticles in Ethanol Spray Flame B12-018 Improved Semiempirical Correlation to Permanent Magnet B12-047 Heat Sink and Conversion of Catalytic Predict Lean Blowout Limits for Gas Turbine B12-087 Performance Evaluation of an Iodine- Steam Reforming for Hydrocarbon Fuel Combustors Vapor Hall Thruster B12-055 Experimental Testing and Numerical B12-017 Investigation of Flow Characteristics in B12-022 Fuel Selection for Pulsed Cathodic Arc Simulations of Shrouded Plug-Nozzle Flowfields Lean Direct Injection Combustors Thrusters 1432 J. PROPULSION, VOL. 28, NO. 6: 2012 INDEX B12-002 Unstable Discharge Phenomenon and B12-001 Iterative Inverse Design Method with Ramijets and Scramjets Stabilization of Hall Thruster Operating in Self- AUSM+-Up Scheme Implemented on Unstruc- B12-133 Rim-Rotor Rotary Ramjet Engine, Part Excited Mode tured Grids 2: Quasi-One-Dimensional Aerothermodynamic B12-039 Computer Simulations of Exothermic B12-016 Study of Prediction Methods for NOx Design Propellants in a Microlaser Ablation Plasma Emission from Turbofan Engines B12-135 Nozzle Design Optimization for Ax- Thruster B12-018 Improved Semiempirical Correlation to isymmetric Scramjets by Using Surrogate Predict Lean Blowout Limits for Gas Turbine Assisted Evolutionary Algorithms Emissions and Noises Combustors B12-076 Effects of Flameholder Configurations B12-016 Study of Prediction Methods for NOx on Combustion in Scramjet Engines Hybrid Rocket Engines Emission from Turbofan Engines B12-007 Isolator-Combustor Interactions in a B12-075 Aerodynamic Performance of Fan-Flow B12-137 Nonlinear Combustion and Fluid Me- Direct-Connect Ramjet-Scramjet Experiment Deflectors for Jet-Noise Reduction chanics in a Hybrid Rocket B12-050 Mixing Augmentation with Cooled Hypersonic Propulsion Pylon Injection in a Scramjet Combustor Engine Cooling and Heat Transfer B12-100 Mean and Turbulent Velocity Field for B12-093 Thermal Performance of Different B12-135 Nozzle Design Optimization for Ax- Jet Injected into Supersonic Flow with Pseudosh- Cooled Tips in a High-Pressure Turbine Cascade isymmetric Scramjets by Using Surrogate- ock Wave B12-019 Tank Heating Model for Aircraft Fuel Assisted Evolutionary Algorithms B12-130 Hysteresis Phenomenon of Mode Tran B12-102 Numerical Simulation of Injection Thermal Systems with Recirculation sition in Ramjet Engines and Its Topological Rules Strategies in a Cavity-Based Supersonic Combus- B12-044 Enhanced Cooling of a Liquid-Fueled B12-131 Off-Design Condition Cooling Capacity tor Rocket Thrust Chamber by Metal Foams Analysis of Recooling Cycle for a Scramjet B12-072 Effects of Flow Passage Expansion or B12-047 Heat Sink and Conversion of Catalytic B12-049 Performance Evaluation of a Ramjet Contraction on Jet-Fuel Surface Deposition Steam Reforming for Hydrocarbon Fuel Model in a Pulse Facility at Mach 4.5 B12-101 Supersonic Flow over a Ramped-Wall B12-145 Effectso f Flameholder Configurationo n Engine Performance Cavity Flame Holder with an Upstream Strut a Staged Supersonic Combustor B12-005 Effect of Local Flow Parameters on B12-094 Experimental and Theoretical Perform- B12-051 Study on Aeroramp Injector/Gas-Pilot Skin-Friction Coefficient in Hypersonic Air- ance of High-Pressure Hydrogen Peroxide Flame in a Supersonic Combustor breathing Engines Catalyst Beds B12-009 Mechanism and Control of Combustion B12-074 Thermodynamic Gas Model Effect on B12-007 Isolator—-Combustor Interactions in a Mode Transition in a Scramjet Engine Gas Turbine Performance Simulations Direct-Connect Ramjet-Scramjet Experiment B12-005 Effect of Local Flow Parameters on B12-037 Performance Evaluation of the T6 lon B12-051 Study on Aeroramp Injector/Gas-Pilot Skin-Friction Coefficient in Hypersonic Air Flame in a Supersonic Combustor Engine breathing Engines Ignition B12-042 Investigation of Short Contact Time Fuels and Propellants, Properties of B12-012 Ignition of Metal Powder Layers of Reactors for Regeneratively Cooled Hypersonic B12-140 Modeling the Combustion of a Solid Different Thickness by Electrostatic Discharge Vehicles Fuel Containing a Liquid Oxidizer Droplet B12-048 Spatial Development and Temperature B12-069 Comparison of Flammability Character Rotating Machinery of Spark Kernels Exiting into Quiescent Air istics of Paraffin Mixtures and Polyethylene B12-086 Laser Ablation Propulsion Performance B12-001 Iterative Inverse Design Method with B12-090 Deep Regulation and Reusable Rocket of Surface-Modified Polyoxymethylene AUSM+-Up Scheme Implemented on Unstruc- Propulsion Using Premixed Slurry Propellant tured Grids B12-010 Estimation of Flow Properties of Gelled Liquid Rocket Engines B12-098 Study on the Suppression of Cavitation Fuels with Regard to Propulsion Systems B12-059 Experimental Study Swirl Injector Instability in a Two-Stage Inducer B12-072 Effects of Flow Passage Expansion or Dynamic Response Using a Hydromechanical B12-!20 Cavitation Performance and Instability Contraction on Jet-Fuel Surface Deposition Pulsator of a Two-Bladed Inducer B12-012 Ignition of Metal Powder Layers of B12-138 Combustion Dynamics of Swirl Coaxial Different Thickness by Electrostatic Discharge Injectors in Fuel-Rich Combustion Solar Power B12-060 Velocity Coupling from Pulse-Test B12-030 Experimental Study on Rocket Nozzle B12-065 Analysis of Thrust Characteristics of a Firings Side Load Reduction Magnetic Sail in a Magnetized Solar Wind B12-020 Study on Combustion Characteristics B12-054 Control of Operation Mode Transition in and Performance of HTPB/AP Propellants Solid Rocket Motors Dual-Bell Nozzles with Film Cooling Containing Zirconium B12-109 Jet Oscillation at Low-Altitude Oper- B12-141 Experimental Investigation of High B12-022 Fuel Selection for Pulsed Cathodic Arc ation Mode in Dual-Bell Nozzle Burning-Rate Composite Solid Propellants Thrusters B12-011 Analytical and Numerical Development B12-084 Carbon—Carbon Nozzle Erosion and of a Baffled Liquid Rocket Combustion Stability Shape-Change Effects in Full-Scale Solid-Rocket Gas Turbine Engines Code Motors B12-073 Ignition and Combustion of Boron B12-040 Fabrication of Catalyst-Insertion-Type B12-022 Fuel Selection for Pulsed Cathodic Arc Nanoparticles in Ethanol Spray Flame Microelectromechanical Systems Monopropel Thrusters B12-121 Combined Wake and Pulsed Jet Effects lant Thruster B12-046 Effect of Surface Roughness and on Separation on a Turbine Airfoil B12-032, Dynamic Characteristics of Simplex Radiation on Graphite Nozzle Erosion in Solid B12-093 Thermal Performance of Different Swirl Injector in Low Frequency Range Rocket Motors Cooled Tips in a High-Pressure Turbine Cascade B12-060 Velocity Coupling from Pulse-Test B12-125 Shock Management in Diverging Flow Magnetohydrodynamic Power Generation Firings Passages by Blowing/Suction, Part |: Quasi-One- B12-014 Magnetohydrodynamic Augmentation Dimensional Theory of Pulse Detonation Rocket Engines Supersonic Combustion B12-122 Intercooled Aero-Gas-Turbine Duct B12-076 Effects of Flameholder Configurations Aerodynamics: Core Air Delivery Ducts Micro Propulsion and Power on Combustion in Scramjet Engines B12-017 Investigation of Flow Characteristics in B12-008 Experimental Effects of Nozzle Geom- B12-007 Isolator-Combustor Interactions in a Lean Direct Injection Combustors etry on Flow Efficiency at Low Reynolds Direct-Connect Ramjet-Scramjet Experiment B12-074 Thermodynamic Gas Model Effect on Numbers B12-047 Heat Sink and Conversion of Catalytic Gas Turbine Performance Simulations B12-040 Fabrication of Catalyst-Insertion-Type Steam Reforming for Hydrocarbon Fuel B12-115 Performance of a Thrust-Vectoring Microelectromechanical Systems Monopropel B12-009 Mechanandi Csonmtro l of Combustion- Solution for Unmanned Air Vehicles lant Thruster Mode Transition in a Scramjet Engine J. PROPULSION, VOL. 28, NO. 6: 2012 INDEX B12-005 Effect of Local Flow Parameters on SPACE TECHNOLOGY Computational Heat Transfer Skin-Friction Coefficient in Hypersonic Air- B12-046 Effect of Surface Roughness and breathing Engines Landers Radiation on Graphite Nozzle Erosion in Solid B12-145 Effects of Flameholder Configuration on B12-083 Side-Force Amplification on an Aero- Rocket Motors a Staged Supersonic Combustor dynamically Thrust-Vectored Aerospike Nozzle Forced Convection Turbomachinery STRUCTURAL MECHANICS B1i2-015 Large-Eddy Simulation of Film Cooling B12-133 Rim-Rotor Rotary Ramjet Engine, Part AND MATERIALS with Internal Coolant Crossflow Effects 2: Quasi-One-Dimensional Aerothermodynamic Structural Design Nonintrusive Diagnostics Design B12-096 Penny Gap Effect on Performance and B12-132 Rim-Rotor Rotary Ramjet Engine, Part B12-048 Spatial Development and Temperature Secondary Flowfield in a Compressor Cascade 1: Structural Design of Spark Kernels Exiting into Quiescent Air B12-097 Reduction of Tip Clearance Losses in an Structural Durability (Including Fatigue, B12-113 Photon Laser-Induced Fluorescence of Unshrouded Turbine by Rotor-Casing Contouring Fracture, and Environmental Neutral Xenon in a Thin Xenon Plasma B12-132 Rim-Rotor Rotary Ramjet Engine, Part Degradation) Radiation in Participating Media 1: Structural Design B12-119 Determination of Turbine Blade Life B12-048 Spatial Development and Temperature B12-057 Squealer Geometry Effects on Aero- from Engine Field Data of Spark Kernels Exiting into Quiescent Air thermal Performance of Tip-Leakage Flow of B12-089 Infrared Radiation and Acoustic Char- Cavity Tips THERMOPHYSICS AND HEAT acteristics of Combustion Instabilities in Turbu- B12-093 Thermal Performance of Different TRANSFER lent Premixed Flames Cooled Tips in a High-Pressure Turbine Cascade B12-123 Separation-Control Mechanisms _ of Ablation, Pyrolysis, Thermal Thermal Control Steady and Pulsed Vortex-Generator Jets Decomposition and Degradation B12-019 Tank Heating Model for Aircraft Fuel B12-120 Cavitation Performance and Instability B12-084 Carbon—Carbon Nozzle Erosion and Thermal Systems with Recirculation of a Two-Bladed Inducer Shape-Change Effects in Full-Scale Solid-Rocket B12-001 Iterative Inverse Design Method with Motors Thermal Modeling and Analysis \USM+-Up Scheme Implemented on Unstruc- B12-019 Tank Heating Model for Aircraft Fuel tured Grids Aerothermodynamics/Thermal Protection Thermal Systems with Recirculation B12-095 Lessons Learned from an Aggressive B12-057 Squealer Geometry Effects on Aero Outlet Vane Design for Axia! Compressors thermal Performance of Tip-Leakage Flow of Thermochemistry and Chemical Kinetics B12-092 Optimization of Centrifugal Impellers Cavity Tips B12-042 Investigation of Short Contact Time niform Discharge Flow and Wide Operating B12-015 Large-Eddy Simulation of Film Reactors for Regeneratively Cooled Hypersonic with Internal Coolant Crossflow Effects Vehicles JOURNAL OF PROPULSION AND POWER Vol. 28, No. 6, November—December 2012 2012 Author Index DOI: 10.2514/1.60631 Abdelhafez, A., B11-010 Chung, Yunjae, B12-032 Gimelshein, Sergey F., B12-085 Karagozian, Ann, B12-014 Adamovich, Igor V., B11-046 Ciezki, Helmut K., B12-010 Godke, Chaitanya, B12-101 Karmakar, Srinibas, B12-073 Adams, Nikolaus A., B11-001 Cole, Lord K., B12-014 Goebel, Dan M., B12-035, B12-037 Kearney-Fischer, M., B12-027 Ahn, Kyubok, B11-062, B11-090 Collado, Elena, B12-043 Gong, Jingsong, B12-047 Keidar, Michael, B12-142 Acharya, Sumanta, B12-073 Conners, Timothy R., B12-055 Gord, James R., B12-063 Ketsdever, Andrew D., B12-085 Adolfo, Reggiori, B12-049 Corke, Thomas C., B12-053 Gore, Jay P., B12-089 Key, Nicole, B12-095 Ahn, Benjamin, B12-059 Cornella, Barry M., B12-085 Goss, Larry, B12-048 Khil, Taeock, B12-032 Ahn, Kyubok, B12-138 Costa, Fernando S., B12-069 Gottschall, Marcel, B12-096 Kiel, Barry V., B12-048, B12-089 Alkislar, Mehmet B., B12-029 Courtiade, Nicholas, B12-118 Gourdain, Nicolas, B12-043, Kim, J.-H., B12-027 An, Chongwei, B12-045 Cui, Jinsheng, B12-003 B12-118 Kim, Jeonglae, B12-026 Anderson, William E., B12-091, Cui, Tao, B12-052, B12-130 Grady, Nathan, B12-101 Kimura, Tatsuya, B12-054, B12-109 B12-094 Cui, Y. D., B12-003 Groening, S., B12-136 Kirkpatrick, Allan T., B12-011 Araka, Kasumi, B12-109 Dalle, Derek, B12-056 Guha, Abhijit, B12-016 Knapp, B., B12-136 Araki, Mikiya, B12-128 Daminelli, Giambattista, B12-049 Guidos, Mike, B12-110 Knoetze, J. H., B12-060 Ashida, Yasumasa, B12-066 Danczyk, Stephen, B12-071 Guo, Xiaode, B12-045 Koga, Hidekazu, B12-054 Auweter-Kurtz, Monika, B12-113 Dang, Thong Q., B12-125, B12-126 Gurovich, V., B12-117 Koichi, Yonezawa, B12-109 Babinsky, Holger, B12-006 DeBenedictis, Erika, B12-038 Gutmark, Ephraim, B12-106 Kojima, Hirotsogu, B12-066 Bai, Mo, B12-044 Denman, Paul A., B12-122 Han, Ke, B12-002 Kojima, Takayuki, B12-128 Balcazar, Thania S., B12-114 Denninger, Marc, B12-132 He, Xuegang, B12-052 Kostka, Stanislav, B12-063 Bao, Wen, B12-124, B12-131 Dewanji, D., B12-017 Heister, Stephen D., B12-059, Kouchi, Toshinori, B12-009 Baoxi, Wei, B12-051 Ding, Yongjie, B12-002 B12-094, B12-141 Krasik, Y. E., B12-117 Bazarov, Vladimir G., B12-032 Dooley, Kerry M., B12-073 Hendricks, Robert C., B12-119 Krothapalli, Anjaneyulu, B12-029 Beloni, Ervin, B12-012 Dowling, A. P., B12-104 Heo, Jun-Young, B12-088 Kudo, Kenji, B12-005 Benel, Gabriel, B12-042 Dreizin, Edward L., B12-012 Herges, Thomas G., B12-127 Kwon, Sejin, B12-040, B12-145 Beppu, Shinji, B12-061 Drela, Mark, B12-008 Herman, Daniel, B12-064 Lakusta, Patrick J., B12-063 Bianchi, Daniele, B12-084 Driscoll, James F., B12-007, Hillier, Adam, B12-087 Lee, Changjin, B12-137 Bilek, M.M.M., B12-022 B12-056 Himeno, Takehiro, B12-108 ee, Jeongsub, B12-040 Binder, Nicolas, B12-115 Duan, Yan Juan, B12-131 Hinerman, Timothy D., B12-011 Lee, Ji Hyung, B12-111 Bland, R.A., B12-094 Dutton, J. Craig, B12-127 Hodson, Howard P., B12-057, Lee, Kyoung-Hoon, B12-098, Blunck, David L., B12-048, B12-089 Eastwood, Simon, B12-024 B12-078, B12-079, B12-093, B12-120 Bodony, Daniel J., B12-026 Ebrahimi, Houshang, B12-102 B12-123 I ee, Kyungjae, B12-145 Bombardelli, Claudio, B12-068 Edwards, Jack R., B12-099 Hofer, Richard R., B12-035, Lee, Sang-Hyeon, B12-050 Bondarenko, Sergiy G., B12-090 Eichhorn, Christoph, B12-113 B12-037 Lee, Soo Yong, B12-021 Boyce, Russell R., B12-135 Eilers, Shannon D., B12-083 Hong, Moongeun, B12-021 Lee, Yang Gi, B12-076 Branam, Richard D., B12-063, Elliott, Gregory S., B12-127 Hou, Lingyun, B12-047 Lee, Yangji, B12-145 B12-087 Ervin, Jamie, B12-072 Hsu, Kuang- Yu, B12-101 Leiter, Hans, B12-113 Braun, Eric, B12-114 Etele, J., B12-105 Hu, Bin, B12-018 Leiter, Randy, B12-008 Bray, K.N. C., B12-104 Evans, Simon W., B12-078, Huang, Yong, B12-018 Lev, Dan R., B12-062 Bridges, James, B12-023 B12-079, B12-123 Hubble, Aimee, B12-116 Leylegian, John, B12-042 Brouillette, Martin, B12-133 Farahani, Mohammad, B12-077 Huffmann, Richard E., B12-087 Li, Fengsheng, B12-045 Bruccoleri, Alexander, B12-008 Fasoulas, Stefanos, B12-113 Huo, Hongfa, B12-139 Li, Jun-wei, B12-031 ai, Guobiao, B12-139 Ferguson, Donald, B12-129 Hussaini, M. Youssuff, B12-025 Lian, Chenzhou, B12-058 ‘ambier, Jean-Luc, B12-014 Foster, John E., B12-116 Hynes, Tom P., B12-078, B12-079 Lightfoot, Malissa, B12-071 arbonneau, Xavier, B12-115 Fotia, Matthew L., B12-007 lim, Hongsik, B12-081 Lim, Jihwan, B12-111 arrotte, Jon F., B12-122 Freund, Jonathan B., B12-026 Inoue, Chihiro, B12-108 Lin, Jeff, B12-110 ‘arter, Campbell D., B12-101 Fritzsche, Stephan, B12-113 Ismailov, Maksud, B12-059 Litt, Jonathan S., B12-119 ‘asalino, Lorenzo, B12-041 Fu, Qing-fei, B12-144 Ivanchenko, Anatoliy M., B12-090 Liu, F., B12-075 “astaldi, Marco J., B12-042 Fulayter, Roy D., B12-095 Jackson, Anthony, B12-074 Lock, Gary, B12-093 ‘erantola, D.J., B12-105 Funaki, Ikkoh, B12-065, B12-066, Jameson, Kristina K., B12-035 Lohle, Stefan, B12-113 ha, Bongjun, B12-145 B12-067 Janbozorgi, Mohammad, B12-070 Loth, Eric, B12-006 ‘handrasekaran, N., B12-016 Gaitonde, Datta V., B12-028, Jeon, Jaehyoung, B12-021 Lozano, Paulo, B12-008 ‘hanez, Philippe, B12-078, B12-079 Bi2-102 Ji, Yanchao, B12-002 Lu, Frank K., B12-114 ‘hang, Juntao, B12-124 Gallar, Luis, B12-074 Jia, Zhen, B12-047 Lynch, Amy, B12-048 ‘hen, Jihua, B12-132 Ganesh, S., B12-001 Jiang, Hua, B12-072 Madhav, Ajay, B12-091 ‘hen, Xiang-Ying, B12-081 Gany, Alon, B12-140 Jiang, Pei-Xue, B12-015 Madlener, Klaus, B12-010 heng, Gary C., B12-110 Gao, Jie, B12-097 Jonsson, Magnus, B12-082 Maiguma, Muneyuki, B12-061 ‘hinitz, Wallace, B12-042 Gao, Yuan, B12-104 Kajimura, Yoshihiro, B12-066, Mailach, R., B12-096 hoi, Byungil, B12-076, B12-145 Garrigues, L., B12-034 B12-067 Malo-Molina, Faure J., B12-102 ~PRFAFAAAARA F‘AAAhRAo iRAAA, AHwLanA- Seok, B12-138 Gemaque, Marcos J. A., B12-069 Kakami, Akira, B12-061 Manship, Timothy D., B12-141 Choi, Jang-Woon, B12-098, B12-120 Genin, Chloe, B12-030 Kang, Sang Hun, B12-076, B12-145 Martelli, Francesco, B12-082 Choi, Yung-Il, B12-099 German, Brian J., B12-019 Kang, Shin-Hyung, B12-098, Martin, Christopher, B12-129 Choueiri, Edgar, B12-062 Ghosh, Santanu, B12-099 B12-120 Masuya, Goro, B12-009 Choutapalli, Isaac, B12-029 Gicquel, Laurent Y. M., B12-043 Kao, Kanenori, B12-005 Matsumoto, Masaharu, B12-067 Chung, J. N., B12-044 Gimelshein, Natalia E., B12-085 Kapilavai, Dheeraj, B12-055 McKenzie, D.R., B12-022 J. PROPULSION, VOL 28, NO. 6: 2012 INDEX Menon, Suresh, B12-101 Prasad, B.V.S.S., B12-001 Su-Kyum, Kim, B12-040 Williams, Rayon A., B12-012 Merkle, Charles L., B12-055, Proschanka, Dzianis, B12-054, Sullivan, John, B12-055 Wilson, Donald R., B12-114 B12-058 B12-109 Sung, Hong-gye, B12-088 Wilson, Matthew D., B12-083 Metgalchi, Hameed, B12-070 Protsan, Yulian, B12-090 Szabo, James, B12-087 Wilson, Shaun A., B12-090 Meyer, S. E., B12-094 Qin, Jiang, B12-124, B12-131 Tachibana, Takeshi, B12-061 Xhou, Yifan, B12-047 Milano, Dan, B12-011 Quinlan, John Matthew, B12-011 Taguchi, Hideyuki, B12-128 Xia, Guoping, B12-058 Miller, Kyle L., B12-095 Rakitin, Alexsandr E., B12-013 Tang, Shunlin, B12-052, B12-130 Xia, Hao, B12-024 Min, Byoung-Sun, B12-020 Ranalli, Joseph, B12-129 Tapee, John, B12-055 Xie, Fa, B12-018 Minglei, Yan, B12-051 Rancourt, David, B12-132, B12-133 Thakre, Piyush, B12-046 Xinxing, Shi, B12-051 Mitani, Tohru, B12-009 Rankin, Brent A., B12-089 Thompson, Richard, B12-039 Xiong, J., B12-075 Mitchell, Charles E., B12-011 Rao, A. G., B12-017 Tomioka, Sadatake, B12-005, Xu, Kunning, B12-112 Mizrahi, J., B12-117 Regunath, Gavita S., B12-122 B12-009 Xu, Xu, B12-051 Moeller, Trevor Michael, B12-039 Renfro, Michael W., B12-063 Torrez, Sean M., B12-056 Xue, Wei, B12-124 Monfort, Jeff, B12-089 Riva, Giulio, B12-049 Trask, Nathaniel, B12-071 Yamakawa, Hiroshi, B12-066, Morris, Scott C., B12-053 Robin, Mike, B12-087 Tsujimoto, Yoshinobu, B12-054, B12-067 Murakamo, Atsuo, Bi2-005 Rosen, Stanford, B12-091 B1i2-109 Yamamoto, M., B12-036 Na, Yang, B12-137 Roth, Timothy, B12-014 Tsukamoto, Masahiro, B12-128 Yamasaki, Hiroyuki, B12-005 Nakamoto, S., B12-036 Rousseau, C. W., B12-060 Tsukuda, Hiroaki, B12-109 Yang, Lijun, B12-144 Nasuti, Francesco, B12-084 Rovey, Joshua L., B12-033 Tsuru, Taira, B12-005 Yang, Soo Seok, B12-076, B12-145 Neumannn, P.R.C., B12-022 Roy, Sukesh, B12-063 Tucker, Paul G., B12-024 Yang, Vigor, B12-046 Nishida, Hiroyuki, B12-065 Ruf, Joe, B12-110 Umeh, Chukwueloka O.1 Yang, Yang, B12-051 Nishino, S., B12-036 Rusak, Zvi, B12-106 B12-106 Yao, Zhaopu, B12-104 Niu, Jun, B12-124 Russell, Ryan P., B12-143 Usui, Hideyuki, B12-067 Yasaka, Yasuyosho, B12-036 O'Neil, Patrick T., B12-141 Rybalko, Michael, B12-006 Uzun, Ali, B12-025 Yi, Tongxun, B12-103 Ogawa, Hideaki, B12-135 Salussolia, Martino, B12-074 van Buijitenen, J. P., B12-017 Yokota, Kazuhiko, B12-054, Ogita, Naoya, B12-086 Salvadori, Simone, B12-082 Van Ness, Daniel, B12-053 B12-109 Ott, Peter, B12-082 Samimy, M., B12-027 Van Noord, Jonathan L., B12-064 Yonezawa, Koichi, B12-054 Ottanelli, Luca, B12-082 Santavicca, Domenic, B12-103 Vekselman, V., B12-117 Yoon, Woong-Sup, B12-111 Ottavy, Xavier, B12-118 Sarimurat, Mehmet, B12-125, Verma, S. B., B12-134 Yoon, Youngbin, B12-032 Pachidis, Vassilios, B12-074 B12-126 Vogeler, K., B12-096 Yousefpour, Ali, B12-132 Paintal, Surjeet, B12-087 Sasoh, Akihoro, B12-086 Volino, Ralph, B12-121 Yu, Daren, B12-002, B12-052, Papamoschou, D., B12-075 Schmidt, David P., B12-071 Volpe, Valentino, B12-074 B12-130, B12-131 Papas, Paul, B12-107 Shiga, Seiichi, B12-128 Wakelam, Christian T., B12-078, Yu, Guogiang, B12-097 Park, Byung Hoon, B12-111 Shikida, MItsuhiro, B12-086 B12-079 Yu, Yen, B12-091 Park, Sunghyun, B12-111 Shin, Kyoung-hoon, B12-137 Walker, Alastair, B12-122 Zabarnick, Steven, B12-072 Pasha, Amjad A., B12-004 Shinohara, Iku, B12-067 Walker, Mitchell L. R., B12-112, Zeineh, Christopher F., B12-014 Pastrone, Dario, B12-041 Simpson, Huw, B12-037 B12-143 Zha, Gecheng, B12-081 Patterson, Michael J., B12-064 Singh, Lake, B12-143 Wallace, Neil C., B12-037 Zhang, Chao, B12-130 Pekker, Leonid, B12-142 Sinha, Krishnendu, B12-004 Wang, Fang, B12-018 Zhang, Chuhua, B12-092, B12-100, elosi, Avishag, B12-140 Sinko, John E., B12-086 Wang, Jingyu, B12-045 B12-146, B12-147, B12-148 Peng, Wei, B12-015 Sisco, James C., B12-091 Wang, Lei, B12-124 Zhang, Gouzhou, B12-139 Peterson, Zachary W., B12-083 Slater, John, B12-080 Wang, Ning-fei, B12-031 Zhang, Jun-Mei, B12-003 Piao, Ying, B12-047 Sliphorst, M., B12-136 Wang, Ten-See, B12-110 Zhang, Qiao, B12-031 Picard, Mathieu, B12-132, B12-133 Snyder, John, B12-037 ang, Xiaowei, B12-139 Zhang, Silong, B12-131 Pitz, Robert W., B12-101 Soditus, Sherry M., B12-119 atanabe, Toshinori, B12-108 Zheng, Qun, B12-097 Plante, Jean-Sebastian, B12-132, Soltani, Mohammad Reza, B12-077 aung, T., B12-105 Zhou, Chao, B12-057, B12-093 B12-133 Soo Hyun, Hyung, B12-020 ayman, Thomas R., B12-055 Zhou, Weixing, B12-131 Polk, James E., B12-037 Sou, Hua-Shu, B12-003 Wei, Liqui, B12-002 Zhu, Min, B12-104 Pote, Bruce, B12-087 Soulas, George C., B12-064 Wei, Zhi-jun, B12-031 Zidar, David G. B12-033 Pourpoint, Timothee, B12-094 Starikovskiy, Andrew, B12-013 Wernet, Mark P., B12-023 Pourquie, M., B12-017 Stark, Ralf, B12-030, B12-134 West, Zachary, B12-072 Powell, Orval, B12-107 Su, Wan-Xing, B12-031 Whitmore, Stephen A., B12-083 JOURNAL OF PROPULSION AND POWER Vol. 28, No. 6, November—December 2012 2012 Chronological Index DOI: 10.2514/1.60632 B12-001 Iterative Inverse Design Method with AUSM+-Up Scheme B12-014 Magnetohydrodynamic Augmentation of Pulse Detonation Implemented on Unstructured Grids. S. Ganesh, /ndian Institute of Rocket Engines. Christopher F. Zeineh, Lord K. Cole, Timothy Roth, and Technoloyg, India: and B. V. S. S. Prasad, Indian Institute of Technology, India Ann Karagozian, University of California, Los Angeles; and Jean-Luc (28, 1, p. 16) Article Cambier, U.S. Air Force Research Laboratory (28, |, p. 146) Article B12-002 Unstable Discharge Phenomenon and Stabilization of Hall B12-015 Large-Eddy Simulation of Film Cooling with Internal Thruster Operating in Self-Excited Mode. Ke Han, Liqui Wei, Yongjie Coolant Crossflow Effects. Wei Peng and Pei-Xue Jians Tsinghua Ding, YanchaoJi , and Daren Yu, Harbin Institute of Technology, China (PRC) University, China (PRC) (28, |, p. 160) Article (28, 1, p. 27) Article B12-016 Study of Prediction Methods for NOx Emission from B12-003 Numerical Investigation of Lateral Jets over Body of Turbofan Engines. N. Chandrasekaran and Abhijit Guha, /ndian Institute of Revolution in Supersonic Crossflow. Jun-Mei Zhang, Y.D. Cui, and Technology, India (28, 1, p. 170) Article Jinsheng Cui, National University of Singapore, Singapore (ROS); and Hua- Shu Sou, Zhejiang Sci-Tech University, China (PRC) (28, |, p. 33) Article B12-017 Investigation of Flow Characteristics in Lean Direct Injection Combustors. D. Dewanji, A. G. Rao, M. Pourquie, and J. P van B12-004 Simulation of Hypersonic Shock/Turbulent Boundary- Buijitenen, Delft University of Techn The Netherlands (28, 1, p. 181) Layer Interactions Using Shock-Unsteadiness Model. Amjad A. Pasha and Article Krishnendu Sinha, /ndian Institute of Technology, India (28, |, p. 46) Article B12-018 Improved Semiempirical Correlation to Predict Lean B12-005 Effect of Local Flow Parameters on Skin-Friction Blowout Limits for Gas Turbine Combustors. Fa Xie, Yong Huan Bin Hu Coefficient in Hypersonic Airbreathing Engines. Taira Tsuru, Tokyo and Fang Wang, Beihang University, China (PRC) (28, |, p. 197) Article Institute of Technology, Japan; Sadatake Tomicka, Kenji Kudo, Atsuo Murakamo, and Kanenori Kao, Japan Aerospace Exploration Agency, Japan; B12-019 Tank Heating Model for Aircraft Fuel Thermal Systems and Hiroyuki Yamasaki, Tokyo Institute of Technology, Japan (28, 1, p. 61) with Recirculation. Brian J. German, Georgia Institute of Te gy (28, | Article p. 204) Article B12-006 Vortex Generators for a Normal Shock/Boundary-Layer B12-020 Study on Combustion Characteristics and Performance of Interaction with a Downstream Diffuser. Michae! Rybalko, University of HTPB/AP Propellants Containing Zirconium. Byoung-Sun Min and Illinois at Urbana-Champaign, Holger Babinsky, University of Cambridge, Hyung Soo Hyun, Agency for Defense De ynent, Korea (ROK) (28, |, p Great Britain; and Eric Loth, University of Virginia (28, 1, p. 71) Article 211) Technical Note B12-007 Isolator—-Combustor Interactions in a _ Direct-Connect B12-021 Discharge Coefficient of Pressure-Swirl Atomizers with Ramjet-Scramjet Experiment. Matthew | Fotia and James F. Driscoll, Low Nozzle Opening Coefficients. Moong Hong, Jaehyoung Jeon, and University of Michigan (28, 1, p. 83) Article Soo Yong Lee, Korea Aerospace Research Institute, Korea (ROK) (28, 1, p 213) Technical Note B12-008 Experimental Effects of Nozzle Geometry on Flow Efficiency at Low Reynolds Numbers. Alexander Bruccoleri, Randy Leiter, B12-022 Fuel Selection for Pulsed Cathodic Arc Thrusters. P. R. ¢ Mark Drela, and Paulo Lozano, Massachusetts Institute of Technology (28, |, Neumannn, M. M. M. Bilek, and D. R. McKenzie, Univer Sydne p. 96) Article Australia (28, 1, p. 218) Technical Not B1i2-009 Mechanism and Control of Combustion-Mode Transition in B12-023 Validating Large-Eddy Simulation for Jet Aeroacoustics. a Scramjet Engine. Toshinori Kouchi and Goro Masuya, Tohoku University, James Bridges and Mark P. Wernet, NASA John H. Glenn Rese Center at Japan; Tohru Mitani and Sadatake Tomioka, Japan Aerospace Exploration Lewis Field (28, 2, p. 226) Article Agency, Japan (28, |, p. 106) Article B12-024 Large-Eddy Simulation of Complex Geometry Jets. Simon B12-010 Estimation of Flow Properties of Gelled Fuels with Regard Eastwood, University of Cambridge, Gi eat Britain: Hao Xia to Propulsion Systems. Klaus Madlenearn d Helmut K. Ciezki, DLR, German Oxford, Great Britain; and Paul G. Tucker, University of Cambri Aerospace Research Center, Germany (28, |, p. 113) Article based on AIAA Britain (28, 2, p. 235) Article Paper 2009-5240 B12-025 Some Issues in Large-Eddy Simulations for Chevron Nozzle B12-011 Analytical and Numerical Development of a Baffled Liquid Jet Flows. Ali Uzun and M. Y. Hussaini, Florida State University (28, 2, p Rocket Combustion Stability Code. John Matthew Quinlan, Allan 7 246) Article Kirkpatrick, Dan Milano, and Charles E. Mitchell, Colorado State University: and Timothy D. Hinerman, Pratt and Whitney Rocketdyne (28, 1, p. 122) B12-026 Effect of Large-Eddy Simulation Fidelity on Predicted Article Mechanisomf sJ et Noise Reduction. Jeonglae Kim, Daniel J. Bodony, and Jonathan B. Freund, University of Illinois at mpaign (28, 2, p B1i2-012 Ignition of Metal Powder Layers of Different Thickness by 259) Article Electrostatic Discharge. Rayon A. Williams, Edward L. Dreizin, and Ervin Beloni, New Jersey Institute of Technology (28, |, p. 132) Article B12-027 High-Speed and High-Reynolds-Number Jet Control Using Localized Arc Filament Plasma Actuators. M. Samimy, M. Kearney B12-013 Gradient Mechanism of Detonation Initiation Under Action Fischer, and J.-H. Kim, Ohio State University (28, 2, p. 269) Article of High-Voltage Nanosecond Discharge. Andrew Starikovskiy and Alexsandr E. Rakitin, Moscow Institute of Physics and Technology, Russia B12-028 Analysis of the Near Field in a Plasma-Actuator-Controlled (28, |, p. 140) Article Supersonic Jet. D. V. Gaitonde, Ohio State University (28, 2, p. 281) Article I. PROPULSION. VOI B12-029 Pulsed-Jet Ejector Thrust Augmentor Characteristics. |saac B12-044 Enhanced Cooling of a Liquid-Fueled Rocket Thrust Choutapalli, University of Texas—Pan American, Anjaneyulu Krothapalli Chamber by Metal Foams. Mo Bai and J. N. Chung. University of Florida State University, and Mehmet B. Alkislar, Bo Commercie 28 (28, 2, p. 293) Article based on AIAA Paper 2005 B12-045 Surface Coatingo f Nitroamine Explosives and Its Effectso n B12-030 Experimental Study on Rocket Nozzle Side Load Reduction. the Performance of Composite Modified Double-Base Propellants. nd Chloe Genin, DLR, Ger lerospace ¢ ( a 28 CI Chi China (PRC) : Fengsheng Li, Article \ vlogy, China (PRC); Jingyu Wang, ind Xiaode Guo, Nanjing University B12-031 rheoretical Modeling and Numerical Study for Thrust- &C) (28, 2. p. 444) Artick Oscillation Characteristics in Solid Rocket Motors. Q har /hi W Wan-Xinge Su. Jun-wei Li. ar ne. B B12-046 Effect of Surface Roughness and Radiation on Graphite ] China (PRC) (28, 2, | Nozzle Erosion in Solid Rocket Motors. Piyush Thakre, CS-adapco, Lid ogy (28, 2, p. 448) Technical B12-032 Dynamic Characteristics of Simplex Swirl Injector in Low Frequency Range. Tacock Khil, L/G A Kor ROK ( University. Korea (ROK): Vladimir G. B Vv B12-04 Heat Sink and Conversioonf Catalytic Steam Reforming for ite. Russia: and Yi Von Hydrocarbon Fuel ‘hen Jia, Jingsong Gong, Yitan Xhou, and (28, 2, p. 323) Artick 1a (PRC) (28, 3, p. 453) Article B12-033 Hall-Effect Thruster Channel Surface Properties Inves- B12-048 Spatial Development and Temperature of Spark Kernels tigation. David G. Zidar and Joshu Exiting into Quiescent Air. D unck and Barry V. Kiel, U. 5. Au OR 7» 33 j wative Scientific Solutions: and sible (28, 3, p. 458) Article B12-034 Computational Study of Hall-Effect Thruster with Ambient : Performance Evaluation of a Ramjet Model in a Pulse Atmospheric Gas as Propellant. ; a i | 8 » 344) Artick { t Mach 4.5 Reeesiort Adolfo, and Giambattista Italy (28, 3, p. 466) Artick B12-035 Hall Thruster Cathode Flow Impact on Coupling Voltage nentation with Cooled Pylon Injection in a and Cathode Life. Dan Goebel, K K. J | [ fl Korea (ROK) } Laborato ( 28 ramp Injector/Gas-Pilot Flame in a B12-036 Novel Control of Magnetoplasma Thruster by Using a X \ ind Yan Mineglei, Beithane Rotating Radio Frequency System. N ( m Scramjet Y nd S. Nakamoto, A J 238 i China (PRC) B 12-037 Performance Evaluation of the T6 lon Engine D M. bel, Richard R. H ind Loops-Coupled Hysteresis: : Fli: ght-Test of Inlet Start/Unstart. Tao Cui, Xuegang He, 7 ) China(PRC)(28 B12-038 Autonomous Navigation System for Spacecraft Using Low lhrust Trajectories. Erika DeB ( tor Blade Tip Clearance Flow Control in a 28 SO) Article Thon C, Corke, and Scott ¢ 2> 5 YO) ‘ \rt B12-039 Computer Simulations of Exothermic Propellants in a Microlaser Ablation Plasma Thruster. | eration Mode Transition in Dual-Bell Nozzles Mo ersily of Tenne 28 with Cooling Koichi Yonezawa, Hidekazu Koga Japan; Tatsuya Kimura B 12-040 Fabrication of Catalyst-Insertion-Type Microelectrome id Kazuhiko Yokota. Aovama chanical Systems Monopropellant Thruster. J \ / ie of Science K AK | ce Research 1 N KOK Festing and Numerical Simulations of N r -< ( ‘ lu ‘ ‘ vfields. D raj Kapilavai and John Tapee, John Thomas R. Wayman and (28. 3 p 530) B12-041 Optimization of Hybrid Sounding Rockets for Hypersonic lesting. | nzo Casalino and D ri c. & i 28 105) Article (05 Rapid Analysis of Scraanmd Ljineeart Pl ug Nozzles. Derek 7 Wir an (283,. p B12-042 Investigation of Short Contact Time Reactors for Regeneratively Cooled Hypersonic Vehicles. Jo! ( \W allace Chinitz and Gal B \Th M ?.()5 quea ometry Effectso n Aerothermal Performanceo f ( ambi ! [ } eaka low Ca lips. Chao Zhou, P ui rsity, China e, Great Britain (28, 3, p B12-043 Comparison of RANS and LES for Prediction of Wall Heat rransfer in a Highly Loaded Turbine Guide Vane Laut Y. Gicquel, European ¢ \ ; 5 ffect f Chamber Diameter on the Flowfield in Computation, France: and | | / | 2 | if ombustors. ¢ hou Lian, Charles L. Merkle, and 28 p Article 1438 J. PROPULSION, VOL .. 28, NO. 6: 2012 INDEX B12-059 Experimental Study Swirl Injector Dynamic Response B12-074 Thermodynamic Gas Model Effect on Gas Turbine Using a Hydromechanical Pulsator. Benjamin Ahn, Maksud Ismailov, and Performance Simulations. Luis Gallar, Valentino Volpe, Martino Salussolia, Stephen Heister, Purdue University (28, 3, p. 585) Article Vassilios Pachidis, and Anthony Jackson, Cranfield University, Great Britain (28, 4, p. 719) Article B12-060 Velocity Coupling from Pulse-Test Firings. C. W. Rousseau and J. H. Knoetze, University of Stellenbosch, South Africa (28, 3, p. 596) B12-075 Aerodynamic Performance of Fan-Flow Defiectors for Jet- Article Noise Reduction. J. Xiong, F. Liu, and D. Papamoschou, University of California, Irvine (28, 4, p. 728) Article B12-061 Performance of Dimethyl Ether Arcjet Thrusters and Its Dependence on Electrode Configurations. Akira Kakami, Shinji Beppu, B12-076 Effects of Flameholder Configurations on Combustion in Muneyuki Maiguma, and Takeshi Tachibana, Kyushu Institute of Technology, Scramjet Engines. Sang Hun Kang, Yang G. Lee, and Soo Seok Yang, Korea Japan (28, 3, p. 603) Article Aerospace Research Institute, Korea (ROK); and Byungil Choi, Tohoku University, Korea (ROK) (28, 4, p. 739) Article B12-062 Scaling of Efficiency with Applied Magnetic Field in Magnetoplasmadynamic Thrusters. Dan R. Lev and Edgar Choueiri, B12-077 Effects of Angle of Attack on Inlet Buzz. Mohammad Reza Princeton University (28, 3, p. 609) Article Soltani and Mohammad Farahani, Sharif University of Technology, tran (28, 4, p. 747) Article B12-063 Laser-Induced Fluorescence Measurements of Product Penetration Within an Ultracompact Combustor. Stanislav Kostka, B12-078 Separation Control for Aeroengine Intakes, Part 1: Low- Spectral Energies, LLC; Richard D. Branam, Air Force Institute of Speed Investigation of Control Strategies. Christian 1 Wakelam, Technology: Michael W. Renfro, Universityo f Connecticut; Patrick J. Lakusta, Universitat der Bundeswehr Munchen, Germany; Tom P. Hynes and Howard Air Force Institute of Technology, James R. Gord, U.S. Air Force Research P. Hodson, University of Cambridge, Great Britain; Simon W Evans, Laboratory; and Sukesh Roy, Spectral Energies, LLC (28, 3, p. 617) Article Worcester Polytechnic Institute, and Philippe Chanez, Snecma, France (28, 4, p. 758) Article B12-064 NASA’s Evolutionary Xenon Thruster Long-Duration Test Results. Daniel Herman, George C. Soulas, Jonathan L. Van Noord, and B12-079 Separation Control for Aeroengine Intakes, Part 2: High- Michael J. Patterson, NASA John H. Glenn Research Center at Lewis Field Speed Investigations. Christian T. Wakelam, Universitat der Bundeswehr (28, 3, p. 625) Article Munchen, Germany; Tom P. Hynes and Howard P. Hodson, University of Cambridge, Great Britain; Simon W. Evans, Worcester Polytechnic Institute; B12-065 Analysis of Thrust Characteristics of a Magnetic Sail in a and Philippe Chanez, Snecma, France (28, 4, p. 766) Article Magnetized Solar Wind. Hiroyuki Nishida, Tokyo University of Agriculture and Technology, Japan; and Ikkoh Funaki, Japan Aerospace Exploration B12-080 Improvements in Modeling 90-Degree Bleed Holes for Agency, Japan (28, 3, p. 636) Article Supersonic Inlets. John Slater, NASA John H. Glenn Research Center at Lewis Field (28, 4, Pp 773) Article B12-066 Thrust Evaluation of aM agnetic Sail by Flux-Tube Model. Yasumasa Ashida, Kyoto University, Japan; Ikkoh Funaki, Japan Aerospace B12-081 Detached-Eddy Simulation of Rotating Stall Inception for a Exploration Agency, Japan; Hiroshi Yamakawa, Kyoto University, Japan; Full-Annulus Transonic Rotor. Hongsik lim, Xiang-Ying Chen, and Yoshihiro Kajimura, Akashi National College of Technology, Japan; and Gecheng Zha, University of Miami (28, 4, p. 782) Article Hirotsogu Kojima, Kyoto University, Japan (28, 3, p. 642) Article B12-082 Investigation of High-Pressure Turbine Endwall Film- B12-067 Thrust and Attitude Evaluation of Magnetic Sail by Three- Cooling Performance Under Realistic Inlet Conditions. Simone Salvadori Dimensional Hybrid Particle-in-Cell Code. Yoshihiro Kajimura, Akashi and Luca Ottanelli, University of Florence, Italy; Magnus Jonsson and Peter National College of Technology, Japan; Ikkoh Funaki, Japan Aerospace Ott, Ecole Polytechnique Fédérale de Lausanne, Switzerland; and Francesco Exploration Agency, Japan, Masaharu Matsumoto, Kobe University, Tku Martelli, University of Florence, Italy (28, 4, p. 799) Article Shinohara, Japan Aerospace Exploration Agency, Japan; Hideyuki Usui, Kobe University, Japan; and Hiroshi Yamakawa, Kyoto University, Japan (28, B12-083 Side-Force Amplification on an Aerodynamically Thrust- 3, p. 652) Article Vectored Aerospike Nozzle. Shannon D. Eilers, Matthew D. Wilson, Stephen A. Whitmore, and Zachary W. Peterson, Utah State University (28, 4, p. 811) B12-068 Power Density of aB are Electrodynamic Tether Generator. Claudio Bombardelli, Technical University of Madrid, Spain (28, 3, p. 664) Article Technical Note B12-084 Carbon-Carbon Nozzle Erosion and Shape-Change Effects B12-069 Comparison of Flammability Characteristics of Paraffin in Full-Scale Solid-Rocket Motors. Francesco Nasuti and Daniele Bianchi, Mixtures and Polyethylene. Marcos J. Gemaque and Fernando S. Costa, University of Rome “La Sapienza”, Italy (28, 4, p. 820) Article Brazilian National Institute for Space Research, Brazil (28, 3, p. 668) Technical Note B12-085 Analysis of Multivane Radiometer Arrays in High-Altitude Propulsion. Barry M. Cornella and Andrew D. Ketsdever, University of B12-070 Rate-Controlled Constrained-Equilibrium Modeling of H/ Colorado at Colorado Springs, Natalia E Gimelshein and Sergey F. O Reacting Nozzle Flow. Mohammad Janbozorgi and Hameed Metgalchi, Gimelshein, ERC, Inc. (28, 4, p. 831) Article Northeastern University (28, 4, p. 677) Article B12-086 Laser Ablation Propulsion Performance of Surface- B12-071 Compressible Modeling of the Internal Flow in a Gas- Modified Polyoxymethylene. Akihoro Sasoh, Naoya Ogita and Mitsuhiro Centered Swirl-Coaxial Fuel Injector. Nathanie! Trask and David P. Shikida, Nagoya University, Japan; and John E. Sinko, Ohio State University Schmidt, University of Massachuset:s, Malissa Lightfoot and Stephen at Newark (28, 4, p. 840) Article Danczyk, U.S. Air Force Research Laboratory (28, 4, p. 685) Article B12-087 Performance Evaluation of an lodine- Vapor Hall Thruster. B12-072 Effects of Flow Passage Expansion or Contraction on Jet- James Szabo, Bruce Pote, Surjeet Paintal, and Mike Robin, Busek Company, Fuel Surface Deposition. Hua Jiang, Jamie Ervin, Steven Zabarnick, and Inc.; Adam Hillier, Richard D. Branam, and Richard E. Huffmann, Air Force Zachary West, University of Dayton Research Institute (28, 4, p. 694) Article Institute of Technology (28, 4, p. 848) Article B12-073 Ignition and Combustion of Boron Nanoparticles in Ethanol B12-088 Fluidic Thrust Vector Control of Supersonic Jet Using Spray Flame. Sumanta Acharya, Srinibas Karmakar, and Kerry M. Dooley, Coflow Injection. Jun-Young Heo and Hong-Gye Sung, Korea Aerospace Louisiana State University (28, 4, p. 707) Article University, Korea (ROK) (28, 4, p. 858) Technical Note