Table Of Content

JOURNAL OF PROPULSION AND POWER Vol. 10, No. 6, Nov.—Dec. 1994 1994 Journal of Propulsion and Power Index How to Use the Index In the Subject Index, pages 917-921, each technical paper is listed under a maximum of three appropriate headings. Note the number in boldface type following each paper title, and use that number to locate the paper in the Chronological Index. The Author Index, pages 922 and 923, lists all authors associated with a given technical paper. The locating numbers are identical to those in the Subject Index. The Chronological Index, pages 923-927, lists all papers by their unique code numbers. This list- ing contains titles, authors and their affiliations, and volume, issue number and page where the paper appeared. It also gives the AIAA paper number, if any, on which the article was based, as well as the “CP” or conference volume number if the paper was published in a bound collection of meetings papers. Comments, Replies, and Errata are listed directly beneath the paper to which they refer. If the paper to which they refer was published prior to 1993, that paper also will appear in both the Subject and Chro- nological Indexes. Authors of Comments also are listed in the Author Index. Subject Index Aircraft Technology, Conventional, sion Applications B94-112 Fuel Cells STOL/VTOL Improved Method for Estimation of the Maxi- mum Instantaneous Distortion Values Hierarchical Analysis of Options for Lunar-Sur- Aerodynamics B94-072 face Power B94-059 Circular-to-Rectangular Transition Duct Flow Study on Computing Separating Flows Within a Without and with Inlet Swirl B94-011 Hydrogen and Unique Fuels Diffusing Inlet S-Duct B94-091 Multiple Hole Ejector Performance with Short Propeller and Rotor Systems Turbulent Combustion Regimes for Hypersonic Wide Angle Diffusers B94-051 Propulsion Employing Hydrogen-Air Diffu- Axial Compressor Performance During Surge Design of Optimum Propellers B94-093 sion Flames B94-061 B94-045 Estimation of Fatigue Strength Enhancement for Three-Dimensional Simulation of a Translating Carburized and Shot-Peened Gears Photovoltaic Power Strut Inlet B94-025 B94-050 Pellet Bed Reactor Concepts for Nuclear Propul- Comparison of Optical Measurement Techniques Experimental Investigation of Counter-Rotating sion Applications B94-112 for Turbomachinery Flowfields B94-023 Propfan Flutter at Cruise Conditions Hierarchical Analysis of Options for Lunar-Sur- High-Alpha Vectoring Characteristics of the B94-047 face Power B94-059 F-18 /HARV B94-015 Feasibility Study of a Contained Pulsed Nuclear Simulation Propulsion Engine B94-035 Aeroelasticity and Aeroservoelasticity Numerical Study of Low-Pressure Concept for Nonlinear Dynamic Simulation of Single- and Nuclear Thermal Rockets B94-003 Experimental Investigation of Counter-Rotating Multispool Core Engines, Part I: Computa- Hierarchical Analysis of Options for Lunar-Sur- Propfan Flutter at Cruise Conditions tional Method B94-117 face Power B94-059 B94-047 Nonlinear Dynamic Simulation of Single- and Multispool Core Engines, Part II: Simulation, Rotating Machinery Aerospace Plane Code Validation B94-118 Numerical Solutions of Two-Dimensional Multi- Thrust Loss Due to Supersonic Mixing STOL/VTOL/STOVL stage Rotor/Stator Unsteady Flow Interactions B94-110 B94-120 Multiple Hole Ejector Performance with Short Flight Control Integration Wide Angle Diffusers B94-051 Theoretical vs Experimental Rotordynamic Coef- ficients of Incompressible Flow Labyrinth Approximate Similarity Principle for a Full- Sensor Biases Effect on the Estimation Algo- Scale STOVL Ejector B94-026 Seals B94-099 rithm for Performance-Seeking ControBll9e4r-s0 73 IntCeornnafli guRreavteirosni ngfo r FAlSowT OVinL a ATiariclrpaifpt e Offtake Chatriaocn teirni azna tiAoxnia l ofF lAobwr uCpto mpRroetsatsionrg StalBl 94I-ni0t9ia7- Flight Operations B94-016 Compressor Unsteady Aerodynamic Response to Rotating Stall and Surge Excitations Testing, Flight and Ground Turbulent Combustion Regimes for Hypersonic B94-096 Propulsion Employing Hydrogen-Air Diffu- Pyrometry for Turbine Applications in the Pres- Forcing Function Generator Fluid Dynamic Ef- sion Flames B94-061 ence of Reflection and Combustion fects on Compressor Blade Gust Response B94-027 B94-126 Noise Comparison of Optical Measurement Techniques for Turbomachinery Flowfields B94-023 Vibration Low-Noise, High-Strength, Spiral-Bevel Gears Theoretical Study of Sensor-Actuator Schemes for Helicopter Transmission B94-049 Low-Noise, High-Strength, Spiral-Bevel Gears for Rotating Stall Control B94-013 for Helicopter Transmission B94-049 Performance Solar Power Sensor Biases Effect on the Estimation Algo- Production and Use of Metals and Oxygen for Lu- rithm for Performance-Seeking Controllers Energy nar Propulsion B94-114 B94-073 Alternate Fuels Wind Power Powerplant Integration Combustion of Microemulsion Sprays Design of Optimum Propellers B94-093 Pellet Bed Reactor Concepts for Nuclear Propul- B94-103 Dynamic Aeroelastic Stability of Vertical-Axis 918 J. PROPULSION, VOL. 10, NO. 6: 1994 INDEX Wind Turbines Under Constant Wind Velocity Comment on “Simple Modeling of Particle Tra- Near-Wake Characteristics of Various V-Shaped B94-048 jectories in Solid Rocket Motors” Bluff Bodies B94-006 B91-026 Comment on “Method for Reducing Stagnation Fluid Dynamics Pressure Losses in Segmented Solid Rocket Hydrodynamics Motors” B92-105 Aeroacoustics Theoretical vs Experimental Rotordynamic Co- Multiphase Flows Effect of Impinging Jet Excitation on Curved efficients of Incompressible Flow Labyrinth Surface Heat Transfer B94-040 Seals B94-099 Characteristics of Sprays Produced by Coaxial Combustion Zone-Acoustic Cavity Interactions Airblast Atomizers B94-064 in Rocket Combustors B94-030 Hypersonic Flow Effect of External Forcing on Droplet Dispersion in a Developing Shear Layer B94-055 Boundary Layers and Heat Transfer— Calculation of Scramjet Inlet with Thick Bound- Numerical Prediction of a Turbulent Evaporating Turbulent ary-Layer Ingestion B94-086 Fuel Spray in a Recirculating Flow Experimental and Computational Results for the B94-039 External Flowfield of a Scramjet Inlet High Reynolds Number and Turbulence Effects on Turbine Heat Transfer B94-119 B94-074 Plasmadynamics and MHD Turbulent Combustion Regimes for Hypersonic Lag Model for Turbulent Boundary Layers over Rough Bleed Surfaces B94-078 Propulsion Employing Hydrogen-Air Diffu- Similarity Relation for Maximal Gas Compres- Investigation of Shock/Turbulent Boundary- sion Flames B94-061 sion by Strong Ionizing Shocks B94-124 Layer Bleed Interactions B94-010 Use of Permanent Magnets to Reduce Anode Inlet, Nozzle, Diffuser, and Channel Flows Losses in MPD Thrusters B94-077 Boundary-Layer Stability and Transition F/A-18 Inlet Calculations at 60-Deg Angle of At- Rarefied Flows tack and 10-Deg Sideslip B94-116 High Reynolds Number and Turbulence Effects on Turbine Heat Transfer B94-119 Numerical Study of the Performance of Swept, Direct Simulation Monte Carlo Model of Low Curved Compression Surface Scramijet Inlets Reynolds Number Nozzle Flows B94-076 B94-115 Computational F luid Dynamics Design of Axisymmetric Channels with Rota- Reacting Flows and Combustion Numerical Solutions of Two-Dimensional Multi- tional Flow B94-100 stage Rotor/Stator Unsteady Flow Interac- Study of the Compressible Flow in a Diffusing S- OH Laser-Induced Fluorescence Velocimetry tions B94-120 Duct B94-092 Technique for Steady, High-Speed, Reacting F/A-18 Inlet Calculations at 60-Deg Angle of At- Study on Computing Separating Flows Within a Flows B94-108 tack and 10-Deg Sideslip B94-116 Diffusing Inlet S-Duct B94-091 Modeling of Supersonic Turbulent Combustion Coupling Between Vorticity and Pressure Oscil- Calculation of Scramjet Inlet with Thick Bound- Using Assumed Probability Density Func- lations in Combustion Instability ary-Layer Ingestion B94-086 tions B94-107 B94-106 Direct Simulation Monte Carlo Model of Low Coupling Between Vorticity and Pressure Oscil- Investigation of Supersonic Jet Plumes Using an Reynolds Number Nozzle Flows B94-076 lations in Combustion Instability B94-106 Improved Two-Equation Turbulence Model Three-Dimensional Analysis of Scramjet Nozzle Simultaneous Velocity and Temperature Mea- B94-101 Flows B94-075 surements in a Premixed Dump Combustor Experimental and Computational Results for the B94-088 Design of Axisymmetric Channels with Rota- External Flowfield of a Scramjet Inlet Droplet Transport in a Swirl-Stabilized Spray tional Flow B94-100 B94-074 Flame B94-087 Theoretical vs Experimental Rotordynamic Co- Improved Method for Estimation of the Maxi- Computation of Shock-Induced Combustion Us- efficients of Incompressible Flow Labyrinth mum Instantaneous Distortion Values ing a Detailed Methane-Air Mechanism Seals B94-099 B94-072 B94-084 Single-Passage Euler Analysis of Oscillating New Tube End Closure System for the Ram Ac- Formulation, Predictions, and Sensitivity Analy- Cascade Aerodynamics for Arbitrary Inter- celerator B94-071 sis of a Pyrotechnically Actuated Pin Puller blade Phase B94-095 Three-Dimensional Simulation of a Translating Model B94-069 Study on Computing Separating Flows Within a Strut Inlet B94-025 Assumed Joint Probability Density Function Ap- Diffusing Inlet S-Duct B94-091 Internal Reversing Flow in a Tailpipe Offtake proach for Supersonic Turbulent Combustion Solution-Adaptive Structured-Unstructured Grid Configuration for ASTOVL Aircraft B94-016 B94-066 Method for Unsteady Turbomachinery Analy- Installed F/A-18 Inlet Flow Calculations at a Nonequilibrium Combustion Model for Fuel- sis, Part I: Methodology B94-080 High Angle of Attack B94-014 Rich Gas Generators B94-065 Solution-Adaptive Structured-Unstructured Grid Computational Investigation of Circular-to-Rect- Prediction of NOx Production in a Turbulent Hy- Method for Unsteady Turbomachinery Analy- angular Transition Ducts B94-012 drogen-Air Jet Flame B94-021 sis, Part II: Results B94-081 Circular-to-Rectangular Transition Duct Flow Inlet Velocity Profile Effects on Turbulent Swirl- Lag Model for Turbulent Boundary Layers over Without and with Inlet Swirl B94-011 ing Flow Predictions B94-020 Rough Bleed Surfaces B94-078 Numerical Study of Low-Pressure Concept for Velocity Characteristics of Reacting and Nonre- Three-Dimensional Analysis of Scramjet Nozzle Nuclear Thermal Rockets B94-003 acting Flows ina Dump Combustor B94-019 Flows B94-075 Experimental and Computational Results for the Jets, Wakes, and Viscid-Inviscid Flow Separated Flows External Flowfield of a Scramjet Inlet Interactions B94-074 F/A-18 Inlet Calculations at 60-Deg Angle of At- Assumed Joint Probability Density Function Ap- Coupling Between Vorticity and Pressure Oscil- tack and 10-Deg Sideslip B94-116 proach for Supersonic Turbulent Combustion lations in Combustion Instability B94-106 Study of the Compressible Flow in a Diffusing S- B94-066 Supersonic-Ejector Characteristics Using a Petal Duct B94-092 Effect of External Forcing on Droplet Dispersion Nozzle B94-102 New Tube End Closure System for the Ram Ac- in a Developing Shear Layer B94-055 Investigation of Supersonic Jet Plumes Using an celerator B94-071 Numerical Study of Mixing in Supersonic Com- Improved Two-Equation Turbulence Model Incipient Torsional Stall Flutter Aerodynamic bustors with Hypermixing Injectors B94-101 Experiments on Three-Dimensional Wings B94-041 Structure and Penetration of a Supercritical Fluid B94-028 Numerical Prediction of a Turbulent Evaporating Jet in Supersonic Flow Forcing Function Generator Fluid Dynamic Ef- Fuel Spray in a Recirculating Flow Multiple Hole Ejector Performance with Short fects on Compressor Blade Gust Response B94-039 Wide Angle Diffusers B94-051 B94-027 Three-Dimensional Simulation of a Translating Effect of Impinging Jet Excitation on Curved Near-Wake Characteristics of Various V-Shaped Strut Inlet B94-025 Surface Heat Transfer B94-040 Bluff Bodies B94-006 Installed F/A-18 Inlet Flow Calculations at a Approximate Similarity Principle for a Full- High Angle of Attack B94-014 Scale STOVL Ejector B94-026 Shock Waves and Detonations Computational Investigation of Circular-to-Rect- Experimental Studies on Mixing of Two Co-Ax- anguiar Transition Ducts B94-012 ial High-Speed Streams B94-008 Similarity Relation for Maximal Gas Compres- J. PROPULSION, VOL. 10, NO. 6: 1994 INDEX sion by Strong Ionizing Shocks B94-124 Incipient Torsional Stall Flutter Aerodynamic Sensor Systems Computation of Shock-Induced Combustion Us- Experiments on Three-Dimensional Wings ing a Detailed Methane-Air Mechanism B94-028 Pyrometry for Turbine Applications in the Pres- B94-084 Forcing Function Generator Fluid Dynamic Ef- ence of Reflection and Combustion B94-126 Review of Shock-Induced Supersonic Combus- fects on Compressor Blade Gust Response tion Research and Hypersonic Applications B94-027 Launch Vehicle and Missile (LV/M) B94-082 Theoretical Study of Sensor-Actuator Schemes Technology for Rotating Stall Control B94-013 Subsonic Flow Launch Vehicle and Sounding Rocket Systems Vortices Design of Axisymmetric Channels with Rota- Launch Vehicle Performance Using Metallized tional Flow B94-100 Experimental Investigation of a Supersonic Propellants B94-113 Installed F/A-18 Inlet Flow Calculations at a Swept Ramp Injector Using Laser-Induced Io- New Tube End Closure System for the Ram Ac- High Angle of Attack B94-014 dine Fluorescence B94-017 celerator B94-071 Circular-to-Rectangular Transition Duct Flow Air Liquefaction and Enrichment System Propul- Without and with Inlet Swirl B94-011 Wave Motion and Sloshing sion in Reusable Launch Vehicles B94-067 Comment on “Simple Modeling of Particle Tra- Supersonic Flow On-Orbit Propellant Motion Resulting from an jectories in Solid Rocket Motors” B91-026 Impulsive Acceleration B94-090 Thrust Loss Due to Supersonic Mixing B94-110 Mission Studies and Economics Supersonic-Ejector Characteristics Using a Petal Nozzle B94-102 Guidance, Control, and Dynamics Investigation of Supersonic Jet Plumes Using an Technology Launch Vehicle Performance Using Metallized Propellants B94-113 Improved Two-Equation Turbulence Model B94-101 Aircraft Stability and Control Effect of Film Cooling/Regenerative Cooling on Scramjet Engine Performances B94-085 High-Alpha Vectoring Characteristics of the F- Propulsion and Propellant Systems Preliminary Investigations on Improving Air- 18/HARV B94-015 Solid Rocket Motor Temperature Sensitivity StrAuuctgumree ntaendd PRenoectkreatt ioPne rfofo ram aSnucpeer criticBa9l 4-F0lu6i0d Astrodynamics High Reynolds Number and Turbulence B9E4f-f1ec2t5s ExpJSeewtre ipimnte nStRuapalem rps onIIninvcje esctFtilogroa wtU isoinn g oLfa sear -ISnudpBue9cr4esd-o 0n5iI4oc- StaLtaiuonnckheeerpsin g with Two-Way ElectromBa9g4n-e1t2i7c Effopenoc sti Ttueor fb PirMnouep letlHiledaainttm eTnCrsoaimnosbnfuaeslrt ioFnl amelets BBin99 44C--o111m095- dine Fluorescence B94-017 Control System Design Effect of Regenerative Cooling on Rocket En- Investigation of Shock/Turbulent Boundary-Lay- gine Specific Impulse B94-037 er Bleed Interactions B94-010 Damage-Mitigating Control of a Reusable Rock- Experimental Demonstration and Simulation of a Experimental Studies on Mixing of Two Co-Ax- et Engine B94-029 Dual-Stage Solid Propellant Gun Concept ial High-Speed Streams B94-008 B94-036 Control Theory Transonic Flow Simulation Sensor Biases Effect on the Estimation Algo- Single-Passage Euler Analysis of Oscillating rithm for Performance-Seeking Controllers Experimental Demonstration and Simulation of a Cascade Aerodynamics for Arbitrary Inter- blade Phase B94-095 B94-073 Dual-Stage Solid Propellant Gun Concept B94-036 Vane-Blade Interaction in a Transonic Turbine, Dynamics Part I: Aerodynamics B94-042 Unsteady Flows Nonlinear Dynamic Simulation of Single- and Propulsion Multispool Core Engines, Part I: Computa- Nonlinear Dynamic Simulation of Single- and tional Method B94-117 Airbreathing Propulsion Multispool Core Engines, Part I: Computa- Nonlinear Dynamic Simulation of Single- and tional Method B94-117 Multispool Core Engines, Part II: Simulation, Facility Opportunities and Associated Stream Nonlinear Dynamic Simulation of Single- and Code Validation B94-118 Chemistry Considerations for Hypersonic Air- Multispool Core Engines, Part II: Simulation, Breathing Propulsion B94-001 Code Validation B94-118 Engine Control Adaptive Modeling of Jet Engine Performance Pulsed Jets in Supersonic Crossflow B94-104 with Application to Condition Monitoring Characterization of Abrupt Rotating Stall Initia- Damage-Mitigating Control of a Reusable Rock- B94-122 tion in an Axial Flow Compressor et Engine B94-029 Numerical Study of the Performance of Swept, B94-097 Theoretical Study of Sensor-Actuator Schemes Curved Compression Surface Scramjet Inlets Compressor Unsteady Aerodynamic Response to for Rotating Stall Control B94-013 B94-115 Rotating Stall and Surge Excitations Supersonic-Ejector Characteristics Using a Petal B94-096 Interdisciplinary Topics Nozzle B94-102 Single-Passage Euler Analysis of Oscillating Characterization of Abrupt Rotating Stall Initia- Cascade Aerodynamics for Arbitrary Inter- Lasers and Laser Application tion in an Axial Flow Compressor B94-097 blade Phase B94-095 Compressor Unsteady Aerodynamic Response to Solution-Adaptive Structured-Unstructured Grid Interlaboratory Comparison of Phase Doppler Rotating Stall and Surge Excitations Method for Unsteady Turbomachinery Analy- Measurements in a Research Simplex Atomiz- B94-096 sis, Part I: Methodology B94-080 er Spray B94-056 Analytic Design Methods for Wave Rotor Cy- Solution-Adaptive Structured-Unstructured Grid Raman Measurements at the Exit of a Combustor cles B94-094 Method for Unsteady Turbomachinery Analy- Sector B94-022 Design of Optimum Propellers B94-093 sis, Part II: Results B94-081 NO,-Based Laser-Induced Fluorescence Tech- Study of the Compressible Flow in a Diffusing S- Efficient Method for Predicting Rotor/Stator In- nique to Measure Cold-Flow Mixing Duct B94-092 teraction B94-046 B94-007 Solution-Adaptive Structured-Unstructured Grid Axial Compressor Performance During Surge Method for Unsteady Turbomachinery Analy- B94-045 Research Facilities and Instrumentation sis, Part I: Methodology B94-080 Vane-Blade Interaction in a Transonic Turbine, Solution-Adaptive Structured-Unstructured Grid Part I: Aerodynamics B94-042 Test Facilities for High-Power Electric Propul- Method for Unsteady Turbomachinery Analy- Vane-Blade Interaction in a Transonic Turbine, sion B94-002 sis, Part II: Results B94-081 Part II: Heat Transfer B94-043 Facility Opportunities and Associated Stream Improved Method for Estimation of the Maxi- Performance Evaluation of LE-7 High-Pressure Chemistry Considerations for Hypersonic Air- mum Instantaneous Distortion Values Pumps B94-038 Breathing Propulsion B94-001 B94-072 920 J. PROPULSION, VOL. 10, NO. 6: 1994 INDEX Air Liquefaction and Enrichment System Propul- NO)-Based Laser-Induced Fluorescence Tech- Preliminary Design of a Space Propulsion Sys- sion in Reusable Launch Vehicles B94-067 nique to Measure Cold-Flow Mixing tem Utilizing Stored Thermal Energy Nonequilibrium Combustion Model for Fuel- B94-007 B94-004 Rich Gas Generators B94-065 Comment on “Evaluation of the Munich Method Experimental Study of a Model Gas Turbine Combustion Instability for Modeling Rocket Engine Performance” Combustor Swirl Cup, Part I: Two-Phase B93-029 Characterization B94-062 Effect of Multidimensional Flamelets in Com- Experimental Study of a Model Gas Turbine posite Propellant Combustion B94-105 Environmental Effects Combustor Swirl Cup, Part II: Droplet Dy- Application of Dynamical Systems Theory to namics B94-063 Nonlinear Combustion Instabilities B94-070 Analytic Design Methods for Wave Rotor Cy- Preliminary Investigations on Improving Air- Combustion Zone-Acoustic Cavity Interactions cles B94-094 Augmented Rocket Performance B94-060 in Rocket Combustors B94-030 Combustion and Environmental Challenges for Estimation of Fatigue Strength Enhancement for Gas Turbines in the 1990s B94-018 Droplet Characterization Carburized and Shot-Peened Gears B94-050 Fuels and Propellants, Properties of Droplet Transport in a Swirl-Stabilized Spray Efficient Method for Predicting Rotor/Stator In- Flame B94-087 Solid Rocket Motor Temperature Sensitivity teraction B94-046 Characteristics of Sprays Produced by Coaxial B94-125 Vane-Blade Interaction in a Transonic Turbine, Airblast Atomizers B94-064 Production and Use of Metals and Oxygen for Part I: Aerodynamics B94-042 Experimental Study of a Model Gas Turbine Lunar Propulsion B94-114 Vane-Blade Interaction in a Transonic Turbine, Combustor Swirl Cup, Part I: Two-Phase Effect of Multidimensional Flamelets in Com- Part II: Heat Transfer Characterization B94-062 posite Propellant Combustion B94-105 Incipient Torsional Stall Flutter Aerodynamic Experimental Study of a Model Gas Turbine Combustion of Microemulsion Sprays Experiments on Three-Dimensional Wings Combustor Swirl Cup, Part II: Droplet Dy- B94-103 B94-028 namics B94-063 Performance Evaluation of LE-7 High-Pressure Approximate Similarity Principle for a Full- Scale STOVL Ejector B94-026 Motor and Plume Particle Size Measurements in Pumps B94-038 Solid Propellant Micromotors B94-057 Comment on “Method for Reducing Stagnation Comparison of Optical Measurement Techniques Interlaboratory Comparison of Phase Doppler Pressure Losses in Segmented Solid Rocket for Turbomachinery Flowfields B94-023 Measurements in a Research Simplex Atomiz- Motors” B92-105 Prediction of NOx Production in a Turbulent Hy- er Spray B94-056 drogen-Air Jet Flame B94-021 Effect of External Forcing on Droplet Dispersion Hybrid Rocket Engines Inlet Velocity Profile Effects on Turbulent Swiri- in a Developing Shear Layer B94-055 ing Flow Predictions B94-020 Numerical Prediction of a Turbulent Evaporating Damage-Mitigating Control of a Reusable Rock- Velocity Characteristics of Reacting and Nonre- Fuel Spray in a Recirculating Flow et Engine B94-029 acting Flows in a Dump Combustor B94-039 B94-019 Ignition and Ignitor Design Combustion and Environmental Challenges for Electric and Advanced Space Propulsion Gas Turbines in the 1990s B94-018 Formulation, Predictions, and Sensitivity Analy- Experimental Investigation of a Supersonic Stationkeeping with Two-Way Electromagnetic sis of a Pyrotechnically Actuated Pin Puller Swept Ramp Injector Using Laser-Induced Io- Launchers B94-127 Model B94-069 dine Fluorescence B94-017 Optimization of Heat Transfer in a High-Energy Internal Reversing Flow in a Tailpipe Offtake Booster Rocket B94-111 Injector Design and Characterization Configuration for ASTOVL Aircraft Use of Permanent Magnets to Reduce Anode B94-016 Losses in MPD Thrusters B94-077 Characteristics of Sprays Produced by Coaxial High-Alpha Vectoring Characteristics of the Direct Simulation Monte Carlo Model of Low Airblast Atomizers F-18/HARV B94-015 Reynolds Number Nozzle Flows B94-076 B94-064 Investigation of Shock/Turbulent Boundary- Thermal Radiation in Gas Core Nuclear Reactors Layer Bleed Interactions B94-010 for Space Propulsion B94-058 Dynamic Turbine Blade Temperature Measure- Experimental Demonstration and Simulation of a Liquid Rocket Motors and Missile Systems ments Dual-Stage Solid Propellant Gun Concept Experimental Studies on Mixing of Two Co-Ax- B94-036 On-Orbit Propellant Motion Resulting from an ial High-Speed Streams B94-008 Feasibility Study of a Contained Pulsed Nuclear Impulsive Acceleration B94-090 Near-Wake Characteristics of Various V-Shaped Propulsion Engine B94-035 Bipropellant Performance of N>7H,/MMH Mixed Bluff Bodies B94-006 Anode Power Deposition in an Applied-Field Fuel in a Regeneratively Cooled Engine Segmented Anode MPD Thruster B94-034 B94-089 Combustion and Combustor Designs Demonstration and Evaluation of Carbon-Car- Hydrogen Recombination Kinetics and Nuclear bon Ion Optics B94-033 Thermal Rocket Performance Prediction Combustion of Microemulsion Sprays B94-103 Generalized Hall Acceleration B94-032 B94-068 Droplet Transport in a Swirl-Stabilized Spray Numerical Study of Low-Pressure Concept for Performance Evaluation of LE-7 High-Pressure Flame B94-087 Nuclear Thermal Rockets B94-003 Pumps B94-038 Nonequilibrium Combustion Model for Fuel- Test Facilities for High-Power Electric Propul- Effect of Regenerative Cooling on Rocket En- Rich Gas Generators B94-065 sion B94-002 gine Specific Impulse B94-037 Experimental Study of a Model Gas Turbine Axial Thrust Behavior in LOX-Pump of Rocket Combustor Swirl Cup, Part I: Two-Phase Engine Performance Engine B94-031 Characterization B94-062 Combustion Zone—Acoustic Cavity Interactions Experimental Study of a Model Gas Turbine Adaptive Modeling of Jet Engine Performance in Rocket Combustors B94-030 Combustor Swirl Cup, Part II: Droplet Dy- with Application to Condition Monitoring New Generation of High-Performance Engines namics B94-063 B94-122 for Spacecraft Propulsion B94-005 Motor and Plume Particle Size Measurements in Launch Vehicle Performance Using Metallized Comment on “Evaluation of the Munich Method Solid Propellant Micromotors B94-057 Propellants B94-113 for Modeling Rocket Engine Performance” Numerical Study of Mixing in Supersonic Com- Analytic Design Methods for Wave Rotor Cy- B93-029 bustors with Hypermixing Injectors cles B94-094 B94-041 Bipropellant Performance of NyH4/MMH Mixed Raman Measurements at the Exit of a Combustor Fuel in a Regeneratively Cooled Engine Ramjet Combustors Sector B94-022 B94-089 Prediction of NOx Production in a Turbulent Hy- Hysteresis and Bristle Stiffening Effects in Brush Numerical Study of Mixing in Supersonic Com- drogen-Air Jet Flame B94-021 Seals B94-079 bustors with Hypermixing Injectors Inlet Velocity Profile Effects on Turbulent Swirl- Axial Thrust Behavior in LOX-Pump of Rocket B94-041 ing Flow Predictions B94-020 Engine B94-031 Velocity Characteristics of Reacting and Nonre- Combustion and Environmental Challenges for New Generation of. High-Performance Engines acting Flows in a Dump Combustor Gas Turbines in the 1990s B94-018 for Spacecraft Propulsion B94-005 B94-019 J. PROPULSION, VOL. 10, NO. 6: 1994 INDEX Ramjets and Scramjets On-Orbit Propellant Motion Resulting from an Structural Optimization Impulsive Acceleration B94-090 Development of Hypersonic Engine Seals: Flow Ply Layup Optimization and Micromechanics Effects of Preload and Engine Pressures Space Systems Tailoring of Composite Aircraft Engine Struc- B94-121 tures B94-123 Numerical Study of the Performance of Swept, Pellet Bed Reactor Concepts for Nuclear Propul- Curved Compression Surface Scramjet Inlets sion Applications B94-112 Thermal Effects B94-115 Preliminary Design of a Space Propulsion Sys- Thrust Loss Due to Supersonic Mixing tem Utilizing Stored Thermal Energy Ply Layup Optimization and Micromechanics B94-110 B94-004 Tailoring of Composite Aircraft Engine Struc- Calculation of Scramjet Inlet with Thick Bound- tures B94-123 ary-Layer Ingestion B94-086 Spacecraft Propulsion System Integration Effect of Film Cooling/Regenerative Cooling on Thermophysics and Heat Transfer Scramjet Engine Performances B94-085 Optimization of Heat Transfer in a High-Energy Review of Shock-Induced Supersonic Combus- Booster Rocket B94-111 Aerothermodynamics/Thermal Protection tion Research and Hypersonic Applications New Generation of High-Performance Engines B94-082 for Spacecraft Propulsion B94-005 Effect of Film Cooling/Regenerative Cooling on Preliminary Investigations on Improving Air- Preliminary Design of a Space Propulsion Sys- Scramjet Engine Performances B94-085 Augmented Rocket Performance B94-060 tem Utilizing Stored Thermal Energy Structure and Penetration of a Supercritical Fluid B94-004 Computational Heat Transfer Jet in Supersonic Flow B94-054 Test Facilities for High-Power Electric Propul- Planar KrF Laser-Induced OH Fluorescence Im- sion B94-002 Thermal Radiation in Gas Core Nuclear Reactors aging in a Supersonic Combustion Tunnel for Space Propulsion B94-058 B94-052 Structural Mechanics and Materials Vane-Blade Interaction in a Transonic Turbine, Advanced Injection and Mixing Techniques for Part II: Heat Transfer B94-043 Scramjet Combustors B94-024 Aeroelasticity and Control Forced Convection Solid Rocket Motors and Missile Systems Dynamic Aeroelastic Stability of Vertical-Axis Wind Turbines Under Constant Wind Effect of Impinging Jet Excitation on Curved Solid Rocket Motor Temperature Sensitivity Velocity B94-048 Surface Heat Transfer B94-040 B94-125 Experimental Investigation of Counter-Rotating Motor and Plume Particle Size Measurements in Propfan Flutter at Cruise Conditions Heat Conduction Solid Propellant Micromotors B94-057 B94-047 Comment on “Method for Reducing Stagnation Localization of Aeroelastic Modes in Mistuned Optimization of Heat Transfer in a High-Energy Pressure Losses in Segmented Solid Rocket High-Energy Turbines B94-044 Booster Rocket B94-111 Motors” B92-105 Comment on “Simple Modeling of Particle Tra- Flexible and Active Structures Noninstrusive Diagnostics jectories in Solid Rocket Motors” B91-026 Hot Dynamic Test Rig for Measuring Hyperson- Pyrometry for Turbine Applications in the Pres- Supersonic Combustion ic Engine Seal Flow and Durability B94-098 ence of Reflection and Combustion B94-126 OH Laser-Induced Fluorescence Velocimetry OH Laser-Induced Fluorescence Velocimetry Technique for Steady, High-Speed, Reacting Technique for Steady, High-Speed, Reacting Materials Structural Properties Flows B94-108 Flows B94-108 Planar KrF Laser-Induced OH Fluorescence Im- Review of Shock-Induced Supersonic Combus- Development of Hypersonic Engine Seals: Flow aging in a Supersonic Combustion Tunnel tion Research and Hypersonic Applications Effects of Preload and Engine Pressures B94-082 B94-121 B94-052 Planar KrF Laser-Induced OH Fluorescence Im- Dynamic Turbine Blade Temperature Measure- aging in a Supersonic Combustion Tunnel Structural Composite Materials ments B94-009 B94-052 Advanced Injection and Mixing Techniques for Ply Layup Optimization and Micromechanics Radiation in Participating Media Scramjet Combustors B94-024 Tailoring of Composite Aircraft Engine Struc- tures B94-123 Thermal Radiation in Gas Core Nuclear Reactors Transient Combustion and Detonation Development of Hypersonic Engine Seals: Flow for Space Propulsion B94-058 Effects of Preload and Engine Pressures Formulation, Predictions, and Sensitivity Analy- B94-121 Thermal Modeling and Analysis sis of a Pyrotechnically Actuated Pin Puller Hot Dynamic Test Rig for Measuring Hyperson- Model B94-069 ic Engine Seal Flow and Durability Dynamic Turbine Blade Temperature Measure- ments B94-009 B94-098 Space Technology Structural Durability (Including Fatigue, Thermochemistry and Chemical Kinetics Mission Trajectories (Earth and Fracture, and Environmental Degradation) Hydrogen Recombination Kinetics and Nuclear Interplanetary) Hot Dynamic Test Rig for Measuring Hyperson- Thermal Rocket Performance Prediction Stationkeeping with Two-Way Electromagnetic ic Engine Seal Flow and Durability B94-068 Launchers B94-127 B94-098 Thermophysical Properties Space Processing Structural Dynamics and Characterization Comment on “Evaluation of the Munich Method Production and Use of Metals and Oxygen for Localization of Aeroelastic Modes in Mistuned for Modeling Rocket Engine Performance” Lunar Propulsion B94-114 High-Energy Turbines B94-044 B93-029 J. PROPULSION, VOL. 10, NO. 6: 1994 INDEX Author Index Abdol-Hamid, K. S., B94-101, Fagan, J. R., Jr., B94-023 Koumandakis, M., B94-100 Niino, M., B94-037 B94-012 Favin, S., B94-083 Krauss, R. H., B94-052 Nitzsche, F., B94-048 Acker, T. L., B94-030 Fendell, F., B91-026 Kren, L. A., B94-098 Nordley, G. D., B94-127 Acosta, P., B91-026 Fernandes Pereira, J. C., B94-039 Kumar, A., B94-115 O’Brien, W. F., B94-009 Adkins, C. N., B94-093 Fleeter, S., B94-023, B94-027, Kurkov, A. P., B94-047 Okiishi, T. H., B94-011, B94-092 Aggarwal, S. K., B94-055 B94-095, B94-096, B94-097 Kuroda, Y., B94-089 Ono, F., B94-085 Ahmad, I., B94-103 Foelsche, R. O., B94-065 Kurokawa, J., B94-031 Osborn, J. R., B94-125 Alexopoulos, G. A., B94-066, Gabruk, R. S., B94-019 Kuwahara, T., B94-089 Palaszewski, B., B94-113 B94-107 Gallimore, A. D., B94-034, Lai, H. T., B94-086 Pao, S. P., B94-012 Ameri, Ali, B94-119 B94-077 Lai, W. H., B94-056 Papailiou, K. D., B94-100, Anderson, B. H., B94-091 Gauba, G., B94-108 Lakshmanan, B., B94-101 B94-122 Anderson, G. Y., B94-001 Gauntt, R. O., B94-058 Lambiris, B., B94-122 Papamoschou, D., B94-110 Anil, K. N., B94-060 Ghali, A., B94-099 Landis, G. A., B94-114 Papas, P., B94-054 Arai, T., B94-053 Ghoniem, A. F., B94-106 Laredo, D., B94-057 Parkes, J. E., B94-002 Asbury, S. C., B94-015 Glick, R. L., B92-105, B92-107 Latham, T., B94-058 Parlos, A. G., B94-035 Attia, M., B94-117, B94-118 Gollahalli, S. R., B94-103 Laufer, G., B94-052 Parthasarathy, V. N., B94-123 Ault, D. A., B94-074 Gonthier, K. A., B94-069 Lawless, P. B., B94-097 Paynter, G. C., B94-078 Auslender, A. H., B94-115 Gordon, S., B93-029 Lee, J., B94-041, B94-078 Pelaccio, D. G., B94-112 Avedisian, C. T., B94-087 Gould, R. D., B94-088 Lee, S.-T., B94-105 Perusek, G. P., B94-026 Aydelott, J. C., B94-090 Grisnik, S. P., B94-002 Lewicki, D. G., B94-049 Pierre, C., B94-044 Balakrishnan, G., B94-061 Gulati, A., B94-007, B94-022 Lewis, M. J., B94-111 Podleski, S. D., B94-116 Barankiewicz, W. S., B94-026 Gupta, A. K., B94-018, B94-087 Liang, D. W., B94-072 Poinsatte, P. E., B94-119 Baskharone, E. A., B94-099 Gysling, D. L., B94-013 Liebeck, R. H., B94-093 Powell, R., B94-113 Basu, P., B94-079 Hamed, A., B94-010 Lilley, D. G., B94-018, B94-020 Powers, J. M., B94-069 Bauer, R. C., B94-082 Handschuh, R. F., B94-049 Lin, S.-J., B94-120 Presser, C., B94-087 Baurle, R. A., B94-066, B94-107 Hardalupas, Y., B94-064 Linne, D. L., B94-114 Price, E. W., B94-105 Becker, W. J., B94-009 Harms, G. A., B94-058 Lippke, C., B94-117, B94-118 Quagliaroli, T. M., B94-052 Bensing, G. K., B94-009 Hartfield, R. J., Jr., B94-017 Litvin, F. L., B94-049 Rabinowitz, M. J., B94-084 Billig, F. S., B94-083 Hartle, M. S., B94-123 Loewenthal, R., B94-079 Rajagopalan, R. G., B94-080, Bogdanoff, D. W., B94-024, Hassan, H. A., B94-066, B94-107 Long, L. N., B94-076 B94-081 B94-071 Hedges, D. E., B94-033 Lorber, P. J., B94-028 Randolph, H., B94-104 Bond, W. H., B94-067 Heister, S. D., B94-125 Lorenzo, C. F., B94-029 Rao, K. V., B94-042, B94-043 Brent, D., B91-026 Hendricks, G. J., B94-013 Lucius, G. A., B94-051 Ray, A., B94-029 Brill, B., B94-036 Henry, Z. S., B94-049 Madavan, N. K., B94-080, Reddy, D. R., B94-091 Brooks, W. T., B92-107 Hepp, A. F., B94-114 B94-081 Reichert, B. A., B94-011, Bruns, J. E., B94-014 Hermanson, J. C., B94-054 Masuya, G., B94-037, B94-085 B94-092 Buckley, P. L., B94-065 Hingst, W. R., B94-011 Mathioudakis, K., B94-122 Resler, E. L., Jr., B94-094 Bushnell, D. M., B94-001 Hippensteele, S. A., B94-119 Mathur, S. R., B94-080, B94-081 Rhodes, J. A., B94-016 Cai, Z., B94-121 Hiraiwa, T., B94-075 Matthews, R. B., B94-059 Rizkalla, O., B94-001 Capone, F. J., B94-015 Hochstein, J. I., B94-090 McArdle, J. G., B94-016 Roby, R. J., B94-009 Carlson, J. R., B94-012 Hollo, S. D., B94-017, B94-052 McCrorie, J. D., I, B94-057 Rodgers, R. J., B94-058 Carpino, M., B94-029 Hong, C. H., B94-056 McDaniel, J. C., Jr., B94-052 Roe, L. A., B94-019, B94-109 Carta, F. O., B94-028 Hudgens Young, J. A., B94-025 McDaniel, J. C., B94-017, Roman, W., B94-058 Caveny, L. H., B92-105 Ibrahim, M. B., B94-026 B94-108 Rose, M. F., B94-004 Chaviaropoulos, P., B94-100 Inoue, K., B94-050 McDonell, V. G., B94-056, Rosenberg, S. D., B94-005 Chen, J.-Y., B94-021 Ishiguro, T., B94-075 B94-062, B94-063 Rubins, P. M., B94-082 Chen, S. H., B94-046 Jackson, E. D., B94-046 McKnight, R. L., B94-123 Rutkevich, I. M., B94-124 Chen, T. H., B94-109 Jahn, R. G., B94-034, B94-077 McMurtry, P. A., B94-021 Samuelsen, G. S., B94-056 Chen, X.-Q., B94-039 Jahnke, C. C., B94-070 Mehmed, O., B94-047 Samuelsen, S., B94-062, B94-063 Chew, L., B94-104 Jenkins, R. M., B94-004 Menon, S., B94-021 Sasoh, A., B94-032 Chinitz, W., B94-001 Johari, H., B94-104 Meserole, J. S., B94-033 Schetz, J. A., B94-053, B94-083 Chinzei, N., B94-037 Johnson, R., B94-079 Metzger, J. D., B94-035 Schobeiri, M. T., B94-117, Colvin, J. E., B94-114 Johnson, W. A., B92-105 Micci, M. M., B94-076 B94-118 Coomes, E. P., B94-059 Juhasz, A., B94-112 Miller, J. H., B94-098 Schoenman, L., B94-005 Cornelius, K. C., B94-051 Kamijo, K., B94-031, B94-038 Mitani, T., B94-075 Semerjian, H. G., B94-087 Corporan, E., B94-065 Kanda, T., B94-037, B94-085 Mitchell, C. E., B94-030 Shih, S., B94-010 Culick, F. E. C., B94-070 Kanmuri, A., B94-037 Miyajima, H., B94-089 Shimura, T., B94-031 Dai, X., B94-029 Kaplan, Z., B94-036 Miolsness, R. C., B94-090 Short, J., B94-079 Damodaran, K. A., B94-008, Kapoor, K., B94-091 Mocsari, J. C., B94-094 Sigman, R. K., B94-105 B94-060, B94-102 Kato, M., B94-050 Mond, M., B94-124 Singh, D. J., B94-025, B94-115 Datta, A., B94-079 Kay, I. W., B94-054 Morley, N. J., B94-112 Sirocky, P. J., B94-098 Day, I. J., B94-045 Keen, J. M., B94-065 Murdock, J. W., B91-026 Sloan, M. L., B94-078 Dedoussis, V., B94-100 Kelly, A. J., B94-034, B94-077 Murthy, D. V., B94-044 Slutz, S. A., B94-058 Delaney, R. A., B94-042, Kerstein, A. R., B94-021 Mutharasan, R., B94-121 Smith, C. F., B94-014 B94-043 Khan, E. U., B94-059 Myers, R. M., B94-002, B94-034 Smith, T. E., B94-044 Disimile, P. J., B94-040 Kim, K. H., B94-027, B94-096, Nagamatsu, H. T., B94-086 Solomon, W. C., B94-065, Dong, M., 894-020 B94-097 Nagao, T., B94-038 B94-068 Dunn, M. G., B94-042, B94-043 Kim, S. C., B94-003, B94-086 Najm, H. N., B94-106 Sovey, J. S., B94-002 Eastland, A. H., B94-046 Kimchi, D., B94-036 Nalim, M. R., B94-094 Sowa, W. A., B94-062, B94-063 El-Genk, M. S., B94-112 Klavuhn, K. G., B94-108 Narayanan, A. K., B94-008, Stamatis, A., B94-122 Erdos, J. 1., B94-001 Ko, F. K., B94-121 B94-102 Steinetz, B. M., B94-098, Esker, B. S., B94-016 Kodiyalam, S., B94-123 Nejad, A. S., B94-109 B94-121 Espafia, M. D., B94-073, B94-128 Korte, J. J., B94-115 Netzer, D. W., B94-057 Stevenson, W. H., B94-088 J. PROPULSION, VOL. 10,NO.6: 1994 INDEX Stubbs, R. M., B94-003 Van Wie, D. M., B94-074 Wang, W.-B., B94-006 Xiao, Y., B94-055 Suarez, E., B94-126 Vaughn, J. K., B94-057 Warren, R. E., Jr., B94-007 Yang, J.-T., B94-006 Takaki, R., B94-075 Vetrone, R. H., B94-002 Wellborn, S. R., B94-092 Yang, R.-J., B94-120 Tarpley, C., B94-111 Wadel, M. F., B94-114 Wetzel, K. K., B94-068 Yeh, F. C., B94-119 Thompson, H. D., B94-088 Waibel, R., B93-029 Whitehurst, R. B., II, B94-052 Yeuan, J. J., B94-010 Yi, A. C., B94-067 Torrey, M. D., B94-090 Wakamatsu, Y., B94-037, Whitelaw, J. H., B94-064 Yoshida, M., B94-038 Trexler, C. A., B94-025 B94-085 Williams, F. A., B94-061 Yungster, S., B94-084 Tsai, G.-L., B94-006 Wald, S., B94-036 Williams, G. J., Jr., B94-004 Zelesnik, D., B94-076 Ueda, S., B94-089 Wang, H., B94-062, B94-063 Wolff, J. M., B94-095 Zeleznik, F. J., B93-029 Van Fossen, G. J., B94-119 Wang, M. R., B94-056 Wu, M.-K., B94-029 Zhang, S. Y., B94-072 Chronological Index B91-026 Simple Modeling of Particle Trajectories in Solid B94-005 New Generation of High-Performance Engines for Rocket Motors. G. Carrier, F. Fendell, D. Brent, C. Kimbrough, Spacecraft Propulsion. Sanders D. Rosenberg and Leonard S. Loucks, E. Hess, and P. Acosta, TRW Space & Technology Schoenman, Aerojet Propulsion Division (10, 1, p. 40) Article Group (7, 2, p. 185) Article based on AIAA Paper 90-0452 based on AIAA Paper 91-2039 Technical Comment by John W. Murdock, The Aerospace Corporation (10, 3, p. 437) B94-006 Near-Wake Characteristics of Various V-Shaped Reply (10, 3, p. 438) Bluff Bodies. Jing-Tang Yang, Go-Long Tsai, and Wen-Bin Wang, National Tsing Hua University, Taiwan, ROC (10, 1, p. 47) B92-105 Method for Reducing Stagnation Pressure Losses in Article Segmented Solid Rocket Motors. W. A. Johnston, The Aerospace Corporation (8, 3, p. 720) Technical Note B94-007 NO,-Based Laser-Induced Fluorescence Technique Technical Comment by Robert L. Glick, Talley Defense Systems; to Measure Cold-Flow Mixing. A. Gulati and R. E. Warren Jr., and Leonard H. Caveny, BMDO, Pentagon (10, 2, p. 295) General Electric Company (10, 1, p. 54) Article based on AIAA Reply (10, 2, p. 296) Paper 92-0511 B94-008 Experimental Studies on Mixing of Two Co-Axial B92-107 Relationships for Motor Temperature Sensitivity. R. High-Speed Streams. A. K. Narayanan and K. A. Damodaran, Jn- E. Hamke, Thiokol Corporation; and J. R. Osborn, Purdue Univer- dian Institute of Technology (10, 1, p. 62) Article sity (8, 3, p. 723) Technical Note Technical Comment by Robert L. Glick, Talley Defense Systems; B94-009 Dynamic Turbine Blade Temperature Measure- and Wm. Ted Brooks, Hercules, Inc. (10, 5, p. 754) ments. William J. Becker, Richard J. Roby, and Walter F. O’Brien, Virginia Polytechnic Institute and State University, and Gerald K. B93-029 Evaluation of the Munich Method for Modeling Bensing, Rosemount Aerospace Division (10, 1, p. 69) Article Rocket Engine Performance. Frank J. Zeleznik, NASA Lewis Re- based on AIAA Paper 89-2689 search Center (9, 2, p. 191) Article Technical Comment by Sanford Gordon, Sanford Gordon and B94-010 Investigation of Shock/Turbulent Boundary-Layer Associates (10, 5, p. 749) Bleed Interactions. A. Hamed, S. Shih, and J. J. Yeuan, Univer- Technical Comment by R. Waibel, Federal Armed Forces Uni- sity of Cincinnati (10, 1, p. 79) Article based on AIAA Paper 92- versity, Germany (10, 5, p. 750) 3085 Reply (10, 5, p. 752) B94-011 Circular-to-Rectangular Transition Duct Flow With- B94-001 Facility Opportunities and Associated Stream Chem- out and with Inlet Swirl. Bruce A. Reichert and Warren R. Hingst, istry Considerations for Hypersonic Air-Breathing Propulsion. NASA Lewis Research Center, and Theodore H. Okiishi, Jowa State Wallace Chinitz, John I. Erdos, and Oussama Rizkalla, General University (10, 1, p. 88) Article Applied Science Laboratories, Inc.; and G. Y. Anderson and Dennis M. Bushnell, NASA Langley Research Center (10, 1, p. 6) Survey B94-012 Computational Investigation of Circular-to-Rectan- Paper based on AIAA Paper 92-3991 gular Transition Ducts. S. Paul Pao and John R. Carlson, NASA Langley Research Center, and Khaled S. Abdol-Hamid, Analytical B94-002 Test Facilities for High-Power Electric Propulsion. Services and Materials, Inc. (10, 1, p. 95) Article based on AIAA James S. Sovey, Robert H. Vetrone, and Stanley P. Grisnik, NASA Paper 91-3342 Lewis Research Center, and Roger M. Myers and James E. Parkes, Sverdrup Technology, Inc. (10, 1, p. 18) Article based on AIAA B94-013 Theoretical Study of Sensor-Actuator Schemes for Paper 91-3499 Rotating Stall Control. G. J. Hendricks and D. L. Gysling, Massa- chusetts Institute of Technology (10, 1, p. 101) Article based on B94-003 Numerical Study of Low-Pressure Concept for Nu- AIAA Paper 92-3486 clear Thermal Rockets. Suk C. Kim, Sverdrup Technology, Inc.; and Robert M. Stubbs, NASA Lewis Research Center (10, 1, p. 25) B94-014 Installed F/A-18 Inlet Flow Calculations at a High Article Angle of Attack. James E. Bruns and C. Frederic Smith, Sverdrup Technology, Inc. (10, 1, p. 110) Article based on AIAA Paper 92- B94-004 Preliminary Design of a Space Propulsion System 3175 Utilizing Stored Thermal Energy. George J. Williams Jr., Rhonald M. Jenkins, and M. Frank Rose, Auburn University (10, 1, B94-015 High-Alpha Vectoring Characteristics of the F-18/ p. 32) Article based on AIAA Paper 92-3848 HARV. Scott C. Asbury and Francis J. Capone, NASA Langley Re- 924 J. PROPULSION, VOL. 10, NO. 6: 1994 INDEX search Center (10, 1, p. 116) Article based on AIAA Paper 92-3095 B94-029 Damage-Mitigating Control of a Reusable Rocket En- gine. Asok Ray, Xiaowen Dai, Min-Kuang Wu, and Marc Carpino, B94-016 Internal Reversing Flow in a Tailpipe Offtake Config- Pennsylvania State University, and Carl F. Lorenzo, NASA Lewis uration for ASTOVL Aircraft. Jack G. McArdle and Barbara S. Research Center (10, 2, p. 225) Article Esker, NASA Lewis Research Center, and James A. Rhodes, McDonnell-Douglas Aerospace Company (10, 1, p. 122) Article B94-030 Combustion Zone—Acoustic Cavity Interactions in based on AIAA Paper 92-3790 Rocket Combustors. Thomas L. Acker and Charles E. Mitchell, Colorado State University (10, 2, p. 235) Article B94-017 Experimental Investigation of a Supersonic Swept Ramp Injector Using Laser-Induced Iodine Fluorescence. Roy B94-031 Axial Thrust Behavior in LOX-Pump of Rocket En- J. Hartfield Jr., Steven D. Hollo, and James C. McDaniel, Univer- gine. Junichi Kurokawa, Yokohama National University, Japan; sity of Virginia (10, 1, p. 129) Article based on AIAA Paper 90- and Kenjiro Kamijo and Takashi Shimura, National Aerospace 1518 Laboratory, Japan (10, 2, p. 244) Article based on AIAA Paper 91- 2410 B94-018 Combustion and Environmental Challenges for Gas Turbines in the 1990s. Ashwani K. Gupta, University of Mary- B94-032 Generalized Hall Acceleration. Akihiro Sasoh, Tohoku land; and David G. Lilley, Oklahoma State University (10, 2, p. University, Japan (10, 2, p. 251) Article 137) Survey Paper based on AIAA Paper 91-1964 B94-033 Demonstration and Evaluation of Carbon-Carbon B94-019 Velocity Characteristics of Reacting and Nonreacting Ion Optics. D. E. Hedges and J. S. Meserole, Boeing Defense and Flows in a Dump Combustor. Robert S. Gabruk, ARAP Group of Space Group (10, 2, p. 255) Article Titan Research and Technology, and Larry A. Roe, University of Arkansas (10, 2, p. 148) Article B94-034 Anode Power Deposition in an Applied-Field Seg- mented Anode MPD Thruster. A. D. Gallimore, Princeton Uni- B94-020 Inlet Velocity Profile Effects on Turbulent Swirling versity; R. M. Myers, Sverdrup Technology, Inc.; and A. J. Kelly Flow Predictions. Mingchun Dong and David G. Lilley, Okla- and R. G. Jahn, Princeton University (10, 2, p. 262) Article based homa State University (10, 2, p. 155) Article based on AIAA Paper on AIAA Paper 91-2343 93-0133 B94-035 Feasibility Study of a Contained Pulsed Nuclear Pro- B94-021 Prediction of NOx Production in a Turbulent Hydro- pulsion Engine. Alexander G. Parlos, Texas A&M University; and gen-Air Jet Flame. Suresh Menon, Georgia Institute of Technol- John D. Metzger, Grumman Aerospace & Electronics (10, 2, p. ogy; Patrick A. McMurtry, University of Utah; Alan R. Kerstein, 269) Article Sandia National Laboratories, and J.-Y. Chen, University of Cali- fornia, Berkeley (10, 2, p. 161) Article based on AIAA Paper 92- B94-036 Experimental Demonstration and Simulation of a 0233 Dual-Stage Solid Propellant Gun Concept. Boaz Brill, Shlomo Wald, David Kimchi, and Zvi Kaplan, Soreq Nuclear Research B94-022 Raman Measurements at the Exit of a Combustor Center, Israel (10, 2, p. 279) Article Sector. Anil Gulati, General Electric Corporate Research and De- velopment Center (10, 2, p. 169) Article based on AIAA Paper 92- B94-037 Effect of Regenerative Cooling on Rocket Engine 3350 Specific Impulse. Takeshi Kanda, Goro Masuya, Yoshio Wakamatsu, Akio Kanmuri, Nobuo Chinzei, and Masayuki Niino, B94-023 Comparison of Optical Measurement Techniques for National Aerospace Laboratory, Japan (10, 2, p. 286) Technical Turbomachinery Flowfields. John R. Fagan Jr. and Sanford Note Fleeter, Purdue University (10, 2, p. 176) Article based on AIAA Paper 89-2572 B94-038 Performance Evaluation of LE-7 High-Pressure Pumps. Kenjiro Kamijo and Makoto Yoshida, National Aerospace B94-024 Advanced Injection and Mixing Techniques for Laboratory, Japan; and Takaharu Nagao, National Space Devel- Scramjet Combustors. David W. Bogdanoff, Eloret Institute (10, opment Agency of Japan (10, 2, p. 288) Technical Note 2, p. 183) Article B94-039 Numerical Prediction of a Turbulent Evaporating B94-025 Three-Dimensional Simulation of a Translating Strut Fuel Spray in a Recirculating Flow. Xi-Qing Chen and José Car- Inlet. D. J. Singh, Analytical Services and Materials, Inc.; Carl A. los Fernandes Pereira, /nstituto Superior Técnico/Technical Uni- Trexler, NASA Langley Research Center, and Julie A. Hudgens versity of Lisbon, Portugal (10, 2, p. 290) Technical Note Young, Analytical Services and Materials, Inc. (10, 2, p. 191) Ar- ticle based on AIAA Paper 92-0270 B94-040 Effect of Impinging Jet Excitation on Curved Surface Heat Transfer. P. J. Disimile, University of Cincinnati (10, 2, p. B94-026 Approximate Similarity Principle for a Full-Scale 293) Technical Note STOVL Ejector. Wendy S. Barankiewicz and Gail P. Perusek, NASA Lewis Research Center, and Mounir B. Ibrahim, Cleveland B94-041 Numerical Study of Mixing in Supersonic Combus- State University (10, 2, p. 198) Article based on AIAA Paper 92- tors with Hypermixing Injectors. J. Lee, Sverdrup Technology, 3792 Inc. (10, 3, p. 297) Article B94-027 Forcing Function Generator Fluid Dynamic Effects B94-042 Vane-Blade Interaction in a Transonic Turbine, Part on Compressor Blade Gust Response. Kuk H. Kim and Sanford I: Aerodynamics. K. V. Rao and R. A. Delaney, Allison Gas Tur- Fleeter, Purdue University (10, 2, p. 204) Article based on AIAA bine Division, and M. G. Dunn, Calspan Advanced Technology Paper 93-0157 Center (10, 3, p. 305) Article based on AIAA Paper 92-3323 B94-028 Incipient Torsional Stall Flutter Aerodynamic Exper- B94-043 Vane-Blade Interaction in a Transonic Turbine, Part iments on Three-Dimensional Wings. Peter J. Lorber and Frank- II: Heat Transfer. K. V. Rao and R. A. Delaney, Allison Gas Tur- lin O. Carta, United Technologies Research Center (10, 2, p. 217) bine Division, and M. G. Dunn, Calspan Advanced Technology Article based on AIAA Paper 91-0935 CP911 Center (10, 3, p. 312) Article J. PROPULSION, VOL .. 10, NO. 6: 1994 INDEX 925 B94-044 Localization of Aeroelastic Modes in Mistuned High- Ward Roman, and Richard J. Rodgers, United Technologies Re- Energy Turbines. Christophe Pierre, University of Michigan; search Center (10, 3, p. 419) Article Todd E. Smith, Sverdrup Technology, Inc.; and Durbha V. Murthy, University of Toledo (10, 3, p. 318) Article based on AIAA Paper B94-059 Hierarchical Analysis of Options for Lunar-Surface 91-3379 Power. R. Bruce Matthews, Los Alamos Laboratory, Edmund P. Coomes, Pacific Northwest Laboratory, and Ehsan U. Khan, De- B94-045 Axial Compressor Performance During Surge. I. J. partment of Energy (10, 3, p. 425) Article Day, University ofC ambridge, England, UK (10, 3, p. 329) Article B94-060 Preliminary Investigations on Improving Air- B94-046 Efficient Method for Predicting Rotor/Stator Inter- Augmented Rocket Performance. K. N. Anil and K. A. Damo- action. S. H. Chen, A. H. Eastland, and E. D. Jackson, Rockwell daran, Indian Institute of Technology (10, 3, p. 432) Technical Note International Corporation (10, 3, p. 337) Article B94-061 Turbulent Combustion Regimes for Hypersonic Pro- B94-047 Experimental Investigation of Counter-Rotating pulsion Employing Hydrogen-Air Diffusion Flames. G. Bala- Propfan Flutter at Cruise Conditions. Oral Mehmed and Anatole krishnan and F. A. Williams, University of California, San Diego P. Kurkov, NASA Lewis Research Center (10, 3, p. 343) Article (10, 3, p. 434) Technical Note based on AIAA Paper 93-1634 CP931 B94-062 Experimental Study of a Model Gas Turbine Com- B94-048 Dynamic Aeroelastic Stability of Vertical-Axis Wind bustor Swirl Cup, Part I: Two-Phase Characterization. Hongyu Turbines Under Constant Wind Velocity. Fred Nitzsche, DLR, Wang, Vincent G. McDonell, William A. Sowa, and Scott Sam- German Aerospace Research Establishment, Germany (10, 3, p. uelsen, University of California, Irvine (10, 4, p. 441) Article 348) Article B94-063 Experimental Study of a Model Gas Turbine Com- B94-049 Low-Noise, High-Strength, Spiral-Bevel Gears for bustor Swirl Cup, Part II: Droplet Dynamics. Hongyu Wang, Helicopter Transmission. David G. Lewicki and Robert F. Hand- Vincent G. McDonell, William A. Sowa, and Scott Samuelsen, schuh, NASA Lewis Research Center, Zachary S. Henry, Bell Heli- University of California, Irvine (10, 4, p. 446) Article copter Textron, Inc.; and Faydor L. Litvin, University of Illinois at Chicago (10, 3, p. 356) Article based on AIAA Paper 93-2149 B94-064 Characteristics of Sprays Produced by Coaxial Air- blast Atomizers. Y. Hardalupas and J. H. Whitelaw, /mperial Col- B94-050 Estimation of Fatigue Strength Enhancement for lege of Science, Technology and Medicine, England, UK (10, 4, p. Carburized and Shot-Peened Gears. Katsumi Inoue and Masana 453) Article based on AIAA Paper 93-0698 Kato, Tohoku University, Japan (10, 3, p. 362) Article based on AIAA Paper 93-2294 B94-065 Nonequilibrium Combustion Model for Fuel-Rich Gas Generators. Robert O. Foelsche, Joseph M. Keen, and Wayne B94-051 Multiple Hole Ejector Performance with Short Wide C. Solomon, University of Illinois at Urbana-Champaign, and Angle Diffusers. Kenneth C. Cornelius and Gerald A. Lucius, Parker L. Buckley and Edwin Corporan, Wright-Patterson Air Wright State University (10, 3, p. 369) Article Force Base (10, 4, p. 461) Article based on AIAA Paper 93-2041 B94-052 Planar KrF Laser-Induced OH Fluorescence Imaging B94-066 Assumed Joint Probability Density Function Ap- in a Supersonic Combustion Tunnel. T. M. Quagliaroli, G. proach for Supersonic Turbulent Combustion. R. A. Baurle, G. Laufer, S. D. Hollo, R. H. Krauss, R. B. Whitehurst III, and J. C. A. Alexopoulos, and H. A. Hassan, North Carolina State University McDaniel Jr., University of Virginia (10, 3, p. 377) Article based on (10, 4, p. 473) Article based on AIAA Paper 92-3844 AIAA Paper 92-3346 B94-067 Air Liquefaction and Enrichment System Propulsion B94-053 Injection of Bubbling Liquid Jets from Multiple In- in Reusable Launch Vehicles. W. H. Bond and A. C. Yi, Rockwell jectors into a Supersonic Stream. Takakage Arai and Joseph A. International Corporation (10, 4, p. 485) Article based on AIAA Schetz, Virginia Polytechnic Institute and State Universi(t1y0, 3, p. Paper 93-2025 382) Article based on AIAA Paper 92-5060 B94-054 Structure and Penetration of a Supercritical Fluid Jet B94-068 Hydrogen Recombination Kinetics and Nuclear in Supersonic Flow. J. C. Hermanson, P. Papas, and I. W. Kay, Thermal Rocket Performance Prediction. Kyle K. Wetzel and United Technologies Research Center (10, 3, p. 387) Article Wayne C. Solomon, University of Illinois at Urbana-Champaign (10, 4, p. 492) Article based on AIAA Paper 93-2499 B94-055 Effect of External Forcing on Droplet Dispersion in a Developing Shear Layer. S. K. Aggarwal and Y. Xiao, University B94-069 Formulation, Predictions, and Sensitivity Analysis of of Illinois at Chicago (10, 3, p. 395) Article a Pyrotechnically Actuated Pin Puller Model. Keith A. Gonthier and Joseph M. Powers, University of Notre Dame (10, 4, p. 501) B94-056 Interlaboratory Comparison of Phase Doppler Meas- Article urements in a Research Simplex Atomizer Spray. V.G. Mc- Donell and G. S. Samuelsen, University of California, Irvine; and B94-070 Application of Dynamical Systems Theory to Non- M. R. Wang, C. H. Hong, and W. H. Lai, National Cheng Kung linear Combustion Instabilities. Craig C. Jahnke, Clarkson Uni- University, Taiwan, ROC (10, 3, p. 402) Article based on AIAA versity; and F. E. C. Culick, California Institute of Technology (10, Paper 92-3233 4, p. 508) Article based on AIAA Paper 93-0114 B94-057 Motor and Plume Particle Size Measurements in B94-071 New Tube End Closure System for the Ram Ac- Solid Propellant Micromotors. D. Laredo, J. D.M cCrorie II, J. celerator. David W. Bogdanoff, Eloret Institute (10, 4, p. 518) K. Vaughn, and D. W. Netzer, Naval Postgraduate School (10, 3, Article p. 410) Article B94-072 Improved Method for Estimation of the Maximum B94-058 Thermal Radiation in Gas Core Nuclear Reactors for Instantaneous Distortion Values. D. W. Liang and S. Y. Zhang, Space Propulsion. Stephen A. Slutz, Randall O. Gauntt, and Gary Nanjing University of Aeronautics and Astronautics, PRC (10, 4, p. A. Harms, Sandia National Laboratories, and Thomas Latham, 522) Article 926 J. PROPULSION, VOL .. 10, NO. 6: 1994 INDEX B94-073 Sensor Biases Effect on the Estimation Algorithm for Layer Ingestion. Hien T. Lai and Suk C. Kim, Sverdrup Tech- Performance-Seeking Controllers. Martin D. Espafia, National nology, Inc.; and Henry T. Nagamatsu, Rensselaer Polytechnic In- Research Council/NASA Dryden Flight Research Facility (10, 4, p. stitute (10, 5, p. 625) Article 527) Article based on AIAA Paper 93-1823 B94-087 Droplet Transport in a Swirl-Stabilized Spray Flame. B94-074 Experimental and Computational Results for the Ex- C. Presser, A. K. Gupta, H. G. Semerjian, and C. T. Avedisian, ternal Flowfield of a Scramjet Inlet. D. A. Ault and D. M. Van National Institute of Standards and Technology (10, 5, p. 631) Wie, Johns Hopkins University Applied Physics Laboratory (10, 4, Article p. 533) Article based on AIAA Paper 92-5100 B94-088 Simultaneous Velocity and Temperature Measure- B94-075 Three-Dimensional Analysis of Scramjet Nozzle ments in a Premixed Dump Combustor. Richard D. Gould, Flows. Tomiko Ishiguro and Ryouji Takaki, National Aerospace North Carolina State University, and Warren H. Stevenson and H. Laboratory, Japan; and Tohru Mitani and Tetsuo Hiraiwa, Kakuda Doyle Thompson, Purdue University (10, 5, p. 639) Article Research Center, Japan (10, 4, p. 540) Article based on AIAA Paper 93-5059 B94-089 Bipropellant Performance of NjJH,/MMH Mixed Fuel in a Regeneratively Cooled Engine. Shuichi Ueda, Yukio Kur- B94-076 Direct Simulation Monte Carlo Model of Low Rey- oda, and Hiroshi Miyajima, National Aerospace Laboratory, Ka- nolds Number Nozzle Flows. Donna Zelesnik, Michael M. Micci, kuda Research Center, Japan; and Takuo Kuwahara, Nissan Motor and Lyle N. Long, Pennsylvania State University (10, 4, p. 546) Co., Ltd., Japan (10, 5, p. 646) Article Article B94-090 On-Orbit Propellant Motion Resulting from an Im- B94-077 Use of Permanent Magnets to Reduce Anode Losses pulsive Acceleration. John I. Hochstein, Memphis State Univer- in MPD Thrusters. A. D. Gallimore, A. J. Kelly, and R. G. Jahn, sity; John C. Aydelott, NASA Lewis Research Center, and Raymond Princeton University (10, 4, p. 554) Article based on AIAA Paper C. Mijolsness and Martin D. Torrey, Los Alamos National Lab- 92-3461 oratory (10, 5, p. 653) Article B94-078 Lag Model for Turbulent Boundary Layers over B94-091 Study on Computing Separating Flows Within a Dif- Rough Bleed Surfaces. J. Lee, M. L. Sloan, and G. C. Paynter, fusing Inlet S-Duct. B. H. Anderson, D. R. Reddy, and K. Kapoor, Boeing Commercial Airplane Group (10, 4, p. 562) Article based NASA Lewis Research Center (10, 5, p. 661) Article based on AIAA on AIAA Paper 93-2988 Paper 93-2154 B94-079 Hysteresis and Bristle Stiffening Effects in Brush B94-092 Study of the Compressible Flow in a Diffusing S-Duct. Seals. P. Basu, A. Datta, R. Loewenthal, and J. Short, EG&G Fluid Steven R. Wellborn, Jowa State University; Bruce A. Reichert, Components Technology Group, and R. Johnson, EG&G Sealol NASA Lewis Research Center, and Theodore H. Okiishi, /owa State (10, 4, p. 569) Article based on AIAA Paper 93-1996 University (10, 5, p. 668) Article based on AIAA Paper 92-3622 B94-080 Solution-Adaptive Structured-Unstructured Grid B94-093 Design of Optimum Propellers. Charles N. Adkins; Method for Unsteady Turbomachinery Analysis, Part I: Meth- and Robert H. Liebeck, Douglas Aircraft Company (10, 5, p. 676) odology. Sanjay R. Mathur, Jowa State University, Nateri K. Mad- Article based on AIAA Paper 83-0190 avan, NASA Ames Research Center, and R. Ganesh Rajagopalan, Iowa State University (10, 4, p. 576) Article based on AIAA Paper B94-094 Analytic Design Methods for Wave Rotor Cycles. Ed- 93-0387 win L. Resler Jr., Jeffrey C. Mocsari, and M. Razi Nalim, Cornell University (10, 5, p. 683) Article based on AIAA Paper 93-2523 B94-081 Solution-Adaptive Structured-Unstructured Grid Method for Unsteady Turbomachinery Analysis, Part II: Re- B94-095 Single-Passage Euler Analysis of Oscillating Cascade sults. Sanjay R. Mathur, Jowa State University, Nateri K. Mada- Aerodynamics for Arbitrary Interblade Phase. James M. Wolff van, NASA Ames Research Center, and R. Ganesh Rajagopalan, and Sanford Fleeter, Purdue University (10, 5, p. 690) Article based lowa State University (10, 4, p. 585) Article based on AIAA Paper on AIJAA Paper 93-0389 93-3015 B94-096 Compressor Unsteady Aerodynamic Response to Ro- B94-082 Review of Shock-Induced Supersonic Combustion tating Stall and Surge Excitations. Kuk H. Kim and Sanford Research and Hypersonic Applications. P. M. Rubins, En- Fleeter, Purdue University (10, 5, p. 698) Article gineering Management Consultants, and R. C. Bauer, Arvin/ Calspan Corporation (10, 5, p. 593) Article based on AIAA Paper B94-097 Characterization of Abrupt Rotating Stall Initiation 93-2326 in an Axial Flow Compressor. Patrick B. Lawless, Kuk H. Kim, and Sanford Fleeter, Purdue University (10, 5, p. 709) Article based B94-083 Analysis of External Burning on Inclined Surfaces in on AIAA Paper 93-2238 Supersonic Flow. J. A. Schetz, F. S. Billig, and S. Favin, Johns Hopkins Universit(1y0 , 5, p. 602) Article based on AIAA Paper 91- B94-098 Hot Dynamic Test Rig for Measuring Hypersonic En- 2390 gine Seal Flow and Durability. Jeffrey H. Miller, Sverdrup Tech- nology, Inc.; Bruce M. Steinetz, NASA Lewis Research Center, Paul B94-084 Computation of Shock-Induced Combustion Using a J. Sirocky, Sverdrup Technology, Inc.; and Lawrence A. Kren, Case Detailed Methane-Air Mechanism. Shaye Yungster and Martin Western Reserve University (10, 5, p. 716) Article based on AIAA J. Rabinowitz, NASA Lewis Research Center (10, 5, p. 609) Article Paper 93-1346 CP931 based on AIAA Paper 93-1917 B94-099 Theoretical vs Experimental Rotordynamic Coef- B94-085 Effect of Film Cooling/Regenerative Cooling on ficients of Incompressible Flow Labyrinth Seals. E. A. Scramjet Engine Performances. Takeshi Kanda, Goro Masuya, Baskharone and A. Ghali, Texas A&M University (10, 5, p. 721) Fumiei Ono, and Yoshio Wakamatsu, National Aerospace Lab- Article oratory, Kakuda Research Center, Japan (10, 5, p. 618) Article B94-100 Design of Axisymmetric Channels with Rotational B94-086 Calculation of Scramjet Inlet with Thick Boundary- Flow. M. Koumandakis, V. Dedoussis, P. Chaviaropoulos, and K.