Table Of Content

JOURNAL OF AIRCRAFI Vol. 29, No. 6, Nov.—Dec. 1992 1992 Journal of Aircraft Index How to Use the Index In the Subject Index, pages 1145-1150 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 1151-1152, lists all authors associated with a given technical paper. The locating numbers are identical to those in the Subject Index. The Chronological Index, pages 1153-1159, lists all papers by their unique code 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, 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 1992, that paper also will appear in both the Subject and Chronological Indexes. Authors of Comments also are listed in the Author Index. JOURNAL OF AIRCRAFI Vol. 29, No. 6, Nov.—Dec. 1992 1992 Journal of Aircraft Index How to Use the Index In the Subject Index, pages 1145-1150 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 1151-1152, lists all authors associated with a given technical paper. The locating numbers are identical to those in the Subject Index. The Chronological Index, pages 1153-1159, lists all papers by their unique code 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, 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 1992, that paper also will appear in both the Subject and Chronological Indexes. Authors of Comments also are listed in the Author Index. J. AIRCRAFT, VOL. 29, NO. 6: 1992 INDEX Subject Index Aircraft Technology, Conventional, Experimental Study of Vortex Flows over Correction of Sideslip-Induced Static Pres- STOL/VTOL Delta Wings in Wing-Rock Motion sure Errors in Flight-Test Measurements C92-091 92-016 Aerodynamics Prediction of Inviscid Supersonic/Hyper- Rapid Prediction of High-Alpha Unsteady Buffet Excitation of Wings at Low Speeds sonic Aircraft Flowfields 92-089 Aerodynamics of Slender-Wing Aircraft 92-182 Navier-Stokes Predictions for the F-18 Wing 92-012 Transonic Low-Reynolds Number Airfoils and Fuselage at Large Incidence C92-087 Navier-Stokes Calculations of Inboard Stall C92-178 Establishing a Database for Flight in the Delay Due to Rotation 92-010 Wind-Tunnel Investigation of a Fighter Wakes of Structures 92-086 Hot Gas Environment Around STOVL Air- Model at High Angles of Attack C92-176 Flow over a Twin-Tailed Aircraft at Angle of craft in Ground Proximity—Part 1: Ex- Sources of High Alpha Vortex Asymmetry at Attack, Part Ii: Temporal Characteristics perimental Study 92-009 Zero Sideslip 92-175 92-085 Efficient Panel Method for Vortex Sheet Multigrid Euler Calculations over Complete Accurate Prediction of Drag Using Euler Roll-Up 92-004 Aircraft (92-174 Methods 92-077 Minimum Induced Drag for Wings with Aerodynamic Shape Design and Optimiza- Effect of Thrust Vectoring on Level-Turn Spanwise Camber 90-108 tion: Status and Trends 92-165 Performance 92-074 Improved Calculation of Transonic Potential Improved Measurement of the Dynamic Aeroelasticity and Aeroservoelasticity Flow Past Swept Wings 92-154 Loads Acting on Rotating Parachutes Flight Measurements of Downwash on the 92-067 Demonstration of Structural Optimization Ball-Bartoe Jetwing Powered Lift Aircraft Downwash for Joined-Wing Airframe with Applied to Wind-Tunnel Model Design 92-149 Control Surface Defiections 92-066 (92-156 Application of Computational Fluid Dy- Wake Effects on the Prediction of Transonic Flutter and Stall Response of a Helicopter namics to Sonic Boom Near- and Mid- Viscous Flows Around Airfoils (92-063 Blade with Structural Nonlinearity Field Prediction 92-148 Drag Reduction of Bluff Bodies Through 92-153 Small Two-Dimensional Surface Excres- Momentum Injection 92-062 Multidisciplinary Optimization of Aeroservo- cences on Aircraft Wings Approaching Flow over a Twin-Tailed Aircraft at Angle of elastic Systems Using Reduced-Size Separation 92-145 Attack Part I: Spatial Characteristics Models 92-151 Viscous Flow Simulation of a Fighter Air- 92-060 Dynamic Analysis of Rotor Blades with Root craft 92-143 Prediction of Vortex Shedding from Fore- Retention Design Variations 92-131 Two-Fence Concept for Efficient Trapping bodies with Chines 92-059 Aeroelastic Effects of Spoiler Surfaces on a of Vortices on Airfoils 92-140 Identification of the Transfer Function Be- Low-Aspect-Ratio Rectangular Wing Euler/Experiment Correlation of a Generic tween Turbulence and Aircraft 92-057 92-129 Fighter (92-139 Extension and Validation of an Unsteady Design Load Predictions on a Fighter-Like Navier-Stokes Simulation of a Close-Coupled Wake Model for Rotors 92-055 Aircraft Wing 92-101 Canard-Wing-Body Configuration C92-138 Unsteady Aerodynamic Loading Produced Navier-Stokes Computations on Swept-Ta- Forcing Level Effects of Internal Acoustic by a Sinusoidally Oscillating Delta Wing pered Wings, Including Flexibility Excitation on the Improvement of Airfoil 92-054 92-090 Performance 92-137 Design Optimization of Natural Laminar Structural and Aerodynamic Data Trans- Direct Simulation of Low-Density Flow over Flow Bodies in Compressible Flow formation Using Inverse Isoparametric Airfoils 92-134 C92-050 Mapping 92-073 Effect of Nose-Boom on Forebody Vortex Design and Development of a Compressible Coalescence of Aeroelastic Modes in Flutter Flow 92-122 Dynamic Stall Facility 92-046 Analysis 92-072 Thin-Airfoil Correction for Panel Methods Data Analysis for Unsteady Turbulence Transonic Aeroelasticity Analysis for Rotor 92-115 Measurements over Airfoils 92-045 Blades 92-069 Pitch Rate/Sideslip Effects on Leading-Edge Analysis of Airship Lateral Maneuverability Application of Active Flexible Wing Tech- Extension Vortices of an F/A-18 Aircraft 92-043 nology to the Agile Falcon 92-064 Model 92-114 Subsonic and Transonic Low-Reynolds- Extension and Validation of an Unsteady Minimizing Supersonic Wave Drag with Number Airfoils with Reduced Pitching Wake Model for Rotors 92-055 Physical Constraints at Design and Off- Moments 92-042 Dynamics of an Optimized Rotor Blade at Design Mach Numbers 92-112 Use of Shear-Sensitive Liquid Crystals for Off-Design Flight Conditions 92-041 Optimum Cruise Lift Coefficient in Initial Surface Flow Visualization 92-040 Integrated Aeroelastic Control Optimization Design of Jet Aircraft 92-110 Controlled Opening Method for Clustered of Laminated Composite Lifting Surfaces Time-Average Loading on a Two-Dimen- Parachutes 92-037 92-039 sional Airfoil in Large Amplitude Motion Ground-Testing Techniques for Tethered Transonic Aeroelasticity Analysis Using 92-109 Systems 92-035 State-Space Unsteady Aerodynamic Mod- Unsteady Crossflow on a Delta Wing Using Navier-Stokes Methods to Predict Circula- eling 92-022 Particle Image Velocimetry 92-108 tion Control Airfoil Performance C92-034 Nonlinear Flutter of Two-Dimensional Sim- Self-Induced Roll Oscillations of Low-As- Experimental Study of a Low Reynolds ply Supported Symmetric Composite Lam- pect-Ratio Rectangular Wings 92-106 Number Tandem Airfoil Configuration inated Plates 92-020 Forebody Vortex Control Using Small, Ro- 92-032 NASA Investigation of a Claimed ’Overlap’ tatable Strakes 92-102 Numerical Computation of Improved Tran- between Two Gust Response Analysis Design Load Predictions on a Fighter-Like sonic Potential Method 92-025 Methods 90-105 Aircraft Wing 92-101 Transonic Aeroelasticity Analysis Using Canard-Wing Interaction in Unsteady Su- Simulation of Transonic Flow over Twin-Jet State-Space Unsteady Aerodynamic Mod- personic Flow 89-155 Transport Aircraft 92-097 eling 92-022 Flight Deck Aerodynamics of a Nonaviation Separation Control Using Moving Surface Aerospace Plane Ship 92-094 Effects: A Numerical Simulation C92-019 Aerodynamic Forces on Noncircular Cross- Suppression of the Wing-Body Junction Acoustic Testing of High-Temperature Section Missile Forebodies 92-093 Vortex by Body Surface Suction C92-017 Panels (92-181 1146 J. AIRCRAFT, VOL. 29, NO. 6: 1992 INDEX Numerical Simulation of Re-Entry Flow Fuels and Fuel Systems Fighter Agility Metrics, Research and Test Around the Space Shuttle with Finite-Rate 92-065 Chemistry 092-199 Thermal t for a Mach 5 Cruise Control Strategy for Maximizing Reconnais- Aircraft Using EndotheFurelm Ci92c-05 6 sance Range of Hypersonic Cruise Vehi- Civil Missions and Transportation General Aviation cles 92-053 Preliminary Sizing Methodology for Hyper- Effects of Higher Harmonic Control on sonic Vehicles 92-024 Model Flight Tests of a Spin-Resistant Rotor Performance and Control Loads On the Threshold—The Outlook for Super- Trainer Configuration 92-133 92-049 sonic and Hypersonic Aircraft 92-002 Wing Mass Formula for Subsonic Aircraft Dynamics of an Optimized Rotor Blade at 92-116 Off-Design Flight Conditions 92-041 Communaind cAira Ttrafific oConntr ol Effect of Wind Shear on Airspeed po Agility as a Contrtio bDesuigtn Boalranc e Airplane Landing Approach 92-005 Microwave Landing System Modeling with Application to Air Traffic Control Au- Landing Dynamics Powerplant Integration tomation (92-051 Analytical Modeling of SH-2F Helicopter Optimized Scramjet Integration on a Wave- Configuration Design Shipboard Operation 92-142 rider 92-179 Whirl-Flutter Stability of a Pusher Config- Self-Compensating Carrier Aircraft Recovery Optimized Scramjet Integration on a Wave- System 92-029 uration in Nonuniform Flow 92-117 rider 92-179 Propaned lRotlor eSysrte ms Aerodynamic Shape Design and Optimiza- Lighter-Than-Air-Systems tion: Status and Trends 92-165 Propeller Slip-Stream Model in Subsonic Wing Mass Formula for Twin Fuselage Analysis of Airship Lateral Maneuverability Linearized Potential Flow (92-177 Aircraft (92-146 C92-043 Effects of Fuselage Boundary Layer on Application of Advanced Multidisciplinary Noise Propagation from Advanced Pro- Analysis and Optimization Methods to Man/ Machine Interface pellers 92-163 Vehicle Design Synthesis 92-135 Expert System for Real-Time Aircraft Mon- Dynamic Analysis of Rotor Blades with Root Minimizing Supersonic Wave Drag with itoring 092-011 Retention Design Variations 92-131 Physical Constraints at Design and Off- Whirl-Flutter Stability of a Pusher Config- Design Mach Numbers 92-112 Military Missions uration in Nonuniform Flow 92-117 Optimum Cruise Lift Coefficient in Initial Noise of Two High-Speed Model Counter- Design of Jet Aircraft 92-110 Advanced Pneumatic Impulse Ice Protection Rotation Propellers at Takeoff/Approach System (PIIP) for Aircraft 92-111 Downwash for Joined-Wing ep with Conditions 92-103 Control Surface Deflections Maximizing Thrust-Vectoring Control Power Predicted Pressure Distribution on a Prop- and Agility Metrics 92-098 Design Optimization of Natural waier Fan Blade Through Euler Analysis Flow Bodies in Compressible Flow EstWaabkleissh inogf Sat ruDcattuarbeass e for Flight ain 92-095 C92-050 Structure-Borne Noise Transmission in the Agliy as& Contributor toDe signB alance On the Threshold—The Outlook for Super- Propfan Test Assessment Aircraft sonic and Hypersonic Aircraft (92-002 92-071 On the Threshold—The Outlook for = Compact Dynamometer System That Can Deceleration Systems sonic and Hypersonic Aircraft (92-002 Accurately Determine Propeller Perform- Noise ance 92-001 Nine-Degree-of-Freedom Simulation of Ro- tating Parachute Systems 92-130 Sonic Boom Environment Under a Super- Rotorcraft Improved Measurement of the Dynamic sonic Military Operating Area 92-172 Spinning Mode Analysis of the Acoustic Loads Acting on Rotating Parachutes Effects of Fuselage Boundary Layer on Field Generated by a Turboshaft Engine 92-067 Noise Propagation from Advanced Pro- (92-173 Controlled Opening Method for Clustered pellers 92-163 Flutter and Stall Response of a Helicopter Parachutes 92-037 Mitigation of Pressure Oscillations Induced Blade with Structural Nonlinearity Self-Compensating Carrier Aircraft Recovery by Supersonic Flow over Slender Cavities 92-153 System 92-029 92-162 Dynamic Analysis of Rotor Blades with Root Ground Impingement Noise of Supersonic Retention Design Variations 92-131 Economics Jets from Nozzles with Various Exit Ge- Approach for Analysis and Design of Com- ometries 92-161 posite Rotor Blades 92-105 Software Reliability for Flight Crew Training Application of Computational Fluid Dy- “i> Deck Aerodynamics of a Nonaviation Simulators 92-052 namics to Sonic Boom Near- and Mid- 92-094 Field Prediction 92-148 Pigs,M odel for Unmanned Simulated Hel- Flight Mechanics Experimental Study of Noise Generation and icopters (92-080 Propagation in a Turbofan Model Transonic Aeroelasticity Analysis for Rotor Unsteady Wind-Tunnel Interference in Air- 92-144 Blades 92-069 craft Dynamic Experiments 92-180 Evaluation of Discrete Frequency Sound in Extension and Validation of an Unsteady Escape Strategies for Turboprop Aircraft in Closed-Test-Section Wind Tunnels Wake Model for Rotors 92-055 Microburst Windshear 92-126 92-127 Effects of Higher Harmonic Control on Optimization of Constant Altitude—Con- Noise of Two High-Speed Model Counter- Rotor Performance and Control Loads stant Airspeed Flight of Turbojet Aircraft Rotation Propellers at Takeoff/Approach 92-049 92-119 Conditions 92-103 Navier-Stokes Calculations of Inboard Stall Wing Design for Hanggliders Having Min- Structure-Borne Noise Transmission in the Delay Due to Rotation 92-010 imum Induced Drag C92-118 Propfan Test Assessment Aircraft Safety Reconstruction of Flight Path in Turbulence 92-071 92-081 Escape Strategies for Turboprop Aircraft in Effect of Thrust Vectoring on Level-Turn Performance Microburst Windshear 92-126 Performance 92-074 Wing Mass Formula for Twin Fuselage Advanced Pneumatic Impulse Ice Protection Fighter Agility Metrics, Research and Test Aircraft 92-146 System (PIIP) for Aircraft O27-111 92-065 Optimization of Constant Altitude—Con- Range, Energy, Heat of Motion in the Agility as a Contrtio bDesuigtn oBalran ce stant Airspeed Flight of Turbojet Aircraft Modified NBC, Anti-g, Tank Suit 92-005 C92-119 92-099 Flight Model for Unmanned Simulated Hel- Effects of Ambient Turbulence on the Decay Flight Operations icopters 92-080 of a Trailing Vortex Wake (92-036 Flight Deck Aerodynofa a mNoinavciastio n Effect of Thrust Vectoring on Level-Turn Effect of Wind Shear on Airspeed i Ship 92-094 Performance 92-074 Airplane Landing Approach (92.933 J. AIRCRAFT, VOL. 29, NO. 6: 1992 INDEX Heat Transfer on Accreting Ice Surfaces Evaluation of Discrete Frequency Sound in Fluid Dynamics 92-015 Closed-Test-Section Wind Tunnels Forward-Look Wind-Shear Detection for 92-127 Aeroacoustics Microburst Recovery 92-008 Wind-Tunnel Compressor Stall Monitoring Using Neural Networks 92-121 Sonic Boom Environment Under a Super- Simulation Unsteady Crossflow on a Delta Wing Using sonic Military Operating Area 92-172 ting Lags in Head-Coupled Dis- Particle Image Velocimetry 92-108 Mitigation of Pressure Oscillations Induced plays Using Head Position Prediction and Airdata Calibration Techniques for Meas- by Supersonic Flow over Slender Cavities Image Deflection 92-171 uring Atmospheric Wind Profiles 92-096 92-162 Flight Model for Unmanned Simulated Hel- Remote Measurements of Supercooled In- Ground Impingement Noise of Supersonic tegrated Liquid Water During WISP/FAA Jets from Nozzles with Various Exit Ge- Robicuosptt erFsl ight Reconstruction for Heli9c2o-p0t8e0r Aircraft Icing Program 92-092 ometries 92-161 Flow over 2 Twin-Tailed Aircraft at Angle of Experimental Study of Noise Generation and Simulation and Training 92-061 Attack, Part II: Temporal Characteristics Propagation in a Turbofan Model Software Reliability for Flight Crew — Simulators 92-085 (92-144 Self-Compensating Carrier Aircraft icone. Calibration-Related Pseudo-Reynolds Num- Suppression of Fatigue-Inducing Cavity System 92-929 ber Trends in Transonic Wind Tunnels Acoustic Modes in Turbofan Engines Forward-Look Wind-Shear Detection for 92-084 92-113 Structure-Borne Noise Transmission in the Noise of Two High-Speed Model Counter- Microburst Recovery 92-008 Propfan Test Assessment Aircraft Rotation Propellers at Takeoff/Approach STOL/VTOL/STOVL 92-071 Conditions 92-103 Fighter Agility Metrics, Research and Test Ground Impingement Noise of Supersonic Boundary Layers and Heat 92-065 Jets from Nozzles with Various Exit Ge- Flow over a Twin-Tailed Aircraft at Angle of Transfer—Laminar ometries C92-161 Attack Part I: Spatial Characteristics Three-Dimensional Simulation of Electro- Flight Measurements of Downwash on the C92-060 thermal Deicing Systems 92-167 Ball-Bartoe Jetwing Powered Lift Aircraft Software Reliability for Flight Crew Training Heat Transfer Peculiarities in Supersonic 92-149 Simulators 92-052 Flows 92-158 Navier-Stokes Methods to Predict Circula- Ground-Testing Techniques for Tethered Heat Transfer Effects on Aerodynamics and tion Control Airfoil Performance C92-034 Systems 92-035 Implications for Wind-Tunnel Tests Evaluation of a Navier-Stokes Prediction of a Correction of Sideslip-Induced Static Pres- 92-031 Jet in a Crossflow 92-026 sure Errors in Flight-Test Measurements Twenty-Five Years of Aerodynamic Re- Hot Gas Environment Around STOVL Air- 92-016 search with Infrared Imaging 92-023 craft in Ground Proximity—Part 1: Ex- perimental Study 92-009 Vibration Boundary Layers and Heat Hot Gas Environment Around STOVL Air- Mitigation of Pressure Oscillations Induced Transfer—Turbulent craft in Ground Proximity—Part 2: Nu- merical Study 92-003 by Supersonic Flow over Slender Cavities Heat Transfer Peculiarities in Supersonic C92-162 Flows 92-158 Structural Design (Including Loads) Characteristic Differences Between the Data Analysis for Unsteady Turbulence Demonstration of Structural Optimization Modal Parameters of Cast and Forged Measurements over Airfoils 92-045 Applied to Wind-Tunnel Model Design Structures 92-076 Heat Transfer Effects on Aerodynamics and Effects of Higher Harmonic Control on Implications for Wind-Tunnel Tests 92-156 Coining of Holes in Aluminum Plates: Finite Rotor Performance and Control Loads C92-031 Element Simulations and Experiments C92-049 Twenty-Five Years of Aerodynamic Re- 92-152 Weather Hazards search with Infrared Imaging 92-023 Multidisciplinary Optimization of Aeroservo- Heat Transfer on Accreting Ice Surfaces elastic Systems Using Reduced-Size Assessment of Microburst Models for Down- 092-015 Models 92-151 draft Estimation 92-168 Wing Mass Formula for Twin Fuselage Predicting Droplet Impingement on Yawed Boundary-Layer Stability and Transition Wings 92-155 Aircraft C92-146 Design Optimization of Natural Laminar Wing Mass Formula for Subsonic Aircraft Escape Strategies for Turboprop Aircraft in Flow Bodies in Compressible Flow Microburst Windshear 92-126 C92-116 92-050 Characteristic Differences Between the Advanced Pneumatic Impulse Ice Protection Use of Shear-Sensitive Liquid Crystals for Modal Parameters of Cast and Forged System (PIIP) for Aircraft 092-111 Surface Flow Visualization 92-040 Assessment of One-Dimensional Icing Fore- Structures C92-076 Twenty-Five Years of Aerodynamic Re- Composite Material Repairs to Metallic cast Model Applied to Stratiform Clouds search with Infrared Imaging 92-023 Airframe Components 92-068 92-107 Transition Effects on Airfoil Dynamics and NASA Investigation of a Claimed ’Overlap’ Remote Measurements of Supercooled In- the Implications for Subscale Tests between Two Gust Response Analysis tegrated Liquid Water During WISP/FAA 39-169 Methods 90-105 Aircraft Icing Program 92-092 Aircraft-Triggered Lightning: Processes Fol- ComputatFluiido Dnynaamlic s Structural Materials lowing Strike Initiation that Affect Aircraft Multigrid Euler Calculations over Complete 92-088 Characteristic Differences Between the Hazard Evaluation and Operational Cockpit Aircraft (92-174 Modal Parameters of Cast and Forged Display of Ground-Measured Windshear Numerical Modeling of an Advanced Pneu- Structures 92-076 matic Impulse Ice Protection System for Data 92-047 Testing, Flight and Ground Forward-Look Wind-Shear Detection for Aircraft 92-170 Numerical Simulation of Re-Entry Flow Microburst Recovery 92-008 Unsteady Wind-Tunnel Interference in Air- NASA Investigation of a Claimed ’Overlap’ Around the Space Shuttle with Finite-Rate craft Dynamic Experiments 92-180 between Two Gust Response Analysis Three-Dimensional Simulation of Electro- Methods C90-105 thermal Deicing Systems 92-167 tion: Status and Trends Flight Measurements of Downwash on the Energy Aerodynamic Design via Optimization Ball-Bartoe Jetwing Powered Lift Aircraft 92-164 92-149 Rotating Machinery Unsteady Simulation of Viscous Flowfield High Angle-of-Attack Flush Airdata Sensing Around F-18 Aircraft at Large Incidence System 92-147 Compact Dynamometer System That Can C92-160 Model Flight Tests of a Spin-Resistant Accurately Determine Propeller Perform- "wae. Droplet Impingement on Yawed Trainer Configuration 92-133 ance C92-001 92-155 J. AIRCRAFT, VOL. 29, NO. 6: 1992 INDEX Calculation of Transonic Potential Prediction of Turbulent Flow Behavior over Sources of High Alpha Vortex Asymmetry at Flow Past Swept Wings (92-154 a Slotted Flap 92-007 Zero Sideslip 92-175 Viscous Flow Simulation of a Fighter Air- Hot Gas Environment Around STOVL Air- — Droplet Impingement on Yawed craft 92-143 craft in Ground Proximity—Part 2: Nu- 92-155 Euler/Experiment Correlation of a Generic merical Study 92-003 Suall Two-Dimensional Surface Excres- Fighter (92-139 Transition Effects on Airfoil Dynamics and cences on Aircraft Wings Approaching Navier-Stokes Simulation of a Close-Coupled the Implications for Subscale Tests Separation 92-145 Canard-Wing-Body Configuration C92-138 CB9-169 Wing Design for Hanggliders Having Min- Drag Computation by Vortex Methods imum Induced Drag 92-118 C92-136 Multiphase Flows Predicted Pressure Distribution on a Prop- Thin-Airfoil Correction for Panel Methods Remote Measurements of Supercooled In- Fan Blade Through Euler Analysis 92-115 tegrated Liquid Water During WISP/FAA 92-095 Design Load Predictions on a Fighter-Like Aircraft Icing Program 92-092 Prediction of Vortex Shedding from Fore- Aircraft Wing ©92-101 bodies with Chines 92-059 Simulation of Transonic Flow over Twin-Jet Rarefied Fiows Numerical Simulation of Leading-Edge Vor- Transport Aircraft 92-097 tex Breakdown Using an Euler Code Prediction of Inviscid Supersonic/Hyper- Direct Simulation of Low-Density Flow over 92-044 sonic Aircraft Flowfields 92-089 Airfoils 92-134 Experimental Study of a Low Reynolds Navier-Stokes Predictions for the F-18 Wing Separated Flows Number Tandem Airfoil Configuration and Fuselage at Large Incidence C92-087 92-032 Accurate Prediction of Drag Using Euler Buffet Excitation of Wings at Low Speeds Efficient Panel Method for Vortex Sheet Methods 92-077 92-182 Roll-Up 92-004 Wake Effects on the Prediction of Transonic Sources of High Alpha Vortex Asymmetry at Viscous Flows Around Airfoils (92-063 Zero Sideslip €92-175 Supersonic Flow Numerical Study of Vortex-Dominated Physical Modeling of Ground Effects on Application of Computational Fluid Dy- Flows for Wings at High Incidence and Vortex Wakes 92-166 namics to Sonic Boom Near- and Mid- Sideslip (92-058 Small Two-Dimensional Surface Excres- Field Prediction 92-148 Transonic Navier-Stokes Computations for cences on Aircraft Wings Approaching Prediction of Inviscid Supersonic/Hyper- an Oscillating Wing Using Zonal Grids Separation 92-145 sonic Aircraft Flowfields 92-089 92-048 Physics of Vortical Flows 92-141 Navier-Stokes Study of Supersonic Cavity Numerical Simulation of Leading-Edge Vor- Forcing Level Effects of Internal Acoustic Flowfield with Passive Control (92-030 tex Breakdown Using an Euler Code Excitation on the Improvement of Airfoil Computational Study of Incipient Leading- 92-044 Performance 92-137 Edge Separation on a Supersonic Delta Subsonic and Transonic Low-Reynolds- Suppression of Fatigue-Inducing Cavity Wing (92-028 Number Airfoils with Reduced poco Acoustic Modes in Turbofan Engines Canard-Wing Interaction in Unsteady Su- Moments 92-113 personic Flow 89-155 Navier-Stokes Methods to Predict Cucala. Self-Induced Roll Oscillations of Low-As- tion Control Airfoil Performance C92-034 pect-Ratio Rectangular Wings 92-106 Transonic Flow Navier-Stokes Study of Supersonic Cavity Forebody Vortex Control Using Small, Ro- Transonic Low-Reynolds Number Airfoils Flowfield with Passive Control 92-030 tatable Strakes 92-102 Evaluation of a Navier-Stokes Prediction of a Unsteady Aerodynamics of a Wortmann 92-178 Multigrid Euler Calculations over Complete Jet in a Crossflow 92-026 Wing at Low Reynolds Numbers C92-082 Separation Control Using Moving Surface Drag Reduction of Bluff Bodies = Aircraft (92-174 Aerodynamic Design via Optimization Effects: A Numerical Simulation C92-019 Momentum Injection Comparison of Two Navier-Stokes Codes for Design and Development of a Compacesibie Improved Calculation of Transonic Po9te2n-t1i6a4l Attached Transonic Wing Flows (92-014 Dynamic Stall Facility 92-046 Flow Past Swept Wings 92-154 Navier-Stokes Calculations of Inboard Stall Experimental Study of a Low Reynolds Unsteady Shock-Vortex Interaction on a Delay Due to Rotation 92-010 Number Tandem Airfoil Configuration Flexible Delta Wing 092-132 Hot Gas Environment Around STOVL Air- 92-032 Simulation of Transonic Flow over Twin-Jet craft in Ground Proximity—Part 2: Nu- Navier-Stokes Study of Supersonic Cavity Transport Aircraft 92-097 merical Study 92-003 Flowfield with Passive Control 92-030 Calibration-Related Pseudo-Reynolds Num- Computational Study of Incipient Leading- ber Trends in Transonic Wind Tunnels Hypersonic Flow Edge Separation on a Supersonic Delta Wing 92-028 92-084 — Scramjet Integration on a Wave- Interference Flows Past Cylinder-Fin-Sting- Transonic Aeroelasticity Analysis for Rotor on Simulation of Re-Entry C92F-l1o7w9 WiCnadv-iTtuyn nAesls emSbtiudiieess of F/A-18 Tail 9B2u-f0f2e7t WaBklea deEfsf ects on the Prediction of Tra9n2s-o0n6ic9 CAhreomuinsdt rtyh e Space Shuttle with Finit9e2--R1a6t9e Separation Control Using Moving S9u2r-f0a2c1e TraVnissocnoiucs FNlaovwise r-AStrookuensd CAoirmfpouitlsa tion9s2 -06fo3r Heat Transfer Peculiarities in Supersonic Effects: A Numerical Simulation C92-019 an Oscillating Wing Using Zonal Grids Flows C92-158 Approach to Side Force Alleviation Through 92-048 Subsonic and Transonic Low-Reynolds- Modification of the Pointed Forebody Inlet, Nozzle, Diffusor, and Channel Geometry 92-018 Number Airfoils with Reduced Pitching Flows Suppression of the Wing-Body Junction Moments 92-042 Numerical Computation of Improved Tran- Vortex by Body Surface Suction (92-017 Maximizing Thrust-Vectoring Control Power sonic Potential Method 92-025 Effects of Trailing-Edge Flap on Buffet and Agility Metrics 92-098 Transonic Aeroelasticity Analysis Using Characteristics of a Supercritical Airfoil Investigation of the Diffuser Flow Quality in State-Space Unsteady Aerodynamic Mod- an Icing Research Wind Tunnel (92-006 92-013 eling 92-022 Shock Waves and Detonations Comparison of Two Navier-Stokes Codes for Jets, Wakes, and Viscid-InviscFildow Attached Transonic Wing Flows (92-014 Interactions Sonic Boom Environment Under a Super- Effects of Trailing-Edge Flap on Buffet sonic Military Operating Area 92-172 Characteristics of a Supercritical Airfoil Transonic Low-Reynolds Number Airfoils Numerical Modeling of an Advanced Pneu- C92-013 C92-178 matic Impulse Ice Protection System for Unsteady Flows Unsteady Aerodynamics of a Wortmann Aircraft 92-170 Wing at Low Reynolds Numbers (92-082 Subsonic Flow byes |W ind-Tunnel Interference in Air- Hot Gas Environment Around STOVL Air- craft Dynamic Experiments 92-180 craft in Ground Proximity—Part 1: Ex- Propeller Slip-Stream Model in Subsonic Physical Modeling of Ground Effects on perimental Study 92-009 Linearized Potential Flow (92-177 Vortex Wakes 92-166 J. AIRCRAFT, VOL. 29, NO. 6: 1992 INDEX Unsteady Simulation of Viscous Flowfield Experimental Study of Vortex Flows over Dynamics Around F-18 Aircraft at Large Incidence Delta Wings in Wing-Rock Motion C92-160 C92-091 Longitudinal Stability Analysis of Aerial- Statistical Prediction of Maximum Buffet Navier-Stokes Computations on Swept-Ta- Towed Systems 92-159 Loads on the F/A-18 Vertical Fin pered Wings, Including Flexibility Flutter and Stall Response of a Helicopter 92-120 92-090 Biade with Structural Nonlinearity Time-Average Loading on a Two-Dimen- Navier-Stokes Predictions for the F-18 Wing 92-153 sional Airfoil in Large Amplitude Motion and Fuselage at Large Incidence C92-087 Flight Displays C92-109 Flow over a Twin-Tailed Aircraft at Angle of Unsteady Crossflow on a Delta Wing Using Attack, Part II: Temporal Characteristics ting Lags in Head-Coupled Dis- Particle Image Velocimetry 92-108 92-085 plays Using Head Position Prediction and Self-Induced Roll Oscillations of Low-As- Accurate Prediction of Drag Using Euler Image Deflection 092-171 pect-Ratio Rectangular Wings 92-106 Methods 92-077 Flight Mechanics Experimental Study of Vortex Flows over Flow over a Twin-Tailed Aircraft at Angle of Delta Wings in Wing-Rock Motion Attack Part I: Spatial Characteristics Maximizing Thrust-Vectoring Control Power (92-091 92-060 and Agility Metrics 92-098 Navier-Stokes Computations on Swept-Ta- Prediction of Vortex Shedding from Fore- Identification of the Transfer Function Be- pered Wings, Including Flexibility bodies with Chines 92-059 tween Turbulence and Aircraft (92-057 92-090 Numerical Study of Vortex-Dominated Unsteady Aerodynamics of a Wortmann Flows for Wings at High Incidence and Optimization Techniques Wing at Low Reynolds Numbers C92-082 Sideslip 92-058 Unsteady Aerodynamic Loading Produced Unsteady Aerodynamic Loading Produced Aerodynamic Design via Optimization by a Sinusoidally Oscillating Delta Wing by a Sinusoidally Oscillating Delta Wing 92-164 92-054 92-054 State Estimation Transonic Navier-Stokes Computations for Numerical Simulation of Leading-Edge Vor- an Oscillating Wing Using Zonal Grids tex Breakdown Using an Euler Code Robust Flight Reconstruction for Helicopter 92-048 92-044 Simulation and Training 92-061 Design and Development of a Compressible Effects of Ambient Turbulence on the Decay Dynamic Stall Facility 92-046 of a Trailing Vortex Wake 92-036 System Identification Data Analysis for Unsteady Turbulence Effect of Wind Shear on Airspeed During Reconstruction of Flight Path in Turbulence Measurements over Airfoils 92-045 Airplane Landing Approach 92-033 (92-081 Interference Flows Past Cylinder-Fin-Sting- Computational Study of Incipient Leading- Identification of the Transfer Function Be- Cavity Assemblies 92-027 Edge Separation on a Supersonic Delta tween Turbulence and Aircraft (92-057 Wind-Tunnel Studies of F/A-18 Tail Buffet Wing 92-028 92-021 Approach to Side Force Alleviation Through Trajectory Optimization Effects of Trailing-Edge Flap on Buffet Modification of the Pointed Forebody Characteristics of a Supercritical Airfoil Geometry 92-018 Control Strategy for Maximizing Reconnais- 92-013 Suppression of the Wing-Body Junction sance Range of Hypersonic Cruise Vehi- Rapid Prediction of High-Alpha Unsteady Vortex by Body Surface Suction C92-017 cles 92-053 Aerodynamics of Slender-Wing Aircraft Rapid Prediction of High-Alpha Unsteady Interdisciplinary Topics 92-012 Aerodynamics of Slender-Wing Aircraft Transition Effects on Airfoil Dynamics and 92-012 the Implications for Subscale Tests Efficient Panel Method for Vortex Sheet Aerospace Management 89-169 Roll-Up 92-004 Structural Risk Assessment in the Israel Air Force for Fleet Management 92-083 Viscous Non-Boundary-Layer Flows Guidance, Control, and Dynamics Viscous Flow Simulation of a Fighter Air- Technology Aerospace Technology Utilization craft 92-143 High Angle-of-Attack Flush Airdata Sensing Physics of Vortical Flows 92-141 Aircraft Dynamics System 92-147 Drag Computation by Vortex Methods Analytical Modeling of SH-2F Helicopter C92-136 Shipboard Operation 92-142 Analanyd Ntumeiriccal aMeltho ds Vortices System for Generating Sequences of Phased Numerical Modeling of an Advanced Pneu- Gust or Taxi Loadings 92-104 matic Impulse Ice Protection System for Wind-Tunnel Investigation of a Fighter Aircraft 92-170 Model at High Angles of Attack C92-176 Aircraft Guidance Application of Advanced Multidisciplinary Physical Modeling of Ground Effects on Microwave Landing System Modeling with Analysis and Optimization Methods to Voriex Wakes 92-166 Application to Air Traffic Control Au- Vehicle Design Synthesis 92-135 Unsteady Simulation of Viscous Flowfield tomation 92-051 Numerical Study of Vortex-Dominated Around F-18 Aircraft at Large Incidence Flows for Wings at High Incidence and C92-160 Aircraft Stability and Control Sideslip 92-058 Physics of Vortical Flows 92-141 Longitudinal Stability Analysis of Aerial- Two-Fence Concept for Efficient Trapping Towed Systems 92-159 Atmosapndh Speacer Siciecnce s NavoCifae nrVa-orSrtdtoi-kcWeeissn gSo-inBm ouAdliayrt fiooiCnlos n offi gau rCaltoisoen- Co9Cu922p--l11e43d08 DApopCwloninwctaratosilho n Suforofrf acAJeco tiinDveeef dl-eFWclitenxigiob nlse A irWfirnagm e9 2T-ew0ci6ht6-h Assdreasfstm eEnstt iomfa tMiiocnr oburst Models for 9D2o-w1n6-8 Drag Computation by Vortex Methods nology to the Agile Falcon 92-064 Asscaessts mMeontd elo f AOpnpel-iDeidm etnos iSotnraatli foIrcmi ngC lFoourdes- 92-136 Analysis of Airship Lateral Maneuverability UnsFlteexaidbyle SDhelotcak -VWoirntge x Interaction 92o-n1 32a Artificial Intelligence 92-043 Airudraitnag ACtamliobsrpahteiroinc TWeichnndi quPerosf ilefso r 9C92M2-e-1a00s97-6 Effect of Nose-Boom on Forebody Vortex Flow 92-122 Wind-Tunnel Compressor Stall Monitoring Establishing a Database for Flight in the Pitch Rate/Sideslip Effects on Leading-Edge Using Neural Networks 92-121 Wakes of Structures 92-086 Extension Vortices of an F/A-18 Aircraft Expert System for Real-Time Aircraft Mon- Human Factors Model (92-114 itoring 092-011 Suppression of Fatigue-Inducing Cavity ting Lags in Head-Coupled Dis- Acoustic Modes in Turbofan Engines Control System Design plays Using Head Position Prediction and 92-113 Multidisciplinary Optimization of Aeroservo- Image Deflection 92-171 Forebody Vortex Control Using Small, Ro- elastic Systems Using Reduced-Size Nine-Degree-of-Freedom Simulation of Ro- tatable Strakes 92-102 Models 92-151 tating Parachute Systems 92-130 J. AIRCRAFT, VOL. 29, NO. 6: 1992 INDEX Range, Energy, Heat of Motion in the Compact Dynamometer System That Can Composite Material Repairs to Metallic Modified NBC, Anti-g, Tank Suit — Determine Propeller Perform- Airframe Components 92-068 92-099 92-001 Canard-Wing Interaction in Unsteady Su- Improved Measurement of the Dynamic personic Flow 89-155 Ramjaned Stcrasmje ts Loads Acting on Rotating Parachutes Structural Dynamics and 92-067 Thermal Managfore am Maech n5 Ctrui se Hazard Evaluation and Operational Cockpit AircUsinrg aEndfothterm ic Fuel C92-056 Characterization Display of Ground-Measured Windshear Response of Double-Wall (Sandwich) Cir- Data 92-047 Structural Mechanics and Materials cular Plates to Random Excitations—An- Reliability, Maintainabilitya,n d alytical Approach 92-150 Logistics Support Aeroelastaindc Cionttyro l Aeroelastic Effects of Spoiler Surfaces on a Low-Aspect-Ratio Rectangular Wing Structural Risk Assessment in the Israel Air Unsteady Shock-Vortex Interaction on a 92-129 Force for Fleet Management 92-083 Flexible Delta Wing 92-132 Reduced Basis Alternatives to the Solution of Composite Material Repairs to Metallic Aeroelastic Effects of Spoiler Surfaces on a Nonlinear Dynamical Systems 92-128 Airframe Components 92-068 Low-Aspect-Ratio Rectangular Wing Statistical Prediction of Maximum Buffet 92-129 Loads on the F/A-18 Vertical Fin Research Facilities and Instrumentation Statistical Prediction of Maximum Buffet 92-120 Loads on the F/A-18 Vertical Fin Experimental-Theoretical Investigation of Reconsof tFlirghtu Pacth tini Tuorbunlen ce 92-120 the Vibration Characteristics of Rotating 92-081 Whirl-Flutter Stability of a Pusher Config- Composite Box Beams 92-100 Invesof tthei Difgfusaer tFloiw Qoualnity in uration in Nonuniform Flow 92-117 Nonlinear Flutter of Two-Dimensional Sim- an Icing ResearcWihnd Tunnel (92-006 Transition of the Flutter Mode of a Two- ply Supported Symmetric Composite Lam- Safety Dimensional Section with an External inated Plates 92-020 Store 92-075 Structural Finite Hements Range, Energy, Heat of Motion in the Coalescence of Aeroelastic Modes in Flutter Modified NBC, Anti-g, Tank Suit Analysis 92-072 Coining of Holes in Aluminum Plates: Finite 92-099 Application of Active Flexible Wing Tech- Element Simulations and Experiments Hazard Evaluation and Operational Cockpit nology to the Agile Falcon 92-064 92-152 Display of Ground-Measured Windshear Integrated Aeroelastic Control Optimization Structural and Aerodynamic Data Trans- Data 92-047 of Laminated Composite Lifting Surfaces formation Using Inverse Isoparametric 92-039 Mapping 92-073 Sensor Systems Low-Speed Flutter Characteristics of Some Simple Low-Aspect-Ratio Delta-Wing Structural Modeling Correction of Sideslip-Induced Static Pres- sure Errors in Flight-Test Measurements Models C92-038 Response of Double-Wall (Sandwich) Cir- Wind-Tunnel Studies of F/A-18 Tail Buffet cular Plates to Random Excitations—An- C92-016 92-021 alytical Approach 92-150 Launch Vehicle and Missile (LV/M) Approach for Analysis and Design of Com- DynaModmel iAnaclys is posite Rotor Blades 92-105 Technology Analytical Modeling of SH-2F Helicopter Structural Optimization Shipboard Operation 92-142 Aerodynamics System for Generating Sequences of Phased Demonstration of Structural Optimization Aerodynamic Forces on Noncircular Cross- Gust or Taxi Loadings 92-104 Applied to Wind-Tunnel Model Design Section Missile Forebodies 92-093 Transition of the Flutter Mode of a Two- 92-156 Structurai and Aerodynamic Data Trans- Dimensional Section with an External Application of Advanced Multidisciplinary Analysis and Optimization Methods to formation Using Inverse Isoparametric Store 92-075 Mapping 92-073 Vehicle Design Synthesis (92-135 Interference Flows Past Cylinder-Fin-Sting- Fleanxd Aictibve lStruectur es Integrated Aeroelastic Control Optimization Cavity Assemblies 92-027 of Laminated Composite Lifting Surfaces Approach to Side Force Alleviation Through Wing Design for Hanggliders Having Min- 92-039 imum Induced Drag 92-118 Modification of the Pointed Forebody Thermal Effects Geometry 92-018 Structural Composite Materials Acoustic Testing of High-Temperature Configurational Design Approach for Analysis and Design of Com- Panels (92-181 posite Rotor Blades 092-105 Thermal Structures: Four Decades of AeroFdorceys non Naoncimrcuilar cCro ss- Experimental-Theoretical Investigation of Progress 92-070 Section Missile Forebodies 92-093 the Vibration Chdracteristics of Rotating Thermophysics and Heat Transfer TesFtligiht nandg Gr,ou nd Composite Box Beams 92-100 Nonlinear Flutter of Two-Dimensional Sim- Airdata Calibration Techniques for Meas- ply Supported Symmetric Composite Lam- AerothermodTyhenrmaalm iProctesct/io n uring Atmospheric Wind Profiles C92-096 inated Plates 92-020 Thermal Structures: Four Decades of Pro- Ground-Testing Techniques for Tethered gress 92-070 Systems 92-035 ee ee anne ee and Fracturaned ,E n Forced Convection Propulsion Degradation) Heat Transfer on Accreting Ice Surfaces Acoustic Testing of High-Temperature 92-015 Airbreathing Propulsion Panels (92-181 Melting/ Solidification Thermal Management for a Mach 5 Cruise Coining of Holes in Aluminum Plates: Finite Aircraft Using Endothermic Fuel €92-050 Element Simulations and Experiments Three-Dimensional Simulation of Electro- Control Strategy for Maximizing Reconnais- 92-152 thermal Deicing Systems 92-167 sance Range of Hypersonic Cruise Vehi- System for Generating Sequences of Phased Thermal Modeling and Analysis cles 92-053 Gust or Taxi Loadings 92-104 Preliminary Sizing Methodology for Hyper- Structural Risk Assessment in the Israel Air Thermal Structures: Four Decades of sonic Vehicles 92-024 Force for Fleet Management 92-083 Progress 92-070 J. AIRCRAFT, VOL. 29, NO. 6: 1992 INDEX Author Index Addy, H. E., Jr., C92-006 Dunn, P. F., C92-001 Lan, C. E., ©92-074 Agrawal, S., 92-101 Durck, C. H., C92-099 Larson, T. J., C92-147 Alhusein, M. A., 92-145 Eastin, R. G., C92-104 Lawrence, S. L., C92-148 Amato, M., C92-063 Edwards, T. A., C92-148 Leatherwood, J. D., C92-181 Anderson, W. J., C92-116, C92-146 Eggold, D. P., C92-065 Lee, B. H. K., C92-013, C92-021, Asson, K. M., C92-001 Engblom, !. J., C92-128 92-120 Aulehla, F., C92-084 Epstein, B., C92-174 Lee, C. K., C92-037 Bach, R. E., Jr., C92-016 Ericsson, L. E., C89-169, C92-012, Lee, K. D., C92-164 Bailey, J. E., C92-061 (92-175 Lee, M., C92-064 Baitis, E., C92-142 Est, B. E., C92-093 Lee, P., C92-074 Barnett, R. M., C92-044 Etkin, B., C90-105 Leedy, D. H., €92-176 Baysal, O., C92-027 Eyi, S., C92-164 Leffel, K. L., C92-170 Becker, K., C92-097 Fearn, R. L., C92-026 Leishman, J. G., C92-022 Belcher, P. J., C92-053 Flanders, J. B., C92-011 Lerwick, T. R., C92-104 Benner, R. H., C92-113 Fouladi, K., C92-027 Lesieutre, D. J., C92-059 Beyers, M. E., C92-180 Franke, M. E., C92-034 Leung, R. W., C92-027 Bismarck-Nasr, M. N., C92-072 French, M., C92-156 Levin, D., C92-067, C92-106 Blacodon, D., C92-173 Fuglsang, D. F., C92-101 Lewis, L. C., C92-091 Bobbitt, R. B., C92-126 Gal-Or, B. Z., C92-098 Lewis, M. J., C92-179 Bofilios, D. A., C92-150 Gartenberg, E., C92-023 Léwy, S., C92-144, C92-173 Bonhaus, D. L., C92-014 Garza, R. G., C92-172 Liefer, R. K., C92-065 Boronow, W., C92-167 Gea, L., C92-069 Lin, Y., C92-081 Borovoy, V. Y., C92-158 Gee, K., C92-160 Liou, S. G., C92-060 Bragg, M. B., C92-155 Goodsell, A. M., C92-139 Liu, C. H., 92-058 Brazhko, V. N., C92-158 Graham, G. M., C92-109 Liu, H.-T., C92-036, C92-082, 92-166 Brodersen, R., C92-029 Grandhi, R. V., C92-053 Lo, C. F., €92-121 Brown, D., C92-02i Griffin, M. J., C92-171 Loewy, R. G., C92-131 Burkhalter, J. E., C92-066 Guruswamy, G. P., C92-048, Létstedt, P., C92-177 Butler, B. E., C92-080 C92-090, C92-132 Louie, C. M., C92-044 Canard-Caruana, S., C92-144 Gutmark, E., C92-162 Lowson, M. V., C90-108 Carr, L. W., C92-046 Haering, E. A., Jr., C92-096 Lu, L., €92-020 Carter, J., C92-115 Hammond, D. O., C92-068 Lucas, M. J., C92-172 Caughey, D. A., C92-154 Hankey, W. L., C92-053 Luntz, A., C92-174 Cavazos, O. V., C92-114 Hansman, R. J., Jr., C92-015, Luttges, M. W., (92-054 Lyrintzis, C. S., C92-150 Cenko, A., C92-035 92-047 Chaderjian, N. M., C92-048, C92-087 Harris, R. V., Jr., C92-002 Mabey, D. G., C89-169, C92-031 Chandra, R., C92-100 Hassan, A. A., C92-019 Macedo Moura, G. A., C92-105 Chandrasekhara, M. S., C92-046 Healey, J. V., C92-086, C92-094 MacLean, R., C92-009 Chang, C. L., C92-128 Hebbar, S. K., C92-114, C92-176 Madison, R. M., C92-011 Chang, I-Chung, C92-069 Heragu, S. S., C92-007 Magness, C., C92-108 Chang, J., C92-112 Hicks, R., C92-042 Maikapar, G. I., C92-158 Chang, R. C., C92-137 Hinton, D. A., 92-008 Malcolm, G. N., C92-091, C92-102 Chaput, A. J., C92-024 Howard, R. M., C92-045, C92-126 Malloy, P. J., C92-101 Chattopadhyay, A., C92-041 Hsiao, F.-B., C92-137 Martin, C. A., C92-111, C92-170 Hsu, C.-H., €92-058 Martinez-Val, R., C92-110 Humi, M., C92-136 Mastropaolo, J. A., C92-099 Huyer, S. A., C92-054 Mathew, M. B., C92-131 Hwang, P. A., C92-166 Maull, D. J., C92-182 Tlacqua, P. N., C92-045 Mazur, V., C92-088 Christian, T. F., Jr., C92-068 Islam, M., C92-109 McMillin, S. N., C92-028 Cimbala, J. M., C92-017 Jackson, P. S., C92-115 Mendenhall, M. R., C92-059 Clessas, G., C92-035 Johnson, D. K., C92-045 Metzger, F. B., C92-095 Clevenson, S. A., C92-181 Jones, C. H., C92-011 Meyers, W., C92-142 Cochran, J. B., C92-068 Jones, H., C92-041 Modi, V. J., C92-018, C92-062 Cockrell, D. J., C92-145 Jones, S. C., C92-056 Moes, T. R., ©92-147 Coiro, D. P., C92-063 Julliard, J., C92-144 Mohler, S. H., Jr., C92-155 Cole, S. R., C92-129 Moreau, J., C92-088 Consoli, R. D., C92-135 Mosher, M., C92-127 Crouse, G. L., Jr., C92-022 Moulton, C. L., C92-172 Cummings, R. M., C92-087 Mueller, T. J., C92-032 Daniels, E. F., C92-181 Murthy, S. N. B., C92-009 de Gaston, A. N., C92-099 Keith, T. G., Jr., C92-006, C92-167, Nachshon, A., C92-174 de Matteis, P., C92-063 92-170 Nagabhushan, B. L., C92-043 De Witt, K. J., C92-167, C92-170 Key, M. K., C92-066 Nakagawa, N., C92-159 Délery, J. M., C92-141 Kim, I., C92-030 Narramore, J. C., C92-010 Desai, V. R., C92-172 Kim, J. M., C92-060, C92-085 Nelson, H. F., €92-093 Dodbele, S. S., C92-050 King, H. H. C., C92-012 Ng, T. T., C92-091, C92-102, C92-122 Doggett, R. V., Jr., C92-038 Kobayakawa, M., C92-095 Nguyen, K., €92-049 Doherr, K., C92-130 Kolar, R., C92-105 Nikfetrat, K., C92-077 Dowell, E. H., C92-153 Kolonay, R. M., C92-156 Nitzsche, F., C92-117 Downing, D. R., C92-065 Kor:erath, N. M., C92-060, C92-085 Norum, T. D., C92-161 los, T. N., C92-039 KrishnaKumar, K., C92-061 Obata, A., C92-159 Drela, M., C92-178 Kubota, H., C92-169 Obayashi, S., C92-132 Dulikravich, G. S., C92-165 Kwon, O. J., C92-143 Ogeman, R., C92-152 Dunlavy, S., C92-120 Lamarre, F., C92-004 Ojha, S. K., C92-119 J. AIRCRAFT, VOL. 29, NO. 6: 1992 INDEX O’Neil, P. J., C92-044 Sankar, L. N., C92-019, C92-143 Thakur, S. S., C92-026 O’Neill, M. K. L., 92-179 Sauer, G., C92-029 Thomas, J. L., C92-028 Oz, H., €92-039 Schadow, K. C., C92-162 Thornton, E. A., C92-070 Panossian, H. V., C92-076 Schanzer, G., C92-057 Tidd, D. M., C92-174 Paraschivoiu, I., C92-004 Scharpf, D. F., C92-032 Tran, D., C92-016 Parks, E. K., C92-016 Schiff, L. B., C92-087 Treaster, A. L., C92-017 Pasha, R. P. K., C92-043 Schilling, H., 92-130 Tu, E. L., 92-138 Pendleton, E., 92-064 Schwartz, R. J., C92-060, C92-085 Tunick, A., C92-107 Perez, E., C92-110 Sheftic, J. S., C92-027 Udin, S. V., C92-116, C92-146 Perry, B., ITI, C90-105 Shi, G. Z., C92-121 Unruh, J. F., C92-071 Peters, D. A., C92-055 Shiau, L., C92-020 Valasek, J., C92-065 Petley, D. H., C92-056 Shih, E., C92-062 van Dam, C. P., C92-042, C92-077 Philips, D. B., C92-017 Shpund, Z., C92-067 Van Santen, A. R., C92-099 Phillips, K., €92-035 Shyu, R.-N., 92-137 Vanka, S. P., C92-003 Pidaparti, R. M. V., C92-073 Skow, A. M., C92-005 Verhoff, A., C92-089 Pittman, J. L., C92-028 Skuratov, A. S., C92-158 Vermeland, R., C92-010 Platzer, M. F., C92-114 Smith, R. A., C92-162 Vicroy, D. D., C92-168 Plotkin, K. J., C92-172 Smith, S. C., C92-040 Wada, Y., C92-169 Pototzky, A. S., C90-105 Snider, J. B., 92-092 Wang, L., C92-154 Poulose, M. M., C92-051 So, R. H. Y., €92-171 Wanke, C., C92-047 Powell, C. A., C92-181 Sobieszczanski-Sobieski, J., C92-135 Wasserman, L., C92-064 Prasanth, R. K., C92-061 Soedel, S. M., 92-104 Weber, R. L., C92-092 Putt, J. C., C92-111, C92-170 Soistmann, D. L., C92-038 Wei, F., C92-142 Rachele, H., C92-107 Solies, U. P., C92-149 Westwater, E. R., C92-092 Ramamurthy, S., C92-170 Spence, P. L., C92-163 White, R. J., C92-033 Reuther, J., C92-642 Spring, D. J., C92-066 Whitmore, S. A., (92-147 Rhoades, M. M., C92-094 Srnsky, R. A., C92-166 Williams, S. L., C92-034 Rill, S., C92-097 Stankov, B. B., 92-092 Woods, J. A., C90-105 Rizk, Y. M., C92-087, C92-160 Stark, G. E., C92-052 Woodward, R. P., C92-103 Robelen, D. B., €92-133 Stark, V. J. E., Ce9-155 Wornom, S. F., C92-014 Roberts, A. S., Jr., C92-023 Stewart, A. C., C92-018 Xue-Song, B., C92-025 Robinson, M. C., C92-054 Stookesberry, D., €92-089 Yamaguchi, K., C92-015 Robinson, O., C92-108 Strash, D. J., C92-174 Yang, Z., C92-075 Rockwell, D., C92-108 Struminskaya, I. V., C92-158 Yaslik, A. D., C92-167 Rodrigues, E. A., C92-117 Su, A., C92-055 Ying, B., C92-062 Rosen, A., C92-131 Sugimoto, T., C92-118 Yip, L. P., C92-133 Ross, H. M., C92-133 Sullivan, J., C92-009 Yokomizo, T., C92-062 Rossow, V. J., C92-140 Tafti, D. K., C92-003 Yoo, K. M., C92-055 Roth, K. R., C92-026 Tai, T. C., C92-134 Yosibash, Z., C92-083 Rubin, T., (92-174 Takaki, R., C92-095 Zan, S. J., C92-182 Sadeck, J. E., C92-037 Tang, D. M., C92-153 Zhao, L., C92-075 Zi-qiangq, Z., C92-025 Zotto, M., C92-131

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JOURNAL OF AIRCRAFI Vol. 29, No. 6, Nov.—Dec. 1992 1992 Journal of Aircraft Index How to Use the Index In the Subject Index, pages 1145-1150 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 1151-1152, lists all authors associated with a given technical paper. The locating numbers are identical to those in the Subject Index. The Chronological Index, pages 1153-1159, lists all papers by their unique code 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, 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 1992, that paper also will appear in both the Subject and Chronological Indexes. Authors of Comments also are listed in the Author Index. JOURNAL OF AIRCRAFI Vol. 29, No. 6, Nov.—Dec. 1992 1992 Journal of Aircraft Index How to Use the Index In the Subject Index, pages 1145-1150 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 1151-1152, lists all authors associated with a given technical paper. The locating numbers are identical to those in the Subject Index. The Chronological Index, pages 1153-1159, lists all papers by their unique code 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, 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 1992, that paper also will appear in both the Subject and Chronological Indexes. Authors of Comments also are listed in the Author Index. J. AIRCRAFT, VOL. 29, NO. 6: 1992 INDEX Subject Index Aircraft Technology, Conventional, Experimental Study of Vortex Flows over Correction of Sideslip-Induced Static Pres- STOL/VTOL Delta Wings in Wing-Rock Motion sure Errors in Flight-Test Measurements C92-091 92-016 Aerodynamics Prediction of Inviscid Supersonic/Hyper- Rapid Prediction of High-Alpha Unsteady Buffet Excitation of Wings at Low Speeds sonic Aircraft Flowfields 92-089 Aerodynamics of Slender-Wing Aircraft 92-182 Navier-Stokes Predictions for the F-18 Wing 92-012 Transonic Low-Reynolds Number Airfoils and Fuselage at Large Incidence C92-087 Navier-Stokes Calculations of Inboard Stall C92-178 Establishing a Database for Flight in the Delay Due to Rotation 92-010 Wind-Tunnel Investigation of a Fighter Wakes of Structures 92-086 Hot Gas Environment Around STOVL Air- Model at High Angles of Attack C92-176 Flow over a Twin-Tailed Aircraft at Angle of craft in Ground Proximity—Part 1: Ex- Sources of High Alpha Vortex Asymmetry at Attack, Part Ii: Temporal Characteristics perimental Study 92-009 Zero Sideslip 92-175 92-085 Efficient Panel Method for Vortex Sheet Multigrid Euler Calculations over Complete Accurate Prediction of Drag Using Euler Roll-Up 92-004 Aircraft (92-174 Methods 92-077 Minimum Induced Drag for Wings with Aerodynamic Shape Design and Optimiza- Effect of Thrust Vectoring on Level-Turn Spanwise Camber 90-108 tion: Status and Trends 92-165 Performance 92-074 Improved Calculation of Transonic Potential Improved Measurement of the Dynamic Aeroelasticity and Aeroservoelasticity Flow Past Swept Wings 92-154 Loads Acting on Rotating Parachutes Flight Measurements of Downwash on the 92-067 Demonstration of Structural Optimization Ball-Bartoe Jetwing Powered Lift Aircraft Downwash for Joined-Wing Airframe with Applied to Wind-Tunnel Model Design 92-149 Control Surface Defiections 92-066 (92-156 Application of Computational Fluid Dy- Wake Effects on the Prediction of Transonic Flutter and Stall Response of a Helicopter namics to Sonic Boom Near- and Mid- Viscous Flows Around Airfoils (92-063 Blade with Structural Nonlinearity Field Prediction 92-148 Drag Reduction of Bluff Bodies Through 92-153 Small Two-Dimensional Surface Excres- Momentum Injection 92-062 Multidisciplinary Optimization of Aeroservo- cences on Aircraft Wings Approaching Flow over a Twin-Tailed Aircraft at Angle of elastic Systems Using Reduced-Size Separation 92-145 Attack Part I: Spatial Characteristics Models 92-151 Viscous Flow Simulation of a Fighter Air- 92-060 Dynamic Analysis of Rotor Blades with Root craft 92-143 Prediction of Vortex Shedding from Fore- Retention Design Variations 92-131 Two-Fence Concept for Efficient Trapping bodies with Chines 92-059 Aeroelastic Effects of Spoiler Surfaces on a of Vortices on Airfoils 92-140 Identification of the Transfer Function Be- Low-Aspect-Ratio Rectangular Wing Euler/Experiment Correlation of a Generic tween Turbulence and Aircraft 92-057 92-129 Fighter (92-139 Extension and Validation of an Unsteady Design Load Predictions on a Fighter-Like Navier-Stokes Simulation of a Close-Coupled Wake Model for Rotors 92-055 Aircraft Wing 92-101 Canard-Wing-Body Configuration C92-138 Unsteady Aerodynamic Loading Produced Navier-Stokes Computations on Swept-Ta- Forcing Level Effects of Internal Acoustic by a Sinusoidally Oscillating Delta Wing pered Wings, Including Flexibility Excitation on the Improvement of Airfoil 92-054 92-090 Performance 92-137 Design Optimization of Natural Laminar Structural and Aerodynamic Data Trans- Direct Simulation of Low-Density Flow over Flow Bodies in Compressible Flow formation Using Inverse Isoparametric Airfoils 92-134 C92-050 Mapping 92-073 Effect of Nose-Boom on Forebody Vortex Design and Development of a Compressible Coalescence of Aeroelastic Modes in Flutter Flow 92-122 Dynamic Stall Facility 92-046 Analysis 92-072 Thin-Airfoil Correction for Panel Methods Data Analysis for Unsteady Turbulence Transonic Aeroelasticity Analysis for Rotor 92-115 Measurements over Airfoils 92-045 Blades 92-069 Pitch Rate/Sideslip Effects on Leading-Edge Analysis of Airship Lateral Maneuverability Application of Active Flexible Wing Tech- Extension Vortices of an F/A-18 Aircraft 92-043 nology to the Agile Falcon 92-064 Model 92-114 Subsonic and Transonic Low-Reynolds- Extension and Validation of an Unsteady Minimizing Supersonic Wave Drag with Number Airfoils with Reduced Pitching Wake Model for Rotors 92-055 Physical Constraints at Design and Off- Moments 92-042 Dynamics of an Optimized Rotor Blade at Design Mach Numbers 92-112 Use of Shear-Sensitive Liquid Crystals for Off-Design Flight Conditions 92-041 Optimum Cruise Lift Coefficient in Initial Surface Flow Visualization 92-040 Integrated Aeroelastic Control Optimization Design of Jet Aircraft 92-110 Controlled Opening Method for Clustered of Laminated Composite Lifting Surfaces Time-Average Loading on a Two-Dimen- Parachutes 92-037 92-039 sional Airfoil in Large Amplitude Motion Ground-Testing Techniques for Tethered Transonic Aeroelasticity Analysis Using 92-109 Systems 92-035 State-Space Unsteady Aerodynamic Mod- Unsteady Crossflow on a Delta Wing Using Navier-Stokes Methods to Predict Circula- eling 92-022 Particle Image Velocimetry 92-108 tion Control Airfoil Performance C92-034 Nonlinear Flutter of Two-Dimensional Sim- Self-Induced Roll Oscillations of Low-As- Experimental Study of a Low Reynolds ply Supported Symmetric Composite Lam- pect-Ratio Rectangular Wings 92-106 Number Tandem Airfoil Configuration inated Plates 92-020 Forebody Vortex Control Using Small, Ro- 92-032 NASA Investigation of a Claimed ’Overlap’ tatable Strakes 92-102 Numerical Computation of Improved Tran- between Two Gust Response Analysis Design Load Predictions on a Fighter-Like sonic Potential Method 92-025 Methods 90-105 Aircraft Wing 92-101 Transonic Aeroelasticity Analysis Using Canard-Wing Interaction in Unsteady Su- Simulation of Transonic Flow over Twin-Jet State-Space Unsteady Aerodynamic Mod- personic Flow 89-155 Transport Aircraft 92-097 eling 92-022 Flight Deck Aerodynamics of a Nonaviation Separation Control Using Moving Surface Aerospace Plane Ship 92-094 Effects: A Numerical Simulation C92-019 Aerodynamic Forces on Noncircular Cross- Suppression of the Wing-Body Junction Acoustic Testing of High-Temperature Section Missile Forebodies 92-093 Vortex by Body Surface Suction C92-017 Panels (92-181 1146 J. AIRCRAFT, VOL. 29, NO. 6: 1992 INDEX Numerical Simulation of Re-Entry Flow Fuels and Fuel Systems Fighter Agility Metrics, Research and Test Around the Space Shuttle with Finite-Rate 92-065 Chemistry 092-199 Thermal t for a Mach 5 Cruise Control Strategy for Maximizing Reconnais- Aircraft Using EndotheFurelm Ci92c-05 6 sance Range of Hypersonic Cruise Vehi- Civil Missions and Transportation General Aviation cles 92-053 Preliminary Sizing Methodology for Hyper- Effects of Higher Harmonic Control on sonic Vehicles 92-024 Model Flight Tests of a Spin-Resistant Rotor Performance and Control Loads On the Threshold—The Outlook for Super- Trainer Configuration 92-133 92-049 sonic and Hypersonic Aircraft 92-002 Wing Mass Formula for Subsonic Aircraft Dynamics of an Optimized Rotor Blade at 92-116 Off-Design Flight Conditions 92-041 Communaind cAira Ttrafific oConntr ol Effect of Wind Shear on Airspeed po Agility as a Contrtio bDesuigtn Boalranc e Airplane Landing Approach 92-005 Microwave Landing System Modeling with Application to Air Traffic Control Au- Landing Dynamics Powerplant Integration tomation (92-051 Analytical Modeling of SH-2F Helicopter Optimized Scramjet Integration on a Wave- Configuration Design Shipboard Operation 92-142 rider 92-179 Whirl-Flutter Stability of a Pusher Config- Self-Compensating Carrier Aircraft Recovery Optimized Scramjet Integration on a Wave- System 92-029 uration in Nonuniform Flow 92-117 rider 92-179 Propaned lRotlor eSysrte ms Aerodynamic Shape Design and Optimiza- Lighter-Than-Air-Systems tion: Status and Trends 92-165 Propeller Slip-Stream Model in Subsonic Wing Mass Formula for Twin Fuselage Analysis of Airship Lateral Maneuverability Linearized Potential Flow (92-177 Aircraft (92-146 C92-043 Effects of Fuselage Boundary Layer on Application of Advanced Multidisciplinary Noise Propagation from Advanced Pro- Analysis and Optimization Methods to Man/ Machine Interface pellers 92-163 Vehicle Design Synthesis 92-135 Expert System for Real-Time Aircraft Mon- Dynamic Analysis of Rotor Blades with Root Minimizing Supersonic Wave Drag with itoring 092-011 Retention Design Variations 92-131 Physical Constraints at Design and Off- Whirl-Flutter Stability of a Pusher Config- Design Mach Numbers 92-112 Military Missions uration in Nonuniform Flow 92-117 Optimum Cruise Lift Coefficient in Initial Noise of Two High-Speed Model Counter- Design of Jet Aircraft 92-110 Advanced Pneumatic Impulse Ice Protection Rotation Propellers at Takeoff/Approach System (PIIP) for Aircraft 92-111 Downwash for Joined-Wing ep with Conditions 92-103 Control Surface Deflections Maximizing Thrust-Vectoring Control Power Predicted Pressure Distribution on a Prop- and Agility Metrics 92-098 Design Optimization of Natural waier Fan Blade Through Euler Analysis Flow Bodies in Compressible Flow EstWaabkleissh inogf Sat ruDcattuarbeass e for Flight ain 92-095 C92-050 Structure-Borne Noise Transmission in the Agliy as& Contributor toDe signB alance On the Threshold—The Outlook for Super- Propfan Test Assessment Aircraft sonic and Hypersonic Aircraft (92-002 92-071 On the Threshold—The Outlook for = Compact Dynamometer System That Can Deceleration Systems sonic and Hypersonic Aircraft (92-002 Accurately Determine Propeller Perform- Noise ance 92-001 Nine-Degree-of-Freedom Simulation of Ro- tating Parachute Systems 92-130 Sonic Boom Environment Under a Super- Rotorcraft Improved Measurement of the Dynamic sonic Military Operating Area 92-172 Spinning Mode Analysis of the Acoustic Loads Acting on Rotating Parachutes Effects of Fuselage Boundary Layer on Field Generated by a Turboshaft Engine 92-067 Noise Propagation from Advanced Pro- (92-173 Controlled Opening Method for Clustered pellers 92-163 Flutter and Stall Response of a Helicopter Parachutes 92-037 Mitigation of Pressure Oscillations Induced Blade with Structural Nonlinearity Self-Compensating Carrier Aircraft Recovery by Supersonic Flow over Slender Cavities 92-153 System 92-029 92-162 Dynamic Analysis of Rotor Blades with Root Ground Impingement Noise of Supersonic Retention Design Variations 92-131 Economics Jets from Nozzles with Various Exit Ge- Approach for Analysis and Design of Com- ometries 92-161 posite Rotor Blades 92-105 Software Reliability for Flight Crew Training Application of Computational Fluid Dy- “i> Deck Aerodynamics of a Nonaviation Simulators 92-052 namics to Sonic Boom Near- and Mid- 92-094 Field Prediction 92-148 Pigs,M odel for Unmanned Simulated Hel- Flight Mechanics Experimental Study of Noise Generation and icopters (92-080 Propagation in a Turbofan Model Transonic Aeroelasticity Analysis for Rotor Unsteady Wind-Tunnel Interference in Air- 92-144 Blades 92-069 craft Dynamic Experiments 92-180 Evaluation of Discrete Frequency Sound in Extension and Validation of an Unsteady Escape Strategies for Turboprop Aircraft in Closed-Test-Section Wind Tunnels Wake Model for Rotors 92-055 Microburst Windshear 92-126 92-127 Effects of Higher Harmonic Control on Optimization of Constant Altitude—Con- Noise of Two High-Speed Model Counter- Rotor Performance and Control Loads stant Airspeed Flight of Turbojet Aircraft Rotation Propellers at Takeoff/Approach 92-049 92-119 Conditions 92-103 Navier-Stokes Calculations of Inboard Stall Wing Design for Hanggliders Having Min- Structure-Borne Noise Transmission in the Delay Due to Rotation 92-010 imum Induced Drag C92-118 Propfan Test Assessment Aircraft Safety Reconstruction of Flight Path in Turbulence 92-071 92-081 Escape Strategies for Turboprop Aircraft in Effect of Thrust Vectoring on Level-Turn Performance Microburst Windshear 92-126 Performance 92-074 Wing Mass Formula for Twin Fuselage Advanced Pneumatic Impulse Ice Protection Fighter Agility Metrics, Research and Test Aircraft 92-146 System (PIIP) for Aircraft O27-111 92-065 Optimization of Constant Altitude—Con- Range, Energy, Heat of Motion in the Agility as a Contrtio bDesuigtn oBalran ce stant Airspeed Flight of Turbojet Aircraft Modified NBC, Anti-g, Tank Suit 92-005 C92-119 92-099 Flight Model for Unmanned Simulated Hel- Effects of Ambient Turbulence on the Decay Flight Operations icopters 92-080 of a Trailing Vortex Wake (92-036 Flight Deck Aerodynofa a mNoinavciastio n Effect of Thrust Vectoring on Level-Turn Effect of Wind Shear on Airspeed i Ship 92-094 Performance 92-074 Airplane Landing Approach (92.933 J. AIRCRAFT, VOL. 29, NO. 6: 1992 INDEX Heat Transfer on Accreting Ice Surfaces Evaluation of Discrete Frequency Sound in Fluid Dynamics 92-015 Closed-Test-Section Wind Tunnels Forward-Look Wind-Shear Detection for 92-127 Aeroacoustics Microburst Recovery 92-008 Wind-Tunnel Compressor Stall Monitoring Using Neural Networks 92-121 Sonic Boom Environment Under a Super- Simulation Unsteady Crossflow on a Delta Wing Using sonic Military Operating Area 92-172 ting Lags in Head-Coupled Dis- Particle Image Velocimetry 92-108 Mitigation of Pressure Oscillations Induced plays Using Head Position Prediction and Airdata Calibration Techniques for Meas- by Supersonic Flow over Slender Cavities Image Deflection 92-171 uring Atmospheric Wind Profiles 92-096 92-162 Flight Model for Unmanned Simulated Hel- Remote Measurements of Supercooled In- Ground Impingement Noise of Supersonic tegrated Liquid Water During WISP/FAA Jets from Nozzles with Various Exit Ge- Robicuosptt erFsl ight Reconstruction for Heli9c2o-p0t8e0r Aircraft Icing Program 92-092 ometries 92-161 Flow over 2 Twin-Tailed Aircraft at Angle of Experimental Study of Noise Generation and Simulation and Training 92-061 Attack, Part II: Temporal Characteristics Propagation in a Turbofan Model Software Reliability for Flight Crew — Simulators 92-085 (92-144 Self-Compensating Carrier Aircraft icone. Calibration-Related Pseudo-Reynolds Num- Suppression of Fatigue-Inducing Cavity System 92-929 ber Trends in Transonic Wind Tunnels Acoustic Modes in Turbofan Engines Forward-Look Wind-Shear Detection for 92-084 92-113 Structure-Borne Noise Transmission in the Noise of Two High-Speed Model Counter- Microburst Recovery 92-008 Propfan Test Assessment Aircraft Rotation Propellers at Takeoff/Approach STOL/VTOL/STOVL 92-071 Conditions 92-103 Fighter Agility Metrics, Research and Test Ground Impingement Noise of Supersonic Boundary Layers and Heat 92-065 Jets from Nozzles with Various Exit Ge- Flow over a Twin-Tailed Aircraft at Angle of Transfer—Laminar ometries C92-161 Attack Part I: Spatial Characteristics Three-Dimensional Simulation of Electro- Flight Measurements of Downwash on the C92-060 thermal Deicing Systems 92-167 Ball-Bartoe Jetwing Powered Lift Aircraft Software Reliability for Flight Crew Training Heat Transfer Peculiarities in Supersonic 92-149 Simulators 92-052 Flows 92-158 Navier-Stokes Methods to Predict Circula- Ground-Testing Techniques for Tethered Heat Transfer Effects on Aerodynamics and tion Control Airfoil Performance C92-034 Systems 92-035 Implications for Wind-Tunnel Tests Evaluation of a Navier-Stokes Prediction of a Correction of Sideslip-Induced Static Pres- 92-031 Jet in a Crossflow 92-026 sure Errors in Flight-Test Measurements Twenty-Five Years of Aerodynamic Re- Hot Gas Environment Around STOVL Air- 92-016 search with Infrared Imaging 92-023 craft in Ground Proximity—Part 1: Ex- perimental Study 92-009 Vibration Boundary Layers and Heat Hot Gas Environment Around STOVL Air- Mitigation of Pressure Oscillations Induced Transfer—Turbulent craft in Ground Proximity—Part 2: Nu- merical Study 92-003 by Supersonic Flow over Slender Cavities Heat Transfer Peculiarities in Supersonic C92-162 Flows 92-158 Structural Design (Including Loads) Characteristic Differences Between the Data Analysis for Unsteady Turbulence Demonstration of Structural Optimization Modal Parameters of Cast and Forged Measurements over Airfoils 92-045 Applied to Wind-Tunnel Model Design Structures 92-076 Heat Transfer Effects on Aerodynamics and Effects of Higher Harmonic Control on Implications for Wind-Tunnel Tests 92-156 Coining of Holes in Aluminum Plates: Finite Rotor Performance and Control Loads C92-031 Element Simulations and Experiments C92-049 Twenty-Five Years of Aerodynamic Re- 92-152 Weather Hazards search with Infrared Imaging 92-023 Multidisciplinary Optimization of Aeroservo- Heat Transfer on Accreting Ice Surfaces elastic Systems Using Reduced-Size Assessment of Microburst Models for Down- 092-015 Models 92-151 draft Estimation 92-168 Wing Mass Formula for Twin Fuselage Predicting Droplet Impingement on Yawed Boundary-Layer Stability and Transition Wings 92-155 Aircraft C92-146 Design Optimization of Natural Laminar Wing Mass Formula for Subsonic Aircraft Escape Strategies for Turboprop Aircraft in Flow Bodies in Compressible Flow Microburst Windshear 92-126 C92-116 92-050 Characteristic Differences Between the Advanced Pneumatic Impulse Ice Protection Use of Shear-Sensitive Liquid Crystals for Modal Parameters of Cast and Forged System (PIIP) for Aircraft 092-111 Surface Flow Visualization 92-040 Assessment of One-Dimensional Icing Fore- Structures C92-076 Twenty-Five Years of Aerodynamic Re- Composite Material Repairs to Metallic cast Model Applied to Stratiform Clouds search with Infrared Imaging 92-023 Airframe Components 92-068 92-107 Transition Effects on Airfoil Dynamics and NASA Investigation of a Claimed ’Overlap’ Remote Measurements of Supercooled In- the Implications for Subscale Tests between Two Gust Response Analysis tegrated Liquid Water During WISP/FAA 39-169 Methods 90-105 Aircraft Icing Program 92-092 Aircraft-Triggered Lightning: Processes Fol- ComputatFluiido Dnynaamlic s Structural Materials lowing Strike Initiation that Affect Aircraft Multigrid Euler Calculations over Complete 92-088 Characteristic Differences Between the Hazard Evaluation and Operational Cockpit Aircraft (92-174 Modal Parameters of Cast and Forged Display of Ground-Measured Windshear Numerical Modeling of an Advanced Pneu- Structures 92-076 matic Impulse Ice Protection System for Data 92-047 Testing, Flight and Ground Forward-Look Wind-Shear Detection for Aircraft 92-170 Numerical Simulation of Re-Entry Flow Microburst Recovery 92-008 Unsteady Wind-Tunnel Interference in Air- NASA Investigation of a Claimed ’Overlap’ Around the Space Shuttle with Finite-Rate craft Dynamic Experiments 92-180 between Two Gust Response Analysis Three-Dimensional Simulation of Electro- Methods C90-105 thermal Deicing Systems 92-167 tion: Status and Trends Flight Measurements of Downwash on the Energy Aerodynamic Design via Optimization Ball-Bartoe Jetwing Powered Lift Aircraft 92-164 92-149 Rotating Machinery Unsteady Simulation of Viscous Flowfield High Angle-of-Attack Flush Airdata Sensing Around F-18 Aircraft at Large Incidence System 92-147 Compact Dynamometer System That Can C92-160 Model Flight Tests of a Spin-Resistant Accurately Determine Propeller Perform- "wae. Droplet Impingement on Yawed Trainer Configuration 92-133 ance C92-001 92-155 J. AIRCRAFT, VOL. 29, NO. 6: 1992 INDEX Calculation of Transonic Potential Prediction of Turbulent Flow Behavior over Sources of High Alpha Vortex Asymmetry at Flow Past Swept Wings (92-154 a Slotted Flap 92-007 Zero Sideslip 92-175 Viscous Flow Simulation of a Fighter Air- Hot Gas Environment Around STOVL Air- — Droplet Impingement on Yawed craft 92-143 craft in Ground Proximity—Part 2: Nu- 92-155 Euler/Experiment Correlation of a Generic merical Study 92-003 Suall Two-Dimensional Surface Excres- Fighter (92-139 Transition Effects on Airfoil Dynamics and cences on Aircraft Wings Approaching Navier-Stokes Simulation of a Close-Coupled the Implications for Subscale Tests Separation 92-145 Canard-Wing-Body Configuration C92-138 CB9-169 Wing Design for Hanggliders Having Min- Drag Computation by Vortex Methods imum Induced Drag 92-118 C92-136 Multiphase Flows Predicted Pressure Distribution on a Prop- Thin-Airfoil Correction for Panel Methods Remote Measurements of Supercooled In- Fan Blade Through Euler Analysis 92-115 tegrated Liquid Water During WISP/FAA 92-095 Design Load Predictions on a Fighter-Like Aircraft Icing Program 92-092 Prediction of Vortex Shedding from Fore- Aircraft Wing ©92-101 bodies with Chines 92-059 Simulation of Transonic Flow over Twin-Jet Rarefied Fiows Numerical Simulation of Leading-Edge Vor- Transport Aircraft 92-097 tex Breakdown Using an Euler Code Prediction of Inviscid Supersonic/Hyper- Direct Simulation of Low-Density Flow over 92-044 sonic Aircraft Flowfields 92-089 Airfoils 92-134 Experimental Study of a Low Reynolds Navier-Stokes Predictions for the F-18 Wing Separated Flows Number Tandem Airfoil Configuration and Fuselage at Large Incidence C92-087 92-032 Accurate Prediction of Drag Using Euler Buffet Excitation of Wings at Low Speeds Efficient Panel Method for Vortex Sheet Methods 92-077 92-182 Roll-Up 92-004 Wake Effects on the Prediction of Transonic Sources of High Alpha Vortex Asymmetry at Viscous Flows Around Airfoils (92-063 Zero Sideslip €92-175 Supersonic Flow Numerical Study of Vortex-Dominated Physical Modeling of Ground Effects on Application of Computational Fluid Dy- Flows for Wings at High Incidence and Vortex Wakes 92-166 namics to Sonic Boom Near- and Mid- Sideslip (92-058 Small Two-Dimensional Surface Excres- Field Prediction 92-148 Transonic Navier-Stokes Computations for cences on Aircraft Wings Approaching Prediction of Inviscid Supersonic/Hyper- an Oscillating Wing Using Zonal Grids Separation 92-145 sonic Aircraft Flowfields 92-089 92-048 Physics of Vortical Flows 92-141 Navier-Stokes Study of Supersonic Cavity Numerical Simulation of Leading-Edge Vor- Forcing Level Effects of Internal Acoustic Flowfield with Passive Control (92-030 tex Breakdown Using an Euler Code Excitation on the Improvement of Airfoil Computational Study of Incipient Leading- 92-044 Performance 92-137 Edge Separation on a Supersonic Delta Subsonic and Transonic Low-Reynolds- Suppression of Fatigue-Inducing Cavity Wing (92-028 Number Airfoils with Reduced poco Acoustic Modes in Turbofan Engines Canard-Wing Interaction in Unsteady Su- Moments 92-113 personic Flow 89-155 Navier-Stokes Methods to Predict Cucala. Self-Induced Roll Oscillations of Low-As- tion Control Airfoil Performance C92-034 pect-Ratio Rectangular Wings 92-106 Transonic Flow Navier-Stokes Study of Supersonic Cavity Forebody Vortex Control Using Small, Ro- Transonic Low-Reynolds Number Airfoils Flowfield with Passive Control 92-030 tatable Strakes 92-102 Evaluation of a Navier-Stokes Prediction of a Unsteady Aerodynamics of a Wortmann 92-178 Multigrid Euler Calculations over Complete Jet in a Crossflow 92-026 Wing at Low Reynolds Numbers C92-082 Separation Control Using Moving Surface Drag Reduction of Bluff Bodies = Aircraft (92-174 Aerodynamic Design via Optimization Effects: A Numerical Simulation C92-019 Momentum Injection Comparison of Two Navier-Stokes Codes for Design and Development of a Compacesibie Improved Calculation of Transonic Po9te2n-t1i6a4l Attached Transonic Wing Flows (92-014 Dynamic Stall Facility 92-046 Flow Past Swept Wings 92-154 Navier-Stokes Calculations of Inboard Stall Experimental Study of a Low Reynolds Unsteady Shock-Vortex Interaction on a Delay Due to Rotation 92-010 Number Tandem Airfoil Configuration Flexible Delta Wing 092-132 Hot Gas Environment Around STOVL Air- 92-032 Simulation of Transonic Flow over Twin-Jet craft in Ground Proximity—Part 2: Nu- Navier-Stokes Study of Supersonic Cavity Transport Aircraft 92-097 merical Study 92-003 Flowfield with Passive Control 92-030 Calibration-Related Pseudo-Reynolds Num- Computational Study of Incipient Leading- ber Trends in Transonic Wind Tunnels Hypersonic Flow Edge Separation on a Supersonic Delta Wing 92-028 92-084 — Scramjet Integration on a Wave- Interference Flows Past Cylinder-Fin-Sting- Transonic Aeroelasticity Analysis for Rotor on Simulation of Re-Entry C92F-l1o7w9 WiCnadv-iTtuyn nAesls emSbtiudiieess of F/A-18 Tail 9B2u-f0f2e7t WaBklea deEfsf ects on the Prediction of Tra9n2s-o0n6ic9 CAhreomuinsdt rtyh e Space Shuttle with Finit9e2--R1a6t9e Separation Control Using Moving S9u2r-f0a2c1e TraVnissocnoiucs FNlaovwise r-AStrookuensd CAoirmfpouitlsa tion9s2 -06fo3r Heat Transfer Peculiarities in Supersonic Effects: A Numerical Simulation C92-019 an Oscillating Wing Using Zonal Grids Flows C92-158 Approach to Side Force Alleviation Through 92-048 Subsonic and Transonic Low-Reynolds- Modification of the Pointed Forebody Inlet, Nozzle, Diffusor, and Channel Geometry 92-018 Number Airfoils with Reduced Pitching Flows Suppression of the Wing-Body Junction Moments 92-042 Numerical Computation of Improved Tran- Vortex by Body Surface Suction (92-017 Maximizing Thrust-Vectoring Control Power sonic Potential Method 92-025 Effects of Trailing-Edge Flap on Buffet and Agility Metrics 92-098 Transonic Aeroelasticity Analysis Using Characteristics of a Supercritical Airfoil Investigation of the Diffuser Flow Quality in State-Space Unsteady Aerodynamic Mod- an Icing Research Wind Tunnel (92-006 92-013 eling 92-022 Shock Waves and Detonations Comparison of Two Navier-Stokes Codes for Jets, Wakes, and Viscid-InviscFildow Attached Transonic Wing Flows (92-014 Interactions Sonic Boom Environment Under a Super- Effects of Trailing-Edge Flap on Buffet sonic Military Operating Area 92-172 Characteristics of a Supercritical Airfoil Transonic Low-Reynolds Number Airfoils Numerical Modeling of an Advanced Pneu- C92-013 C92-178 matic Impulse Ice Protection System for Unsteady Flows Unsteady Aerodynamics of a Wortmann Aircraft 92-170 Wing at Low Reynolds Numbers (92-082 Subsonic Flow byes |W ind-Tunnel Interference in Air- Hot Gas Environment Around STOVL Air- craft Dynamic Experiments 92-180 craft in Ground Proximity—Part 1: Ex- Propeller Slip-Stream Model in Subsonic Physical Modeling of Ground Effects on perimental Study 92-009 Linearized Potential Flow (92-177 Vortex Wakes 92-166 J. AIRCRAFT, VOL. 29, NO. 6: 1992 INDEX Unsteady Simulation of Viscous Flowfield Experimental Study of Vortex Flows over Dynamics Around F-18 Aircraft at Large Incidence Delta Wings in Wing-Rock Motion C92-160 C92-091 Longitudinal Stability Analysis of Aerial- Statistical Prediction of Maximum Buffet Navier-Stokes Computations on Swept-Ta- Towed Systems 92-159 Loads on the F/A-18 Vertical Fin pered Wings, Including Flexibility Flutter and Stall Response of a Helicopter 92-120 92-090 Biade with Structural Nonlinearity Time-Average Loading on a Two-Dimen- Navier-Stokes Predictions for the F-18 Wing 92-153 sional Airfoil in Large Amplitude Motion and Fuselage at Large Incidence C92-087 Flight Displays C92-109 Flow over a Twin-Tailed Aircraft at Angle of Unsteady Crossflow on a Delta Wing Using Attack, Part II: Temporal Characteristics ting Lags in Head-Coupled Dis- Particle Image Velocimetry 92-108 92-085 plays Using Head Position Prediction and Self-Induced Roll Oscillations of Low-As- Accurate Prediction of Drag Using Euler Image Deflection 092-171 pect-Ratio Rectangular Wings 92-106 Methods 92-077 Flight Mechanics Experimental Study of Vortex Flows over Flow over a Twin-Tailed Aircraft at Angle of Delta Wings in Wing-Rock Motion Attack Part I: Spatial Characteristics Maximizing Thrust-Vectoring Control Power (92-091 92-060 and Agility Metrics 92-098 Navier-Stokes Computations on Swept-Ta- Prediction of Vortex Shedding from Fore- Identification of the Transfer Function Be- pered Wings, Including Flexibility bodies with Chines 92-059 tween Turbulence and Aircraft (92-057 92-090 Numerical Study of Vortex-Dominated Unsteady Aerodynamics of a Wortmann Flows for Wings at High Incidence and Optimization Techniques Wing at Low Reynolds Numbers C92-082 Sideslip 92-058 Unsteady Aerodynamic Loading Produced Unsteady Aerodynamic Loading Produced Aerodynamic Design via Optimization by a Sinusoidally Oscillating Delta Wing by a Sinusoidally Oscillating Delta Wing 92-164 92-054 92-054 State Estimation Transonic Navier-Stokes Computations for Numerical Simulation of Leading-Edge Vor- an Oscillating Wing Using Zonal Grids tex Breakdown Using an Euler Code Robust Flight Reconstruction for Helicopter 92-048 92-044 Simulation and Training 92-061 Design and Development of a Compressible Effects of Ambient Turbulence on the Decay Dynamic Stall Facility 92-046 of a Trailing Vortex Wake 92-036 System Identification Data Analysis for Unsteady Turbulence Effect of Wind Shear on Airspeed During Reconstruction of Flight Path in Turbulence Measurements over Airfoils 92-045 Airplane Landing Approach 92-033 (92-081 Interference Flows Past Cylinder-Fin-Sting- Computational Study of Incipient Leading- Identification of the Transfer Function Be- Cavity Assemblies 92-027 Edge Separation on a Supersonic Delta tween Turbulence and Aircraft (92-057 Wind-Tunnel Studies of F/A-18 Tail Buffet Wing 92-028 92-021 Approach to Side Force Alleviation Through Trajectory Optimization Effects of Trailing-Edge Flap on Buffet Modification of the Pointed Forebody Characteristics of a Supercritical Airfoil Geometry 92-018 Control Strategy for Maximizing Reconnais- 92-013 Suppression of the Wing-Body Junction sance Range of Hypersonic Cruise Vehi- Rapid Prediction of High-Alpha Unsteady Vortex by Body Surface Suction C92-017 cles 92-053 Aerodynamics of Slender-Wing Aircraft Rapid Prediction of High-Alpha Unsteady Interdisciplinary Topics 92-012 Aerodynamics of Slender-Wing Aircraft Transition Effects on Airfoil Dynamics and 92-012 the Implications for Subscale Tests Efficient Panel Method for Vortex Sheet Aerospace Management 89-169 Roll-Up 92-004 Structural Risk Assessment in the Israel Air Force for Fleet Management 92-083 Viscous Non-Boundary-Layer Flows Guidance, Control, and Dynamics Viscous Flow Simulation of a Fighter Air- Technology Aerospace Technology Utilization craft 92-143 High Angle-of-Attack Flush Airdata Sensing Physics of Vortical Flows 92-141 Aircraft Dynamics System 92-147 Drag Computation by Vortex Methods Analytical Modeling of SH-2F Helicopter C92-136 Shipboard Operation 92-142 Analanyd Ntumeiriccal aMeltho ds Vortices System for Generating Sequences of Phased Numerical Modeling of an Advanced Pneu- Gust or Taxi Loadings 92-104 matic Impulse Ice Protection System for Wind-Tunnel Investigation of a Fighter Aircraft 92-170 Model at High Angles of Attack C92-176 Aircraft Guidance Application of Advanced Multidisciplinary Physical Modeling of Ground Effects on Microwave Landing System Modeling with Analysis and Optimization Methods to Voriex Wakes 92-166 Application to Air Traffic Control Au- Vehicle Design Synthesis 92-135 Unsteady Simulation of Viscous Flowfield tomation 92-051 Numerical Study of Vortex-Dominated Around F-18 Aircraft at Large Incidence Flows for Wings at High Incidence and C92-160 Aircraft Stability and Control Sideslip 92-058 Physics of Vortical Flows 92-141 Longitudinal Stability Analysis of Aerial- Two-Fence Concept for Efficient Trapping Towed Systems 92-159 Atmosapndh Speacer Siciecnce s NavoCifae nrVa-orSrtdtoi-kcWeeissn gSo-inBm ouAdliayrt fiooiCnlos n offi gau rCaltoisoen- Co9Cu922p--l11e43d08 DApopCwloninwctaratosilho n Suforofrf acAJeco tiinDveeef dl-eFWclitenxigiob nlse A irWfirnagm e9 2T-ew0ci6ht6-h Assdreasfstm eEnstt iomfa tMiiocnr oburst Models for 9D2o-w1n6-8 Drag Computation by Vortex Methods nology to the Agile Falcon 92-064 Asscaessts mMeontd elo f AOpnpel-iDeidm etnos iSotnraatli foIrcmi ngC lFoourdes- 92-136 Analysis of Airship Lateral Maneuverability UnsFlteexaidbyle SDhelotcak -VWoirntge x Interaction 92o-n1 32a Artificial Intelligence 92-043 Airudraitnag ACtamliobsrpahteiroinc TWeichnndi quPerosf ilefso r 9C92M2-e-1a00s97-6 Effect of Nose-Boom on Forebody Vortex Flow 92-122 Wind-Tunnel Compressor Stall Monitoring Establishing a Database for Flight in the Pitch Rate/Sideslip Effects on Leading-Edge Using Neural Networks 92-121 Wakes of Structures 92-086 Extension Vortices of an F/A-18 Aircraft Expert System for Real-Time Aircraft Mon- Human Factors Model (92-114 itoring 092-011 Suppression of Fatigue-Inducing Cavity ting Lags in Head-Coupled Dis- Acoustic Modes in Turbofan Engines Control System Design plays Using Head Position Prediction and 92-113 Multidisciplinary Optimization of Aeroservo- Image Deflection 92-171 Forebody Vortex Control Using Small, Ro- elastic Systems Using Reduced-Size Nine-Degree-of-Freedom Simulation of Ro- tatable Strakes 92-102 Models 92-151 tating Parachute Systems 92-130 J. AIRCRAFT, VOL. 29, NO. 6: 1992 INDEX Range, Energy, Heat of Motion in the Compact Dynamometer System That Can Composite Material Repairs to Metallic Modified NBC, Anti-g, Tank Suit — Determine Propeller Perform- Airframe Components 92-068 92-099 92-001 Canard-Wing Interaction in Unsteady Su- Improved Measurement of the Dynamic personic Flow 89-155 Ramjaned Stcrasmje ts Loads Acting on Rotating Parachutes Structural Dynamics and 92-067 Thermal Managfore am Maech n5 Ctrui se Hazard Evaluation and Operational Cockpit AircUsinrg aEndfothterm ic Fuel C92-056 Characterization Display of Ground-Measured Windshear Response of Double-Wall (Sandwich) Cir- Data 92-047 Structural Mechanics and Materials cular Plates to Random Excitations—An- Reliability, Maintainabilitya,n d alytical Approach 92-150 Logistics Support Aeroelastaindc Cionttyro l Aeroelastic Effects of Spoiler Surfaces on a Low-Aspect-Ratio Rectangular Wing Structural Risk Assessment in the Israel Air Unsteady Shock-Vortex Interaction on a 92-129 Force for Fleet Management 92-083 Flexible Delta Wing 92-132 Reduced Basis Alternatives to the Solution of Composite Material Repairs to Metallic Aeroelastic Effects of Spoiler Surfaces on a Nonlinear Dynamical Systems 92-128 Airframe Components 92-068 Low-Aspect-Ratio Rectangular Wing Statistical Prediction of Maximum Buffet 92-129 Loads on the F/A-18 Vertical Fin Research Facilities and Instrumentation Statistical Prediction of Maximum Buffet 92-120 Loads on the F/A-18 Vertical Fin Experimental-Theoretical Investigation of Reconsof tFlirghtu Pacth tini Tuorbunlen ce 92-120 the Vibration Characteristics of Rotating 92-081 Whirl-Flutter Stability of a Pusher Config- Composite Box Beams 92-100 Invesof tthei Difgfusaer tFloiw Qoualnity in uration in Nonuniform Flow 92-117 Nonlinear Flutter of Two-Dimensional Sim- an Icing ResearcWihnd Tunnel (92-006 Transition of the Flutter Mode of a Two- ply Supported Symmetric Composite Lam- Safety Dimensional Section with an External inated Plates 92-020 Store 92-075 Structural Finite Hements Range, Energy, Heat of Motion in the Coalescence of Aeroelastic Modes in Flutter Modified NBC, Anti-g, Tank Suit Analysis 92-072 Coining of Holes in Aluminum Plates: Finite 92-099 Application of Active Flexible Wing Tech- Element Simulations and Experiments Hazard Evaluation and Operational Cockpit nology to the Agile Falcon 92-064 92-152 Display of Ground-Measured Windshear Integrated Aeroelastic Control Optimization Structural and Aerodynamic Data Trans- Data 92-047 of Laminated Composite Lifting Surfaces formation Using Inverse Isoparametric 92-039 Mapping 92-073 Sensor Systems Low-Speed Flutter Characteristics of Some Simple Low-Aspect-Ratio Delta-Wing Structural Modeling Correction of Sideslip-Induced Static Pres- sure Errors in Flight-Test Measurements Models C92-038 Response of Double-Wall (Sandwich) Cir- Wind-Tunnel Studies of F/A-18 Tail Buffet cular Plates to Random Excitations—An- C92-016 92-021 alytical Approach 92-150 Launch Vehicle and Missile (LV/M) Approach for Analysis and Design of Com- DynaModmel iAnaclys is posite Rotor Blades 92-105 Technology Analytical Modeling of SH-2F Helicopter Structural Optimization Shipboard Operation 92-142 Aerodynamics System for Generating Sequences of Phased Demonstration of Structural Optimization Aerodynamic Forces on Noncircular Cross- Gust or Taxi Loadings 92-104 Applied to Wind-Tunnel Model Design Section Missile Forebodies 92-093 Transition of the Flutter Mode of a Two- 92-156 Structurai and Aerodynamic Data Trans- Dimensional Section with an External Application of Advanced Multidisciplinary Analysis and Optimization Methods to formation Using Inverse Isoparametric Store 92-075 Mapping 92-073 Vehicle Design Synthesis (92-135 Interference Flows Past Cylinder-Fin-Sting- Fleanxd Aictibve lStruectur es Integrated Aeroelastic Control Optimization Cavity Assemblies 92-027 of Laminated Composite Lifting Surfaces Approach to Side Force Alleviation Through Wing Design for Hanggliders Having Min- 92-039 imum Induced Drag 92-118 Modification of the Pointed Forebody Thermal Effects Geometry 92-018 Structural Composite Materials Acoustic Testing of High-Temperature Configurational Design Approach for Analysis and Design of Com- Panels (92-181 posite Rotor Blades 092-105 Thermal Structures: Four Decades of AeroFdorceys non Naoncimrcuilar cCro ss- Experimental-Theoretical Investigation of Progress 92-070 Section Missile Forebodies 92-093 the Vibration Chdracteristics of Rotating Thermophysics and Heat Transfer TesFtligiht nandg Gr,ou nd Composite Box Beams 92-100 Nonlinear Flutter of Two-Dimensional Sim- Airdata Calibration Techniques for Meas- ply Supported Symmetric Composite Lam- AerothermodTyhenrmaalm iProctesct/io n uring Atmospheric Wind Profiles C92-096 inated Plates 92-020 Thermal Structures: Four Decades of Pro- Ground-Testing Techniques for Tethered gress 92-070 Systems 92-035 ee ee anne ee and Fracturaned ,E n Forced Convection Propulsion Degradation) Heat Transfer on Accreting Ice Surfaces Acoustic Testing of High-Temperature 92-015 Airbreathing Propulsion Panels (92-181 Melting/ Solidification Thermal Management for a Mach 5 Cruise Coining of Holes in Aluminum Plates: Finite Aircraft Using Endothermic Fuel €92-050 Element Simulations and Experiments Three-Dimensional Simulation of Electro- Control Strategy for Maximizing Reconnais- 92-152 thermal Deicing Systems 92-167 sance Range of Hypersonic Cruise Vehi- System for Generating Sequences of Phased Thermal Modeling and Analysis cles 92-053 Gust or Taxi Loadings 92-104 Preliminary Sizing Methodology for Hyper- Structural Risk Assessment in the Israel Air Thermal Structures: Four Decades of sonic Vehicles 92-024 Force for Fleet Management 92-083 Progress 92-070 J. AIRCRAFT, VOL. 29, NO. 6: 1992 INDEX Author Index Addy, H. E., Jr., C92-006 Dunn, P. F., C92-001 Lan, C. E., ©92-074 Agrawal, S., 92-101 Durck, C. H., C92-099 Larson, T. J., C92-147 Alhusein, M. A., 92-145 Eastin, R. G., C92-104 Lawrence, S. L., C92-148 Amato, M., C92-063 Edwards, T. A., C92-148 Leatherwood, J. D., C92-181 Anderson, W. J., C92-116, C92-146 Eggold, D. P., C92-065 Lee, B. H. K., C92-013, C92-021, Asson, K. M., C92-001 Engblom, !. J., C92-128 92-120 Aulehla, F., C92-084 Epstein, B., C92-174 Lee, C. K., C92-037 Bach, R. E., Jr., C92-016 Ericsson, L. E., C89-169, C92-012, Lee, K. D., C92-164 Bailey, J. E., C92-061 (92-175 Lee, M., C92-064 Baitis, E., C92-142 Est, B. E., C92-093 Lee, P., C92-074 Barnett, R. M., C92-044 Etkin, B., C90-105 Leedy, D. H., €92-176 Baysal, O., C92-027 Eyi, S., C92-164 Leffel, K. L., C92-170 Becker, K., C92-097 Fearn, R. L., C92-026 Leishman, J. G., C92-022 Belcher, P. J., C92-053 Flanders, J. B., C92-011 Lerwick, T. R., C92-104 Benner, R. H., C92-113 Fouladi, K., C92-027 Lesieutre, D. J., C92-059 Beyers, M. E., C92-180 Franke, M. E., C92-034 Leung, R. W., C92-027 Bismarck-Nasr, M. N., C92-072 French, M., C92-156 Levin, D., C92-067, C92-106 Blacodon, D., C92-173 Fuglsang, D. F., C92-101 Lewis, L. C., C92-091 Bobbitt, R. B., C92-126 Gal-Or, B. Z., C92-098 Lewis, M. J., C92-179 Bofilios, D. A., C92-150 Gartenberg, E., C92-023 Léwy, S., C92-144, C92-173 Bonhaus, D. L., C92-014 Garza, R. G., C92-172 Liefer, R. K., C92-065 Boronow, W., C92-167 Gea, L., C92-069 Lin, Y., C92-081 Borovoy, V. Y., C92-158 Gee, K., C92-160 Liou, S. G., C92-060 Bragg, M. B., C92-155 Goodsell, A. M., C92-139 Liu, C. H., 92-058 Brazhko, V. N., C92-158 Graham, G. M., C92-109 Liu, H.-T., C92-036, C92-082, 92-166 Brodersen, R., C92-029 Grandhi, R. V., C92-053 Lo, C. F., €92-121 Brown, D., C92-02i Griffin, M. J., C92-171 Loewy, R. G., C92-131 Burkhalter, J. E., C92-066 Guruswamy, G. P., C92-048, Létstedt, P., C92-177 Butler, B. E., C92-080 C92-090, C92-132 Louie, C. M., C92-044 Canard-Caruana, S., C92-144 Gutmark, E., C92-162 Lowson, M. V., C90-108 Carr, L. W., C92-046 Haering, E. A., Jr., C92-096 Lu, L., €92-020 Carter, J., C92-115 Hammond, D. O., C92-068 Lucas, M. J., C92-172 Caughey, D. A., C92-154 Hankey, W. L., C92-053 Luntz, A., C92-174 Cavazos, O. V., C92-114 Hansman, R. J., Jr., C92-015, Luttges, M. W., (92-054 Lyrintzis, C. S., C92-150 Cenko, A., C92-035 92-047 Chaderjian, N. M., C92-048, C92-087 Harris, R. V., Jr., C92-002 Mabey, D. G., C89-169, C92-031 Chandra, R., C92-100 Hassan, A. A., C92-019 Macedo Moura, G. A., C92-105 Chandrasekhara, M. S., C92-046 Healey, J. V., C92-086, C92-094 MacLean, R., C92-009 Chang, C. L., C92-128 Hebbar, S. K., C92-114, C92-176 Madison, R. M., C92-011 Chang, I-Chung, C92-069 Heragu, S. S., C92-007 Magness, C., C92-108 Chang, J., C92-112 Hicks, R., C92-042 Maikapar, G. I., C92-158 Chang, R. C., C92-137 Hinton, D. A., 92-008 Malcolm, G. N., C92-091, C92-102 Chaput, A. J., C92-024 Howard, R. M., C92-045, C92-126 Malloy, P. J., C92-101 Chattopadhyay, A., C92-041 Hsiao, F.-B., C92-137 Martin, C. A., C92-111, C92-170 Hsu, C.-H., €92-058 Martinez-Val, R., C92-110 Humi, M., C92-136 Mastropaolo, J. A., C92-099 Huyer, S. A., C92-054 Mathew, M. B., C92-131 Hwang, P. A., C92-166 Maull, D. J., C92-182 Tlacqua, P. N., C92-045 Mazur, V., C92-088 Christian, T. F., Jr., C92-068 Islam, M., C92-109 McMillin, S. N., C92-028 Cimbala, J. M., C92-017 Jackson, P. S., C92-115 Mendenhall, M. R., C92-059 Clessas, G., C92-035 Johnson, D. K., C92-045 Metzger, F. B., C92-095 Clevenson, S. A., C92-181 Jones, C. H., C92-011 Meyers, W., C92-142 Cochran, J. B., C92-068 Jones, H., C92-041 Modi, V. J., C92-018, C92-062 Cockrell, D. J., C92-145 Jones, S. C., C92-056 Moes, T. R., ©92-147 Coiro, D. P., C92-063 Julliard, J., C92-144 Mohler, S. H., Jr., C92-155 Cole, S. R., C92-129 Moreau, J., C92-088 Consoli, R. D., C92-135 Mosher, M., C92-127 Crouse, G. L., Jr., C92-022 Moulton, C. L., C92-172 Cummings, R. M., C92-087 Mueller, T. J., C92-032 Daniels, E. F., C92-181 Murthy, S. N. B., C92-009 de Gaston, A. N., C92-099 Keith, T. G., Jr., C92-006, C92-167, Nachshon, A., C92-174 de Matteis, P., C92-063 92-170 Nagabhushan, B. L., C92-043 De Witt, K. J., C92-167, C92-170 Key, M. K., C92-066 Nakagawa, N., C92-159 Délery, J. M., C92-141 Kim, I., C92-030 Narramore, J. C., C92-010 Desai, V. R., C92-172 Kim, J. M., C92-060, C92-085 Nelson, H. F., €92-093 Dodbele, S. S., C92-050 King, H. H. C., C92-012 Ng, T. T., C92-091, C92-102, C92-122 Doggett, R. V., Jr., C92-038 Kobayakawa, M., C92-095 Nguyen, K., €92-049 Doherr, K., C92-130 Kolar, R., C92-105 Nikfetrat, K., C92-077 Dowell, E. H., C92-153 Kolonay, R. M., C92-156 Nitzsche, F., C92-117 Downing, D. R., C92-065 Kor:erath, N. M., C92-060, C92-085 Norum, T. D., C92-161 los, T. N., C92-039 KrishnaKumar, K., C92-061 Obata, A., C92-159 Drela, M., C92-178 Kubota, H., C92-169 Obayashi, S., C92-132 Dulikravich, G. S., C92-165 Kwon, O. J., C92-143 Ogeman, R., C92-152 Dunlavy, S., C92-120 Lamarre, F., C92-004 Ojha, S. K., C92-119 J. AIRCRAFT, VOL. 29, NO. 6: 1992 INDEX O’Neil, P. J., C92-044 Sankar, L. N., C92-019, C92-143 Thakur, S. S., C92-026 O’Neill, M. K. L., 92-179 Sauer, G., C92-029 Thomas, J. L., C92-028 Oz, H., €92-039 Schadow, K. C., C92-162 Thornton, E. A., C92-070 Panossian, H. V., C92-076 Schanzer, G., C92-057 Tidd, D. M., C92-174 Paraschivoiu, I., C92-004 Scharpf, D. F., C92-032 Tran, D., C92-016 Parks, E. K., C92-016 Schiff, L. B., C92-087 Treaster, A. L., C92-017 Pasha, R. P. K., C92-043 Schilling, H., 92-130 Tu, E. L., 92-138 Pendleton, E., 92-064 Schwartz, R. J., C92-060, C92-085 Tunick, A., C92-107 Perez, E., C92-110 Sheftic, J. S., C92-027 Udin, S. V., C92-116, C92-146 Perry, B., ITI, C90-105 Shi, G. Z., C92-121 Unruh, J. F., C92-071 Peters, D. A., C92-055 Shiau, L., C92-020 Valasek, J., C92-065 Petley, D. H., C92-056 Shih, E., C92-062 van Dam, C. P., C92-042, C92-077 Philips, D. B., C92-017 Shpund, Z., C92-067 Van Santen, A. R., C92-099 Phillips, K., €92-035 Shyu, R.-N., 92-137 Vanka, S. P., C92-003 Pidaparti, R. M. V., C92-073 Skow, A. M., C92-005 Verhoff, A., C92-089 Pittman, J. L., C92-028 Skuratov, A. S., C92-158 Vermeland, R., C92-010 Platzer, M. F., C92-114 Smith, R. A., C92-162 Vicroy, D. D., C92-168 Plotkin, K. J., C92-172 Smith, S. C., C92-040 Wada, Y., C92-169 Pototzky, A. S., C90-105 Snider, J. B., 92-092 Wang, L., C92-154 Poulose, M. M., C92-051 So, R. H. Y., €92-171 Wanke, C., C92-047 Powell, C. A., C92-181 Sobieszczanski-Sobieski, J., C92-135 Wasserman, L., C92-064 Prasanth, R. K., C92-061 Soedel, S. M., 92-104 Weber, R. L., C92-092 Putt, J. C., C92-111, C92-170 Soistmann, D. L., C92-038 Wei, F., C92-142 Rachele, H., C92-107 Solies, U. P., C92-149 Westwater, E. R., C92-092 Ramamurthy, S., C92-170 Spence, P. L., C92-163 White, R. J., C92-033 Reuther, J., C92-642 Spring, D. J., C92-066 Whitmore, S. A., (92-147 Rhoades, M. M., C92-094 Srnsky, R. A., C92-166 Williams, S. L., C92-034 Rill, S., C92-097 Stankov, B. B., 92-092 Woods, J. A., C90-105 Rizk, Y. M., C92-087, C92-160 Stark, G. E., C92-052 Woodward, R. P., C92-103 Robelen, D. B., €92-133 Stark, V. J. E., Ce9-155 Wornom, S. F., C92-014 Roberts, A. S., Jr., C92-023 Stewart, A. C., C92-018 Xue-Song, B., C92-025 Robinson, M. C., C92-054 Stookesberry, D., €92-089 Yamaguchi, K., C92-015 Robinson, O., C92-108 Strash, D. J., C92-174 Yang, Z., C92-075 Rockwell, D., C92-108 Struminskaya, I. V., C92-158 Yaslik, A. D., C92-167 Rodrigues, E. A., C92-117 Su, A., C92-055 Ying, B., C92-062 Rosen, A., C92-131 Sugimoto, T., C92-118 Yip, L. P., C92-133 Ross, H. M., C92-133 Sullivan, J., C92-009 Yokomizo, T., C92-062 Rossow, V. J., C92-140 Tafti, D. K., C92-003 Yoo, K. M., C92-055 Roth, K. R., C92-026 Tai, T. C., C92-134 Yosibash, Z., C92-083 Rubin, T., (92-174 Takaki, R., C92-095 Zan, S. J., C92-182 Sadeck, J. E., C92-037 Tang, D. M., C92-153 Zhao, L., C92-075 Zi-qiangq, Z., C92-025 Zotto, M., C92-131

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