Table Of ContentJOURNAL OF AIRCRAFT
Volume 37, No. 6, November—December 2000
ft
2000 Journal of Aircraft Index
How to Use the Index
In the Subject Index, pages 1123-1128, each technical paper is listed under a maximum of three appropriate headings. Note
the locating number in boldface type preceding each paper title, and use that number to find the paper in the Chronological
Index. The Author Index, pages 1129-1130, lists all authors associated with a given technical paper. The locating numbers are
identical to those in the Subject Index. The Chronological Index, pages 1131-1136, also lists all papers by their locating num-
bers. 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 ISBN number if the paper was pub-
lished 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 2000, that paper also will appear in both the Subject and
Chronological Indexes. Authors of Comments also are listed in the Author Index.
Subject Index
Aircraft Technology, Conventional, C00-067 Eigenmode Analysis and Reduced- C00-123 Low Reynolds Number Aerodynamics
STOL/VTOL Order Modeling of Unsteady Transonic Potential of Low-Aspect-Ratio, Thin/Flat/Cambered-Plate
Flow Around Airfoils Wings
Aerodynamics C00-103 Experimental Geometry Optimization C00-033 Measurements of Bound and Wake
C00-156 New Fully Automated Procedure for Techniques for Multi-Element Airfoils Circulation on a Helicopter Rotor
the Prediction of Store Trajectory C00-005 Experiments on a 60-Degree Delta C00-097 Modern Adaptation of Prandtl’s Clas-
C00-122 A Solution-Adaptive Unstructured Wing with Rounded Leading-Edge Vortex Flaps sic Lifting-Line Theory
C00-096 Navier-Stokes Computation of a
Grid Method by Grid Subdivision and Local C00-153 Exploratory Study of Aircraft Wake
Rapidly Deploying Spoiler
Remeshing Vortex Filaments in a Water Tunnel
C00-007 New Model for Vortex Decay in the
C00-039 Acoustics and Unsteady Flow of Tele- C00-107 Fast and Robust Viscous/Inviscid Inter-
Atmosphere
scope Cavity in an Airplane action Code for Wing Flowfield Calculations
C00-082 Numerical Analysis of a Finite Wing
C00-163 Aerodynamic and Aeroacoustic Opti- C00-058 Fixed-Pitch Propeller Selection for
Altered by a Leading-Edge Ice Accretion
mization of Rotorcraft Airfoils Via a Parallel Light Airplanes C00-052 Numerical Evaluation of Airfoil Fric-
Genetic Algorithm C00-028 Flight-Test Techniques Employed to tion Drag
C00-104 Aerodynamic Characteristics of Span- Successfully Verify F/A-18E In-Flight Lift and C00-069 Numerical Simulation of Transonic
wise Cambered Delta Wings Drag Flow over Wing-Mounted Twin-Engine Trans-
C00-158 Aerodynamics of a Single Element C00-091 Flow Control for an Airfoil with Lead- port Aircraft
Wing in Ground Effect ing-Edge Rotation: An Experimental Study C00-050 Origin of Vortex Wandering over Delta
C00-041 Aerodynamics of Gurney Flaps on a C00-064 Ground Effect Characteristics of a Wings
Single-Element High-Lift Wing Two-Dimensional Hypersonic Configuration C00-146 Overview of Wake-Vortex Hazards
C00-068 Characteristics of Transonic Rectangu- C00-135 Helical-Groove and Circular-Trip During Cruise
lar Cavity Flows Effects on Side Force C00-149 Particle Image Coelimetry (PIV) Mea-
C00-141 Comparison of Deterministic and Sto- C00-120 Hover Performance Prediction Using surements of Exhaust Gas Ingestion Relevant to
chastic Optimization Algorithms for Generic Full-Potential Method and Comparison with STOVL Aircraft
Wing Design Problems Experiments C00-108 Proposed Mechanism for Time Lag of
C00-092 Comparison of Induced Velocity Mod- Vortex Breakdown Location in Unsteady Flows
C00-083 Implications of Recent Rotary Rig
els for Helicopter Flight Mechanics C00-137 Results of Theodorsen and Garrick
Results for Flight Prediction
C00-147 Conceptual Design Studies of a Strut- Revisited
C00-078 Implications of the Insensitivity of Vor-
Braced Wing Transonic Transport C00-102 Robust Vortex Control of a Delta Wing
tex Lift to Sweep
C00-095 Convergent-Flow-Derived Waveriders by Distributed Microelectromechanical-Systems
C00-100 Design and Predictions for a High- C00-024 Improvement of a Wing’s Aerodynam- Actuators
Altitude (Low Reynolds Number) Aerodynamic ic Efficiency Using Coanda Tip Jets C00-031 Simulated Flowfields in Near-Ground
Flight Experiment C00-008 Influence of Aspect Ratio on the Per- Operation of Single- and Twin-Rotor Configura-
C00-029 Effect of External Components on V- formance of Outboard-Horizontal-Stabilizer Air- tions
22 Aircraft Forward-Flight Aerodynamics craft C00-116 Smali Disturbance Euler Equations:
C00-121 Effect of Sweep on Buffet over Novel C00-006 Investigation of High-Lift Flowfield of Efficient and Accurate Tool for Unsteady Load
Wing Planforms an Energy Efficient Transport Wing Prediction
00-042 Effects of Anhedral and Dihedral on a C00-157 Lift Augmentation on a 60 Delta Wing C00-105 Tailoring Lift/Drag Ratio for a Lifting-
75-deg Sweep Delta Wing with Leading-Edge Fences and a Gurney Flap Body Airplane Configuration
1123
1124 J. AIRCRAFT, VOL. 37, NO. 6: 2000 INDEX
C00-161 Transition of Subsonic and Transonic Cabin Environment, Crew Training, and Landing Dynamics
Expansion-Corner Flows Life Support
C00-090 Testing of a Semiactive Landing Gear
C00-027 Transonic and Low-Supersonic
Aerodyanmic Analysis of a Wing with Underpy- C00-065 Analysis of Evacuation Strategies for Control for a General Aviation Aircraft
lon/Store Design and Certification of Transport Airplanes Lighter-Than-Air Systems
C00-101 Unsteady Aerodynamics of a Wing-In-
Ground-Effect Airfoil Flying over a Wavy Wall Civil Missions and Transportation C00-093 Equations of Motion of a Vehicle in a
C00-160 Validation and Operation of a Vortex- C00-003 Cost Analysis of the Departure—-En Moving Fluid
Wake/Shear Interaction Model Route Merge Problem Man/Machine Interface
C00-057. Wind Tunnel Tests of a High Lift Gen-
eration and Stall/Spin Recovery System Communication and Air Traffic Control C00-088 Modeling Human Pilot Cue Utilization
C00-001_ Wind-Tunnel Techniques to Success- C00-003 Cost Analysis of the Departure—En with Applications to Simulator Fidelity Assess-
fully Predict F/A-18E In-Flight Lift and Drag Route Merge Problem ment
C00-055 Wind-Tunnel Tests of an Aircraft Tur- C00-061 Evaluation of Scheduling Methods for C00-144 Influence of Icing Information on Pilot
ret Model Multiple Runways Strategies for Operatingin Icing Conditions
Aeroelasticity and Aeroservoelasticity Configuration Design Manufacturing
C00-022 Aeroelastic Sensitivity Analyses for C00-051 Conceptual Aircraft Design Based on a C00-017 Linking Riveting Process Parameters
Flutter Speed and Gust Response to the Fatigue Performance of Riveted Aircraft
Multiconstraint Genetic Optimizer
C00-164 Aeroelastic Tailoring of Composite Structures
C00-147. Conceptual Design Studies of a Strut-
Aircraft Wings Exhibitng Non-Classical Effects
and Carrying External Stores Braced Wing Transonic Transport Military Missions
C00-008 Influence of Aspect Ratio on the Per-
C00-113 Aeroservoelastic Analysis of the B-2 C00-106 Database Tomography Applied to an
Bomber formance of Outboard-Horizontal-Stabilizer Air-
Aircraft Science and Technology Investment
C00-068 Characteristics of Transonic Rectangu- craft
Strategy
lar Cavity Flows C00-105 Tailoring Lift/Drag Ratio for a Lifting-
C00-079 Control of a Three Degree-of-Freedom Body Airplane Configuration Noise
Airfoil with Limit-Cycle Behavior C00-057 Wind Tunnel Tests of a High Lift Gen-
C00-034 Model Helicopter Rotor Aerodynamics
C00-025 Divergence of an Inflated Wing eration and Stall/Spin Recovery System
and Acoustics As Measured in Two Anechoic
C00-067 Eigenmode Analysis and Reduced-
Flight Control Integration Wind Tunnels
Order Modeling of Unsteady Transonic Potential
C00-118 Prediction Measurement of a Low-Fre-
Flow Around Airfoils C00-124 Reduced-Order Dynamic Aeroelastic
C00-125 Euler-Based Dynamic Aeroelastic Model Development and Integration with Non- quency Harmonic Noise of Hovering Model
Analysis of Shell Structures linear Simulation Helicopter Rotor
C00-040 Evaluation of Computational Algo- C00-021 Stiffener Shape Design to Minimize
rithms Suitable for Fluid-Structure Interactions Flight Mechanics Interior Noise
C00-136 Limit Cycle Oscillation Characteristics C00-038 Systems Analysis of Noise Abatement
C00-099 Aerodynamic Sensitivity Theory for
of Fighter Aircraft Procedures Enabled by Advanced Flight Guid-
Rotary Stability Derivatives
C00-115 Limit Cycle Oscillation Flight Test ance Technology
C00-049 Aerodynamic Suppression of Wing
Results of a Fighter with External Stores
Rock Using Fuzzy Logic Control Performance
C00-114 Nonlinear Aeroelastic Analysis of
C00-066 Angular Momentum Control in Non-
Complete Aircraft in Subsonic Flow C00-028 Flight-Test Techniques Employed to
C00-020 Nonlinear Aeroelastic Response of linear Flight Successfully Verify F/A-18E In-Flight Lift and
Delta Wing to Periodic Gust C00-112 Bounded-Variable Gauss-Newton Drag
C00-126 Optical Measurements of Flutter Mode Algorithm for Aircraft Parameter Estimation C00-008 Influence of Aspect Ratio on the Per-
Shapes C00-092 Comparison of Induced Velocity Mod- formance of Outboard-Horizontal-Stabilizer Air-
C00-133 Optimization of Flexible Wing Without els for Helicopter Flight Mechanics craft
Ailerons for Rolling Maneuver C€00-091 Flow Control for an Airfoil with Lead- C00-089 Optimization of Balanced Field Length
C00-124 Reduced-Order Dynamic Aeroelastic ing-Edge Rotation: An Experimental Study Performance of Multi-Engine Helicopters
Model Development and Integration with Non- C00-109 Grid Survey Approach to Store Separa- C00-001 Wind-Tunnel Techniques to Success-
linear Simulation tion Trajectory Prediction fully Predict F/A-18E In-Flight Lift and Drag
C00-137 Results of Theodorsen and Garrick C00-135 Helical-Groove and Circular-Trip
Revisited Effects on Side Force Powerplant Integration
C00-116 Small Disturbance Euler Equations: C00-083 Implications of Recent Rotary Rig C00-064 Ground Effect Characteristics of
Efficient and Accurate Tool for Unsteady Load Results for Flight Prediction Two-Dimensional Hypersonic Configuration
Prediction
C00-071 Improved Closed-Form Approximation C00-069 Numerical Simulation of Transonic
C00-081 Structural Dynamics and Quasistatic
for Dutch Roll Flow over Wing-Mounted Twin-Engine Trans-
Aeroelastic Equations of Motion
C00-142 Optimal Trajectory for a Minimum port Aircraft
C00-165 Flutterometer: An On-Line Tool to Pre-
Fuel Turn
dict Robust Flutter Margins C00-004 Phugoid Approximation for Conven- Propeller and Rotor Systems
C00-037 Unified Aerodynamic-Influence-Coef-
ficient Approach for Aeroservoelastic and Multi- tional Airplanes C00-128 Experimental Demonstration of the
disciplinary Optimization Applications C00-060 Validation of a Rotorcraft Mathemati- Influence of Wing Couplings on Whirl—Flutter
C00-129 Variable Stiffness Spar Approach for cal Model for Autogyro Simulation Instability
Aircraft Maneuver Enhancement Using C00-058 Fixed-Pitch Propeller Selection for
General Aviation
ASTROS Light Airplanes
C00-091 Flow Control for an Airfoil with Lead-
Aerospace Plane Rotorcraft
ing-Edge Rotation: An Experimental Study
C00-064 Ground Effect Characteristics of a C00-105 Tailoring Lift/Drag Ratio for a Lifting- C00-092 Comparison of Induced Velocity Mod-
Two-Dimensional Hypersonic Configuration Body Airplane Configuration els for Helicopter Flight Mechanics
C00-002 Transportation Requirements for the C00-060 Validation of a Rotorcraft Mathemati- C00-087 Evaluation of a Motion Fidelity Crite-
Fast Freight Market cal Model for Autogyro Simulation rion with Visual Scene Changes
J. AIRCRAFT, VOL. 37, NO. 6: 2000 INDEX 1125
C00-120 Hover Performance Prediction Using System Effectiveness C00-098 Hypersonic Flow Predictions Using
Full-Potential Method and Comparison with Linear and Nonlinear Turbulence Closures
C00-002 Transportation Requirements for the
Experiments
Fast Freight Market Boundary-Layer Stability and Transition
C00-059 Important Scaling Parameters for Test-
ing Model-Scale Helicopter Rotors Testing, Flight and Ground C00-023 Numerical Analysis of Advanced
C00-033 Measurements of Bound and Wake Fighter Auxiliary Power Unit Exhaust Impinge-
C00-103 Experimental Geometry Optimization
Circulation on a Helicopter Rotor ment
Techniques for Multi-Element Airfoils
00-034 Model Helicopter Rotor Aerodynamics C00-151 Study of High-Lift Configurations
C00-026 Flight Testing an Optimal Trajectory
and Acoustics As Measured in Two Anechoic for the Saab J35 Draken Using k-c Transition/Turbulence Model
Wind Tunnels C00-028 Flight-Test Techniques Employed to Computational Fluid Dynamics
C00-080 Modification of a Helicopter Inverse Successfully Verify F/A-18E In-Flight Lift and
Simulation to Include an Enhanced Rotor Model Drag C00-156 New Fully Automated Procedure for
C00-089 Optimization of Balanced Field Length C00-083 Implications of Recent Rotary Rig the Prediction of Store Trajectory
Performance of Multi-Engine Helicopters Results for Flight Prediction C00-122 A Solution-Adaptive Unstructured
C00-118 Prediction Measurement of a Low-Fre- C00-123 Low Reynolds Number Aerodynamics Grid Method by Grid Subdivision and Local
quency Harmonic Noise of Hovering Model of Low-Aspect-Ratio, Thin/Flat/Cambered-Plate Remeshing
Helicopter Rotor Wings C00-039 Acoustics and Unsteady Flow of Tele-
C00-060 Validation of a Rotorcraft Mathemati- C00-161 Transition of Subsonic and Transonic scope Cavity in an Airplane
cal Model for Autogyro Simulation Expansion-Corner Flows C00-099 Aerodynamic Sensitivity Theory for
Rotary Stability Derivatives
C00-132 Use of Strip Yield Approach for Multi-
Safety ple-Site Damage Failure Scenarios An Improved Computational Method
for Determining Light Buffet of Flapped Wings
C00-065 Analysis of Evacuation Strategies for C00-001 Wind-Tunnel Techniques to Success-
C00-010 Chimera Donor Cell Search Algorithm
Design and Certification of Transport Airplanes fully Predict F/A-18E In-Flight Lift and Drag
Suitable for Solving the Full Potential Equation
00-046 Neural Network Forecasting of Service
Weather Hazards C00-143 Computational Analysis of F-15 Fore-
Problems for Aircraft Structural Component
body Flow at High Alpha
Groupings C00-014 Common Snowfall Conditions Associ-
C00-094 Development of a Shallow-Water Icing
C00-036 Study of Icing Effects on Performance ated with Aircraft Takeoff Accidents
Model in FENSAP-ICE
and Controllability of an Accident Aircraft C00-015 Predicting Glaze or Rime Ice Growth
C00-029 Effect of External Components on V-
C00-144 Influence of Icing Information on Pilot on Airfoils
22 Aircraft Forward-Flight Aerodynamics
Strategies for Operatingin Icing Conditions C00-036 Study of Icing Effects on Performance C00-125 Euler-Based Dynamic Aeroelastic
C00-160 Validation and Operation of a Vortex- and Controllability of an Accident Aircraft Analysis of Shell Structures
Wake/Shear Interaction Model C00-144 Influence of Icing Information on Pilot C00-040 Evaluation of Computational Algo-
Strategies for Operatingin Icing Conditions
rithms Suitable for Fluid-Structure Interactions
Simulation C00-012 Three-Dimensional Eulerian Approach
C00-107 Fast and Robust Viscous/Inviscid Inter-
to Droplet Impingement Simulation Using FEN-
C00-065 Analysis of Evacuation Strategies for action Code for Wing Flowfield Calculations
SAP-ICE, Part 1: Model, Algorithm, and Valida-
Design and Certification of Transport Airplanes C00-120 Hover Performance Prediction Using
tion
C00-087 Evaluation of a Motion Fidelity Crite- Full-Potential Method and Comparison with
rion with Visual Scene Changes Experiments
Fluid Dynamics
C00-088 Modeling Human Pilot Cue Utilization C00-098 Hypersonic Flow Predictions Using
with Applications to Simulator Fidelity Assess- Aeroacoustics Linear and Nonlinear Turbulence Closures
ment C00-043 Nonlinear Design Loads for Maneu-
C00-080 Modification of a Helicopter Inverse C00-166 Model for Radiated Sound from High vering Elastic Aircraft
Simulation to Include an Enhanced Rotor Model Reynolds Number Turbulence Source C00-140 Novel Beetle Algorithm for Cartesian
C00-124 Reduced-Order Dynamic Aeroelastic C00-039 Acoustics and Unsteady Flow of Tele- Grid Generation in Two Dimensions
Model Development and Integration with Non- scope Cavity in an Airplane C00-082 Numerical Analysis of a Finite Wing
linear Simulation C00-163 Aerodynamic and Aeroacoustic Opti- Altered by a Leading-Edge Ice Accretion
mization of Rotorcraft Airfoils via a Parallel C00-023 Numerical Analysis of Advanced
Stealth Genetic Algorithm Fighter Auxiliary Power Unit Exhaust Impinge-
C00-009 Direct Simulation of Acoustic Scatter- ment
C00-121 Effect of Sweep on Buffet over Novel ing by Two- and Three-Dimensional Bodies C00-052 Numerical Evaluation of Airfoil Fric-
Wing Planforms C00-006 Investigation of High-Lift Flowfield of tion Drag
STOL/VTOL/STOVL an Energy Efficient Transport Wing C00-069 Numerical Simulation of Transonic
00-034 Model Helicopter Rotor Aerodynamics Flow over Wing-Mounted Twin-Engine Trans-
00-029 Effect of External Components on V- and Acoustics As Measured in Two Anechoic port Aircraft
22 Aircraft Forward-Flight Aerodynamics Wind Tunnels C00-119 Numerical Study on Reduction of
C00-128 Experimental Demonstration of the C00-119 Numerical Study on Reduction of Transonic Blade-Vortex Interaction Noise
Influence of Wing Couplings on Whirl—Flutter Transonic Blade-Vortex Interaction Noise C00-031 Simulated Flowfields in Near-Ground
Instability C00-118 Prediction Measurement of a Low-Fre- Operation of Single- and Twin-Rotor Configura-
C00-149 Particle Image Velocimetry for Exhaust quency Harmonic Noise of Hovering Model tions
Gas Ingestion in Short Takeoff and Vertical Helicopter Rotor C00-151 Study of High-Lift Configurations
Landing Aircraft Boundary Layers and Heat Transfer— Using k-c Transition/Turbulence Model
C00-057 Wind Tunnel Tests of a High Lift Gen- C00-012 Three-Dimensional Eulerian Approach
Laminar
eration and Stall/Spin Recovery System to Droplet Impingement Simulation Using FEN-
C00-048 Moving-Wall Effect on Unsteady SAP-ICE, Part 1: Model, Algorithm, and Valida-
Structural Design (Including Loads) Boundary Layers tion
C00-128 Experimental Demonstration of the C00-027 Transonic and Low-Supersonic
Boundary Layers and Heat Transfer—
Influence of Wing Couplings on Whirl—Flutter Aerodyanmic Analysis of a Wing with Underpy-
Turbulent
Instability lon/Store
C00-132 Use of Strip Yield Approach for Multi- C00-053 Boundary-Layer Transition, Separa- C00-101 Unsteady Aerodynamics of a Wing-In-
ple-Site Damage Failure Scenarios tion, and Reattachment on an Oscillating Airfoil Ground-Effect Airfoil Flying over a Wavy Wall
1126 J. AIRCRAFT, VOL. 37, NO. 6: 2000 INDEX
C00-150 Wake Vortices in a Convective Bound- C00-013 Role of Stall Flutter in the Double-Stall C00-072 Closed-Loop Control of Forebody
ary Layer and their Influence on Following Air- Phenomenon of Wind-Turbine Blades Flow Asymmetry
craft C00-101 Unsteady Aerodynamics of a Wing-In- C00-143 Computational Analysis of F-15 Fore-
Ground-Effect Airfoil Flying over a Wavy Wall body Flow at High Alpha
Hydrodynamics
C00-042 Effects of Anhedral and Dihedral on a
Transonic Flow
C00-093 Equations of Motion of a Vehicle in a 75-deg Sweep Delta Wing
Moving Fluid C00-167 Improved Computational Method for C00-153 Exploratory Study of Aircraft Wake
C00-153 Exploratory Study of Aircraft Wake Determining Light Buffet of Flapped Wings Vortex Filaments in a Water Tunnel
Vortex Filaments in a Water Tunnel C00-010 Chimera Donor Cell Search Algorithm C00-138 Flow Complexities of Slender Wing
Suitable for Solving the Full Potential Equation Rock
Hypersonic Flow
C00-155 Flow Stabilization in a Transonic Wind C00-135 Helical-Groove and Circular-Trip
C00-098 Hypersonic Flow Predictions Using Tunnel with a Second Throat Effects on Side Force
Linear and Nonlinear Turbulence Closures C00-161 Transition of Subsonic and Transonic C00-024 Improvement of a Wing’s Aerodynam-
Expansion-Corner Flows ic Efficiency Using Coanda Tip Jets
Inlet, Nozzle, Diffuser, and Channel C00-027 Transonic and Low-Supersonic C00-006 Investigation of High-Lift Flowfield of
Flows Aerodyanmic Analysis of a Wing with Underpy- an Energy Efficient Transport Wing
00-095 Convergent-Flow-Derived Waveriders lon/Store C00-157 Lift Augmentation on a 60 Delta Wing
C00-011 Transonic-Aerodynamic-Influence-
with Leading-Edge Fences and a Gurney Flap
Jets, Wakes, and Viscid-Inviscid Flow Coefficient Approach for Aeroelastic and MDO
C00-033 Measurements of Bound and Wake
Interactions Applications
Circulation on a Helicopter Rotor
C00-166 Model for Radiated Sound from High Unsteady Flows C00-097 Modern Adaptation of Prandtl’s Clas-
Reynolds Number Turbulence Source sic Lifting-Line Theory
C00-107 Fast and Robust Viscous/Inviscid Inter- C00-053 Boundary-Layer Transition, Separa- C00-117 Near-Field Interaction of a Jet with
action Code for Wing Flowfield Calculations tion, and Reattachment on an Oscillating Airfoil Leading-Edge Vortices
C00-117 Near-Field Interaction of a Jet with C00-072 Closed-Loop Control of Forebody C00-007 New Model for Vortex Decay in the
Leading-Edge Vortices Flow Asymmetry Atmosphere
C00-007 New Model for Vortex Decay in the C00-121 Effect of Sweep on Buffet over Novel C00-050 Origin of Vortex Wandering over Delta
Atmosphere Wing Planforms
Wings
C00-146 Overview of Wake-Vortex Hazards C00-067 Eigenmode Analysis and Reduced-
C00-146 Overview of Wake-Vortex Hazards
During Cruise Order Modeling of Unsteady Transonic Potential
During Cruise
C00-150 Wake Vortices in a Convective Bound- Flow Around Airfoils
C00-110 Prediction of Vortex Breakdown Loca-
ary Layer and their Influence on Following Air- C00-125 Euler-Based Dynamic Aeroelastic
tion on a Banked Delta Wing
craft Analysis of Shell Structures
C00-138 Flow Complexities of Slender Wing C00-108 Proposed Mechanism for Time Lag of
Separated Flows Rock Vortex Breakdown Location in Unsteady Flows
C00-167 Improved Computational Method for C00-048 Moving-Wall Effect on Unsteady C00-168 Revisiting Unresolved Dynamic Stall
Determining Light Buffet of Flapped Wings Boundary Layers Phenomena
C00-053 Boundary-Layer Transition, Separa- C00-030 Nonlinear Rate and Amplitude Effects C00-056 Robust Low Cost Airport Wake Vortex
tion, and Reattachment on an Oscillating Airfoil on a Generic Combat Aircraft Model Sensor
C00-138 Flow Complexities of Slender Wing C00-023 Numerical Analysis of Advanced C00-102 Robust Vortex Control of a Delta Wing
Rock Fighter Auxiliary Power Unit Exhaust Impinge- by Distributed Microelectromechanical-Systems
C00-096 Navier-Stokes Computation of a ment Actuators
Rapidly Deploying Spoiler C00-050 Origin of Vortex Wandering over Delta C00-074 Universality of the Moving-Wall Effect
C00-030 Nonlinear Rate and Amplitude Effects Wings C00-160 Validation and Operation of a Vortex-
on a Generic Combat Aircraft Model C00-149 Particle Image Velocimetry for Exhaust Wake/Shear Interaction Model
C00-082 Numerical Analysis of a Finite Wing Gas Ingestion in Short Takeoff and Vertical C00-150 Wake Vortices in a Convective Bound-
Altered by a Leading-Edge Ice Accretion Landing Aircraft ary Layer and their Influence on Following Air-
C00-110 Prediction of Vortex Breakdown Loca- C00-108 Proposed Mechanism for Time Lag of craft
tion on a Banked Delta Wing Vortex Breakdown Location in Unsteady Flows
C00-168 Revisiting Unresolved Dynamic Stall C00-137 Results of Theodorsen and Garrick Guidance, Control, and Dynamics
Phenomena Revisited Technology
C00-013 Role of Stall Flutter in the Double-Stall C00-168 Revisiting Unresolved Dynamic Stall
Phenomenon of Wind-Turbine Blades Phenomena Aircraft Dynamics
C00-074 Universality of the Moving-Wall Effect C00-013 Role of Stall Flutter in the Double-Stall
C00-049 Aerodynamic Suppression of Wing
Phenomenon of Wind-Turbine Blades
Subsonic Flow C00-116 Small Disturbance Euler Equations: Rock Using Fuzzy Logic Control
C00-104 Aerodynamic Characteristics of Span- Efficient and Accurate Tool for Unsteady Load C00-066 Angular Momentum Control in Non-
wise Cambered Delta Wings Prediction linear Flight
C00-143 Computational Analysis of F-15 Fore- C00-011 Transonic-Aerodynamic-Influence- C00-093 Equations of Motion of a Vehicle in a
body Flow at High Alpha Coefficient Approach for Aeroelastic and MDO Moving Fluid
C00-042 Effects of Anhedral and Dihedral on a Applications C00-071 Improved Closed-Form Approximation
75-deg Sweep Delta Wing C00-037 Unified Aerodynamic-Influence-Coef- for Dutch Roll
C00-078 Implications of the Insensitivity of Vor- ficient Approach for Aeroservoelastic and Multi- C00-152 Optimization for Fighter Aircraft Verti-
tex Lift to Sweep disciplinary Optimization Applications cal-Plance Maneuvering Using Post-Stall Flight
C00-123 Low Reynolds Number Aerodynamics C00-074 Universality of the Moving-Wall Effect C00-004 Phugoid Approximation for Conven-
of Low-Aspect-Ratio, Thin/Flat/Cambered-Plate tional Airplanes
Vortices
Wings
Aircraft Guidance
C00-097 Modern Adaptation of Prandtl’s Clas- C00-104 Aerodynamic Characteristics of Span-
sic Lifting-Line Theory wise Cambered Delta Wings C00-038 Systems Analysis of Noise Abatement
C00-030 Nonlinear Rate and Amplitude Effects C00-041 Aerodynamics of Gurney Flaps on a Procedures Enabled by Advanced Flight Guid-
on a Generic Combat Aircraft Model Single-Element High-Lift Wing ance Technology
J. AIRCRAFT, VOL. 37, NO. 6: 2000 INDEX
Aircraft Stability and Control C00-089 Optimization of Balanced Field Length Structural Mechanics and
C00-099 Aerodynamic Sensitivity Theory for Performance of Multi-Engine Helicopters Materials
Rotary Stability Derivatives C00-038 Systems Analysis of Noise Abatement
C00-066 Angular Momentum Control in Non- Procedures Enabled by Advanced Flight Guid- Aeroelasticity and Control
linear Flight ance Technology
C00-084 Active Aeroelastic Wing Flight
C00-071 Improved Closed-Form Approximation
Research Program: Technical Program and
for Dutch Roll Interdisciplinary Topics
Model Analytical Development
C00-004 Phugoid Approximation for Conven-
tional Airplanes Aerospace Management C00-022 Aeroelastic Sensitivity Analyses for
C00-165 Flutterometer: An On-Line Tool to Pre- Flutter Speed and Gust Response
C00-106 Database Tomography Applied to an
dict Robust Flutter Margins C00-164 Aeroelastic Tailoring of Composite
Aircraft Science and Technology Investment
Aircraft Wings Exhibitng Non-Classical Effects
Artificial Intelligence Strategy
and Carrying External Stores
C00-046 Neural Network Forecasting of Service Aerospace Technology Utilization C00-113 Aeroservoelastic Analysis of the B-2
Problems for Aircraft Structural Component Bomber
Groupings C00-106 Database Tomography Applied to an
C00-079 Control of a Three Degree-of-Freedom
Aircraft Science and Technology Investment
Control System Design Airfoil with Limit-Cycle Behavior
Strategy
C00-025 Divergence of an Inflated Wing
C00-049 Aerodynamic Suppression of Wing C00-002 Transportation Requirements for the
C00-114 Nonlinear Aeroelastic Analysis
Rock Using Fuzzy Logic Control Fast Freight Market
C00-072 Closed-Loop Control of Forebody Complete Aircraft in Subsonic Flow
Flow Asymmetry Analytical and Numerical Methods C00-02¢ Nonlinear Aeroelastic Response
C00-079 Control of a Three Degree-of-Freedom Delta Wing to Periodic Gust
C00-141 Comparison of Deterministic and Sto-
Airfoil with Limit-Cycle Behavior C00-133 Optimization of Flexible Wing Without
chastic Optimization Algorithms for Generic
Ailerons for Rolling Maneuver
Control System Effectors Wing Design Problems
C00-127 Performance Enhancement of a Com-
C00-133 Optimization of Flexible Wing Without
C00-102 Robust Vortex Control of a Delta Wing posite Tilt-Rotor Using Aeroelastic Tailoring
by Distributed Microelectromechanical-Systems Ailerons for Rolling Maneuver C00-081 Structural Dynamics and Quasistatic
Actuators
Atmospheric and Space Sciences Aeroelastic Equations of Motion
Flight Mechanics C00-165 Flutterometer: An On-Line Tool to Pre-
C00-014 Common Snowfall Conditions Associ-
dict Robust Flutter Margins
C00-080 Modification of a Helicopter Inverse ated with Aircraft Takeoff Accidents
Simulation to Include an Enhanced Rotor Model C00-162 Experimental Test of the Influence of C00-011 Transonic-Aerodynamic-Influence-
Propulsion Effeciency Contrail Formation Coefficient Approach for Aeroelastic and MDO
Handling Qualities C00-015 Predicting Glaze or Rime Ice Growth Applications
C00-087 Evaluation of a Motion Fidelity Crite- on Airfoils Dynamic Model Analysis
rion with Visual Scene Changes
C00-088 Modeling Human Pilot Cue Utilization Reliability, Maintainability, and Logistics C00-139 Elastomeric Damper Model and Limit
with Applications to Simulator Fidelity Assess- Support Cycle Oscillation in a Bearingless Helicopter
ment
Rotor Blade
C00-090 Testing of a Semiactive Landing Gear C00-016 Need for New Materials in Aging Air-
C00-019 Improvement of a Numerical Proce-
Control for a General Aviation Aircraft craft Structures
dure for the Dynamic Analysis of Aircraft Struc-
Optimization Techniques Research Facilities and Instrumentation tures
C00-141 Comparison of Deterministic and Sto- C00-103 Experimental Geometry Optimization Flexible and Active Structures
chastic Optimization Algorithms for Generic Techniques for Multi-Element Airfoils
Wing Design Problems C00-040 Evaluation of Computational Algo-
C00-051 Conceptual Aircraft Design Based on a Safety rithms Suitable for Fluid-Structure Interactions
CM0u0l-t1i4co2n stOrpatinitm alG eneTtriacj ecOtpotriym izfeorr a Minimum 00-014 Common Snowfall Conditions Associ- Materials Structural Properties
ated with Aircraft Takeoff Accidents
Fuel Turn C00-094 Development of a Shallow-Water Icing C00-016 Need for New Materials in Aging Air-
C00-152 Optimization for Fighter Aircraft Verti-
Model in FENSAP-ICE craft Structures
cal-Plance Maneuvering Using Post-Stall Flight
C00-046 Neural Network Forecasting of Service
Structural Composite Materials
Signal Processing Problems for Aircraft Structural Component
C00-063 Far-field Pressure Estimation of a Plate Groupings C00-134 Analytical Prediction of Damage
from the Interpolated Acceleration Distribution Growth in Notched Composite Panels Loaded in
Sensor Systems
C00-056 Robust Low Cost Airport Wake Vortex Compression
Sensor C00-056 Robust Low Cost Airport Wake Vortex C00-111 Application of Finite Strip Method to
Sensor Composite Panel Flutter Analysis
System Identification
C00-018 Evaluation of Thin Kevlar—Epoxy Fab-
C00-112 Bounded-Variable Gauss-Newton Propulsion ric Panels Subjected to Shear Loading
Algorithm for Aircraft Parameter Estimation
Engine Performance Structural Design
Trajectory Optimization
C00-162 Experimental Test of the Influence of C00-022 Aeroelastic Sensitivity Analyses for
C00-026 Flight Testing an Optimal Trajectory
Propulsion Effeciency Contrail Formation Flutter Speed and Gust Response
for the Saab J35 Draken
C00-147 Conceptual Design Studies of a Strut-
C00-142 Optimal Trajectory for a Minimum Environmental Effects
Fuel Turn Braced Wing Transonic Transport
C00-152 Optimization for Fighter Aircraft Verti- C00-162 Experimental Test of the Influence of C00-043 Nonlinear Design Loads for Maneu-
cal-Plance Maneuvering Using Post-Stall Flight Propulsion Effeciency Contrail Formation vering Elastic Aircraft
1128 J. AIRCRAFT, VOL. 37, NO. 6: 2000 INDEX
Structural Durability (Including Fatigue, C00-019 Improvement of a Numerical Proce- Structural Modeling
Fracture, and Environmental dure for the Dynamic Analysis of Aircraft Struc- C00-164 Aeroelastic Tailoring of Composite
tures
Degradation) Aircraft Wings Exhibitng Non-Classical Effects
C00-136 Limit Cycle Oscillation Characteristics
C00-134 Analytical Prediction of Damage of Fighter Aircraft and Carrying External Stores
Growth in Notched Composite Panels Loaded in C00-115 Limit Cycle Oscillation Flight Test C00-025 Divergence of an Inflated Wing
Compression Results of a Fighter with External Stores
Structural Optimization
C00-017 Linking Riveting Process Parameters C00-081 Structural Dynamics and Quasistatic
to the Fatigue Performance of Riveted Aircraft Aeroelastic Equations of Motion C00-127 Performance Enhancement of a Com-
Structures posite Tilt-Rotor Using Aeroelastic Tailoring
Structural Finite Elements
€00-016 Need for New Materials in Aging Air- C00-037 Unified Aerodynamic-Influence-Coef-
craft Structures C00-134 Analytical Prediction of Damage ficient Approach for Aeroservoelastic and Multi-
C00-045 Strength of 2024-T3 Aluminum Panels Growth in Notched Composite Panels Loaded in disciplinary Optimization Applications
with Multiple Site Damage Compression
C00-111 Application of Finite Strip Method to Structural Stability
Structural Dynamics and Composite Panel Flutter Analysis
C00-131 Response of Selected Integrally Stiff-
Characterization C00-019 Improvement of a Numerical Proce- ened Curved Aluminum Panels Subjected to
dure for the Dynamic Analysis of Aircraft Struc-
C00-113 Aeroservoelastic Analysis of the B-2 Combined Loads
tures
Bomber C00-017 Linking Riveting Process Parameters
C00-111 Application of Finite Strip Method to to the Fatigue Performance of Riveted Aircraft Thermophysics and Heat Transfer
Composite Panel Flutter Analysis Structures
Computational Heat Transfer
C00-139 Elastomeric Damper Model and Limit C00-131 Response of Selected Integrally Stiff-
Cycle Oscillation in a Bearingless Helicopter ened Curved Aluminum Panels Subjected to C00-094 Development of a Shallow-Water
Rotor Blade Combined Loads Icing Model in FENSAP-ICE
J. AIRCRAFT, VOL. 37, NO. 6: 2000 INDEX
Author Index
Agarwal, Ramesh K., C00-107 Chin, Yan-Shin, CO0-119 Goggin, P. J., CO0-124 Kuperman, Murray, CO0-014
Aggarwal, H. R., CO00-118 Ching, Tan Kok, CO0-109 Goh, E. K.R., CO0-135 Kuttenkeuler, Jakob, CO0-126
Ahmed, N. A., C00-024 Cho, Kum Won, C00-156 Goldberg, U., C00-098 Kwon, Jang Hyuk, CO0-156
Ahmed, Saad A., C00-091 Choi, Seong-Wook, C00-096 Goonko, Yu. P., C00-095 Laik, Olivier A., CO0-009
Al-Garni, Abdullah M., C00-091 Choo, Y., C00-036 Gordnier, Raymond E., C00-130 Laine, Seppo, CO0-107
Al-Garni, Ahmed Z., C00-091 + Choo, Yung K., C00-145 Green, Kenneth A., CO00-106 Laitone, E. V., CO0-058
Ambur, Damodar R., C00-134 * Choudhari, Meelan, C00-006 Greer, Donald, C00—-100 Landman, Drew, CO0—103
Andrews, Dana G., C00-002 Chow, Chuen- Yen, CO00-167 Griffin, Kenneth E., C00-084, C00-129 Laschka, Boris, COO-116
Appa, K., C00-133 Chung, J., C00-036 Grossman, B., C00-147 Layukallo, Thombi, C00—155
Archer, R. D., C00-024 Chung, James J., CO0-145 Gundlach, IV, John F., CO0-147 Lee, Calvin K., CO0-070
Arman, M., C00-159 Chung, Kung Ming, C00-068, Gursul, Ismet, C00-050, CO0-108 Lee, Dong-Chan, C00-066
Arthurs, Thomas D., C00-113 C00-161 Habashi, Wagdi G., C00-094, CO0-012 Lee, Gwo-Bin, CO0-102
Babinsky, Holger, CO0-154 Chung, William W.Y., C00-087 Haftka, R. T., C00-147 Lee, In, C00—027
Baker, Donald J., C00-018 Clark, Robert L., C00-079 Hall, Kenneth C., C00-067 Lee, Seungsoo, C00-156
Bartels, Robert E., CO0-076 Clarke, John-Paul Barrington , Hamory, Phil, C00-100 Lee, T., C00-053
Batten, P., CO0-098 C00-038 Hansman, R. John, CO00—-937 Leishman, J. Gordon, C00—033
Beaugendre, H., CO0-094 Cliff, E.M ., C00-099 Hassan, H. A., C00-151 Lewis, Andrew P., C00-125
Behrouzi, P., CO0-149 Cole, Jeff, CO0-014 Hayder, M. E., CO0-166 Lewy, S., C00-034
Berkman, Mert E., CO00-006 Conway, Bruce A., CO00-152 Hayes, J., COO-159 Li, Fengwei, C00-069
Bernhardt, John E., CO0-072 Coppotelli, G., C06-022 Hedo, José M., C00—065 Li, Jie, COO-069
Bertelrud, A., C00-151 Corjon, Alexandre, C00-148 Henry, James K., CO0-020 Librescu, Liviu, CO0-164
Berton, E., CO0-120 Crema, L. Balis, CO0-022 Hess, Ronald A., C00—087, C00-088 Lim, S. H., CO0-160
Bessette, Denis, CO0-084 Crimi, Peter, CO00-025 Ho, Jyh-Yeuan, CO00-167 Lim, T. T., CO0-135
Beyers, Martin E., C00—030, C00-074, Crossley, William A., CO0-086, Hodges, Dewey H., C00—040, Limache, A. C., C00—099
C00-083 C00-163 C00-127, C00-114 Lin, San- Yih, CO0-119
Bhagwat, Mahendra J., C00-033 Cunefare, K. A., C00-021 Holst, Terry L., CO0-010 Lind, Rick, CO0-165
Biesel, V., C00-021 Czerwiec, Ryan, C00-151 Holzapfel, Frank, C00-150 Liu, Chang, CO0—102
Blacodon, Daniel, C00-063 Damodaran, M., C00-141 Horie, Kazuhiro, C00-152 Liu, D. D., C00-011, C00-037,
Blasi, Luciano, C00-051 Darracq, Denis, C00-148 Houston, S. S. , C00-060, C00-092 C00-129
Bletzinger, P., CO0-159 Davila, Carlos G., C00-134 Huang, Adam, C00-102 Lombardi, Giovanni, C00—052
Bloor, Malcolm 1.G., CO0—085 Del Core, Giuseppe, C00-051 Humenik, James A., CO0-106 Loth, John L., C00-064
Bolender, Michael A., C00-003, Denegri, Jr., Charles M., CO0-136, Hurst, David W., C00-041 Lua, K. B., C00-135
C00-061 C00-115 Hwang, Bae-Yih, CO00-119 Luo, S. C., CO0-135
Bond, Robert E., C00-064 Dogan, Atilla, COO-062 Hwang, S. T., CO0-111 Luxhoj, James T., C00-046
Bourgault, Yves, CO0-012, C00-094 Dérnbrack, Andreas, CO00-150 Im, Ye-Hoon, C00-101 Lyrintzis, Anastasios S., C00-163
Boutanios, Ziad, CO0-012 Dowell, Ear! H., CO0-020, C00-067, Inger, George R., CO0-154 Mallik, A. K., C00-139
Boxwell, D. A., C00-034, C00-118 C00-079 luspa, Luigi, CO0-051 Marciniak, Maciej, CO0—077
Brenner, Marty, C00-165 Doyle, Sharon A. , C00-080 Jacobson, Steven B., COO-113 Maresca, C., CO0-120
Brenot, Dominique, C00—-063 Drela, Mark, CO0-100 James, K. D., cto-146 Markelov, G. N., CO00—095
Briggs, David G., CO0-082 Ducros, Frederic, CO0-148 Jategaonkar, R. V., CO0-112 Martinez- Val, Rodrigo, C00-065
Britcher, Colin P., C00-103 Dumitrescu, H., CO0-048 Jeffrey, David, COO-041 Mason, W. H., C00—-147
Britt, Robert T., CO0-113 Dunn, Michael J., C00-002 Jegley, Dawn C., CO00-131 Masquelier, M. L., CO0-055
Brown, R. E., C00-092 Dykman, John R., C00—-081, C00-124 Jha, R., CO0-129 Mastroddi, F., C00-022
Bucci, R. J., CO0-016 E, Qin, C00-069 Jones, Brian R., C00-163 Mazhul, I. I., CO0-095
Buchholz, Mark D., CO00-157 Eastep, F. E., C00-133 Julienne, Alain, C00-063 McGowan, David M., C00-134
Buckley, John E., C00-070 Edwards, J. R., COO0-151 Kabamba, Pierre T., C00-062 McGuirk, J. J., CO0-149
Buckton, Daniel, CO0-148 Engelstad, S. P., C00-021 Kafyeke, F., C00-053 Melville, Reid B., C00-130
Bunton, Robert W., C00-136 Ericsson, Lars E., C00—-013, C00-030, Kang, Ning, C00-031 Miller, Gerald D., COO0-084
Burnham, David C., C00-056 C00-074, C00-083, C00-138, Kapania, R. K., C00-147 Miller, L. Scott, COO-153
Busen, Reinhold, CO0-162 C00-168 Karpel, M., C00-037, C00-043 Mokhtarian, F., C00—053
Byrd, Larry W., CO0-044 Falabella, Gregory J., CO0-082 Katz, Joseph, CO0-105 Moore, R. K., C00-014
Cali, Philip M., C00-023 Farris, T. N., CO0-017 Keane, Mike, CO00-148 Morency, Francois, CO0-035
Camden, Michael P., C00-044 Favier, D., CO0-120 Kentfield, J. A. C., CO0-008 Morris, Gary J., CO0-064
Caplot, M., C00-034 Field, Peter F., CO0-084 Khorrami, Mehdi R., C00-006 Morris, Philip J., CO0-009
Cardos, V., C00-048 Florea, Razvan, CO00-067 Khot, N. S., CO00-133 Mouak, Adil, C00—045
Cesnik, Carlos E. S., C00-040, Foster, Scott R., CO0-153 Kim, David, CO0-077 Mueller, Thomas J., CO0—123
C00-114 Frampton, Kenneth D., C00—-079 Kim, Dong-Hyun, C00-027 Myose, Roy Y., C00-045
Chakravarthy, S., C00-098 Franke, M. E., C00—055 Kim, Ran Y., CO0-044 Nagati, M. G., C00-066
Chang, Keun-Shik, C00-101, C00-096 Frech, Michael, CO0-150 Ko, Andy, C00-147 Nagshineh-Pour, Amir H., CO0-147
Charbonnier, Jean-Marc, CO0-117 Ganguly, B., CO0-159 Kostoff, Ronald N., C00-106 Nair, N. K., CO0-049
Chen, C. K., CO00-132 Gern, Frank H., C00-147, C00-164 Krake, Keith, C00-100 Nakamura, Yoshiaki, CO0-155
Chen, P. C., C00-011, C00-037, Gerz, Thomas, C00-150 Kreiselmaier, Erich, CO0-116 Nelson, Robert C., CO0-110
C00-129 Ghiringhelli, Gian Luca, CO0-090 Kuang, J. H., C00—132 Niewald, P. W., C00-001, C00-028
1130 J. AIRCRAFT, VOL. 37, NO. 6: 2000 INDEX
Nordmann, Lars H. , C00-046 Rechorst, Andrew L., C00-036, Simpson, R. G., C00-024 Traub, Lance W., C00-042, C00-078,
Nowak, D. K., C00-057 C00-145 Singleton, Jeffrey D., C00-059 C00-104, C00-078
Palaniswamy, S., C00-098 Ringertz, Ulf, CO0-026, C00-142 Slater, G. L., C00-003, C00-061 Tsao, Thomas, C00-102
Paraschivoiu, lon, C00-035 Rinoie, Kenichi, CO0-005 Slater, John W., C00-145 Tso, Jin, COO-157
Park, Minwoo, C00-156 Rodden, William P., C00-081 Smith, Bert L., C00-045 Tuncer, Ismail H., C00-075
Parker, S. L., C00-001, C00-028 Roglin, Bernhard, CO0-105 Smith, Marilyn J., C00-040, C00-125 Umstattd, R., CO0-159
Patil, Mayuresh J., CO0-114 Rokhsaz, Kamran, C00-153 Snyder, C. H., C00-055 Venkatesan, C., C00-139
Ross, Tamaira E., C00-086 Vigeant-Langlois, Laurence, CO0-144
Paul, Donald B., C00-044 Snyder, D. O., C00-097
Visser, H. G., CO0-089
Pelletier, Alain, CO0-123, C00-110 Rossow, V. J., CO0-146 Solies, U. P., C00--057
Pendleton, Edmund W., C00-084 Rubeck, Mark, C00-002 Soykasap, Omer, C00-127 WWaanngg,, FX.r,a nCk 00Y-.,1 4C1O 0-117
Peroomian, O., C00-098 Rubin, William L., C00-056 Spaid, Frank W., C00-073
Rubinstein, Robert, CO0-166 Warren, C. J., C00-016
Pesonen, Urpo J., C00-107 Rudis, Robert P., CO00-056 Spitzer, Edward A., C00-056 Williams, David R., C00-072
Petrakis, G., C00-053 Splettstoesser, W. R., C00-034
Wilson, Michael J., CO0-085
Rumsey, C. L., C00-151
Peyran, Richard J., CO0-128 Sreenatha, A. G., C00-049 Winther, B. A., C00-124
Sadowski, Shelly S., C00-006
Phillips, W. F., CO0-004, C00-071, Srinivasan, G. R., CO0-039 Witzeman, Frank C., CO00-054
Sahin, Ahmet Z., C00-091
C00-097 Srivastava, Ashok, C00-140 Wolfe, Howard F., C00-044
Salvetti, Maria Vittoria, CO0-052
Pinelli, Dario, C00-052 Starke, Jr., E. A., CO0-016 Wood, Norman J., C00-121
Sarhaddi, D., C00-011, C00-037,
Pirzadeh, Shahyar Z., COO-122 Strang, William Z., C00-054 Woods, Michael I., COO0-121
C00-129
Platzer, Max F., C00-075 Sudhakar, K., C00-049 Wurtzler, Kenneth E., CO0-143
Sarpkaya, Turgut, C00-007
Plohr, Martin, CO0-162 Sun, Mao, C00-031 Xie, Wensheng, C00-050
Saville, Perry A., C00-045
Pohit, G., C00-139 Schetz, Joseph A., COO-147 Szolwinski, M. P., C00-017 Yang, Guowei, C00-032
Yaniv, S., C00-043
Politovich, Marcia K., CO0-O015 Schmitz, F. H., C00-034, CO0-118 Tai, Tsze C., COO-029
Yeager, Jr., William T., C00-059
Potapezuk, Mark G., C00-036, Tai, Yu-Chong, C00-102
Schroeder, Jeffery A., CO0-087 Yeung, W. W. H., C00-047
C00-145 Schultz, K. J., C00-034 Tang, Deman, C00-020 Yurkovich, R., C00-129
Powell, E. A., C00-021 Schumann, Ulrich, CO0-162 Tétrault, Philippe-André, CO0-147 Zeiler, Thomas A., CO00-137
Proot, Michael M.J., COO-117 Sevant, Natasha E., CO00-085 Tezok, Fatih, C00-035 Zerihan, Jonathan, C00-158
Rand, Omri, C00-128 Sforza, Pasquale M., C00-117 Thomasson, Peter G., C00-093 Zeyada, Y., C00-088
Rasmussen, Roy, C00-014 Shang, J. S., CO0-159 Thomson, Douglas, C00-080 Zhang, Xin, C00-041, C00-158
Raveh, D. E., C00-043 Shiau, L. C., C00-111 Tizzi, Silvano, C00-019 Zheng, Z. C., CO0-160
Ravichandran, K. S., CO0-140 Shih, Chiang, C00-102 Tomaro, Robert F., C00-054 Zhou, Ye, C00-166
Redfern, Mike, C00-148 Simmons, Larry W., C00-044 Toothman, Darrell Ray, C00-106 Zhuang, Lixian, C00-032
J. AIRCRAFT, VOL. 37, NO. 6: 2000 INDEX
Chronological Index
C00-001 Wind-Tunnel Techniques to Successfully Predict F/A- C00-017 Linking Riveting Process Parameters to the Fatigue
18E In-Flight Lift and Drag. P. W. Niewald and S. L. Parker, The Performance of Riveted Aircraft Structures. M. P. Szolwinski,
Boeing Company (37, 1, p. 9) Article Rensselaer Polytechnic Institute; and T. N. Farris, Purdue
University (37, 1, p. 130) Article based on AIAA Paper 99-1339
C00-002 Transportation Requirements for the Fast Freight
Market. Michael J. Dunn, Mark Rubeck, and Dana G. Andrews, C00-018 Evaluation of Thin Kevlar-Epoxy Fabric Panels
The Boeing Company (37, 1, p. 15) Article Subjected to Shear Loading. Donald J. Baker, NASA Langley
Research Center (37, 1, p. 138) Article based on AIAA Paper 96-
C00-003 Cost Analysis of the Departure-En Route Merge 1367
Problem. Michael A. Bolender and G. L. Slater, University of
Cincinnati (37, 1, p. 23) Article based on AIAA Paper 99-4297 C00-019 Improvement of a Numerical Procedure for the
Dynamic Analysis of Aircraft Structures. Silvano Tizzi,
C00-004 Phugoid Approximation for Conventional Airplanes. University of Rome, “La Sapienza”, Italy (37, 1, p. 144) Article
W. F. Phillips, Utah State University (37, 1, p. 30) Article
C00-020 Nonlinear Aeroelastic Response of Delta Wing to
C00-005 Experiments on a 60-Degree Delta Wing with Periodic Gust. Deman Tang, James K. Henry, and Earl H. Dowell,
Rounded Leading-Edge Vortex Flaps. Kenichi Rinoie, Cranfield Duke University (37, 1, p. 155) Article
University, Japan (37, 1, p. 37) Article
C00-021 Stiffener Shape Design to Minimize Interior Noise. S.
C00-006 Investigation of High-Lift Flowfield of an Energy P. Engelstad, Lockheed Martin Aeronautical Systems, K. A.
Efficient Transport Wing. Mert E. Berkman, Mehdi R. Khorrami, Cunefare, Georgia Institute of Technology; E. A. Powell, Lockheed
Meelan Choudhari, and Shelly S. Sadowski, High Technology Martin Aeronautical Systems; and V. Biesel, Georgia Institute of
Corporation (37, 1, p. 45) Article based on AIAA Paper 99-0926 Technology (37, 1, p. 165) Article based on AIAA Paper 97-1620
C00-007 New Model for Vortex Decay in the Atmosphere. C00-022 Aeroelastic Sensitivity Analyses for Flutter Speed and
Turgut Sarpkaya, Naval Postgraduate School (37, 1, p. 53) Article Gust Response. L. Balis Crema and F. Mastroddi, University of
Rome “La Sapienza”, Italy; and G. Coppotelli, Centro Italiano
C00-008 Influence of Aspect Ratio on the Performance of Ricerche Aerospaziale, Italy (37, 1, p. 172) Article
Outboard-Horizontal-Stabilizer Aircraft. J. A. C. Kentfield,
University of Calgary, Canada (37, 1, p. 62) Article C00-023 Numerical Analysis of Advanced Fighter Auxiliary
Power Unit Exhaust Impingement. Philip M. Cali, U.S. Air Force
C00-009 Direct Simulation of Acoustic Scattering by Two- and Research Laboratory (37, 1, p. 181) Engineering Note based on
Three-Dimensional Bodies. Olivier A. Laik and Philip J. Morris, AIAA Paper 98-0770
Pennsylvania State University (37, 1, p. 68) Article based on AIAA
Paper 98-2379 C00-024 Improvement of a Wing’s Aerodynamic Efficiency
Using Coanda Tip Jets. R. G. Simpson, N. A. Ahmed, and R. D.
C00-010 Chimera Donor Cell Search Algorithm Suitable for Archer, University of New South Wales, Australia (37, 1, p. 183)
Solving the Full Potential Equation. Terry L. Holst, NASA Ames Engineering Note
Research Center (37, 1, p. 76) Article based on AIAA Paper 97-
2259 C00-025 Divergence of an Inflated Wing. Peter Crimi, Andover
Applied Sciences, Inc. (37, 1, p. 184) Engineering Note
C00-011 Transonic-Aerodynamic-Influence-Coefficient
Approach for Aeroelastic and MDO Applications. P. C. Chen C00-026 Flight Testing an Optimal Trajectory for the Saab J35
and D. Sarhaddi, ZONA Technology, Inc.; and D. D. Liu, Arizona Draken. Ulf Ringertz, Kungliga Tekniska Hégskolan, Sweden (37,
State University (37, 1, p. 85) Article based on AIAA Paper 97-1181 1, p. 187) Engineering Note
C00-012 Three-Dimensional Eulerian Approach to Droplet C00-027 Transonic and Low-Supersonic Aerodyanmic
Impingement Simulation Using FENSAP-ICE, Part 1: Model, Analysis of a Wing with Underpylon/Store. Dong-Hyun Kim and
Algorithm, and Validation. Yves Bourgault, Ziad Boutanios, and In Lee, Korea Advanced Institute of Science and Technology, Korea
Wagdi G. Habashi, Concordia University, Canada (37, 1, p. 95) (37, 1, p. 189) Engineering Note
Article
C00-028 Flight-Test Techniques Employed to Successfully
C00-013 Role of Stall Flutter in the Double-Stall Phenomenon Verify F/A-18E In-Flight Lift and Drag. P. W. Niewald and S. L.
of Wind-Turbine Blades. Lars E. Ericsson (37, 1, p. 104) Article Parker, The Boeing Company (37, 2, p. 194) Article
C00-014 Common Snowfall Conditions Associated with C00-029 Effect of External Components on V-22 Aircraft
Aircraft Takeoff Accidents. Roy Rasmussen and Jeff Cole, Forward-Flight Aerodynamics. Tsze C. Tai, U.S. Naval Surface
National Center for Atmospheric Research, and R. K. Moore and Warfare Center (37, 2, p. 201) Article
Murray Kuperman, United Airlines (37, 1, p. 110) Article
C00-030 Nonlinear Rate and Amplitude Effects on a Generic
C00-015 Predicting Glaze or Rime Ice Growth on Airfoils. Combat Aircraft Model. Lars E. Ericsson, and Martin E. Beyers,
Marcia K. Politovich, National Center for Atmospheric Research Institutfeo r Aerospace Research, Canada (37, 2, p. 207) Article
(37, 1, p. 117) Article
C00-031 Simulated Flowfields in Near-Ground Operation of
C00-016 Need for New Materials in Aging Aircraft Structures. Single- and Twin-Rotor Configurations. Ning Kang and Mao
R. J. Bucci and C. J. Warren, Alcoa, Inc.; and E. A. Starke Jr., Sun, Beijing University of Aeronautics and Astronautics, PRC (37,
University of Virginia (37, 1, p. 122) Article 2, p. 214) Article
1132 J. AIRCRAFT, VOL. 37, NO. 6: 2000
C00-032 Numerical Simulation of Rotor Flow in Hover. C00-045 Strength of 2024-T3 Aluminum Panels with Multiple
Guowei Yang and Lixian Zhuang, University of Science and Site Damage. Bert L. Smith, Perry A. Saville, Adil Mouak, and
Technology of China, PRC (37, 2, p. 221) Article Roy Y. Myose, Wichita State University (37, 2, p. 325) Article
C00-033 Measurements of Bound and Wake Circulation on a C00-046 Neural Network Forecasting of Service Problems for
Helicopter Rotor. Mahendra J. Bhagwat and J. Gordon Leishman, Aircraft Structural Component Groupings. Lars H. Nordmann
University of Maryland (37, 2, p. 227) Article and James T. Luxhoj, Rutgers University (37, 2, p. 332) Article
C00-034 Model Helicopter Rotor Aerodynamics and Acoustics C00-047 Lift Augmentation for Massive Separation. W. W. H.
As Measured in Two Anechoic Wind Tunnels. F. H. Schmitz, Yeung, Nanyang Technological University, Singapore (37, 2, p.
Univeristy of Maryland; D. A. Boxwell, U.S. Army Aviation and 339) Engineering Note
Missile Command; W. R. Splettstoesser and K. J. Schultz, DLR,
German Aerospace Research Center, Germany; S. Lewy, ONERA, C00-048 Moving-Wall Effect on Unsteady Boundary Layers.
France; and M. Caplot, Thompson—CSF, France (37, 2, p. 235) H. Dumitrescu and V. Cardos, Caius lacob Institute of Applied
Article Mathematics, Romania (37, 2, p. 341) Engineering Note
C00-035 Heat and Mass Transfer in the Case of Anti-Icing C00-049 Aerodynamic Suppression of Wing Rock Using Fuzzy
System Simulation. Francois Morency, Ecole Polytechnique de Logic Control. A. G. Sreenatha, Australian Defence Force
Montréal, Canada; Fatih Tezok, Bombardier Aerospace, Canada; Academy, Australia; and N. K. Nair and K. Sudhakar, /ndian
and Ion Paraschivoiu, Ecole Polytechnique de Montréal, Canada Institute of Technology, India (37, 2, p. 345) Engineering Note
(37, 2, p. 245) Article based on AIAA Paper 99-0623
C00-050 Origin of Vortex Wandering over Delta Wings. Ismet
Gursul, University of Bath, England, UK; and Wensheng Xie,
C00-036 Study of Icing Effects on Performance and
University of Cincinnati (37, 2, p. 348) Engineering Note
Controllability of an Accident Aircraft. A. Reehorst, J. Chung,
M. Potapezuk, and Y. Choo, NASA John H. Glenn Research Center
C00-051 Conceptual Aircraft Design Based on a
(37, 2, p. 253) Article based on AIAA Paper 99-0374
Multiconstraint Genetic Optimizer. Luciano Blasi, Luigi Iuspa,
and Giuseppe Del Core, Second University of Naples, Italy (37, 2,
C00-037 Unified Aerodynamic-Influence-Coefficient Approach
p. 351) Engineering Note
for Aeroservoelastic and Miultidisciplinary Optimization
Applications. P. C. Chen and D. Sarhaddi, ZONA Technology, Inc.;
C00-052 Numerical Evaluation of Airfoil Friction Drag.
D. D. Liu, Arizona State University; and M. Karpel, Technion—
Giovanni Lombardi, Maria Vittoria Salvetti, and Dario Pinelli,
Israel Institute of Technology, Israel (37, 2, p. 260) Article based on
University of Pisa, Italy (37, 2, p. 354) Engineering Note
AIAA Paper 97-1181
C00-053 Boundary-Layer Transition, Separation, and
C00-038 Systems Analysis of Noise Abatement Procedures
Reattachment on an Oscillating Airfoil. T. Lee and G. Petrakis,
Enabled by Advanced Flight Guidance Technology. John-Paul
McGill University, Canada; and F. Mokhtarian and F. Kafyeke,
Barrington Clarke, Massachusetts Institute of Technology (37, 2, p.
Bombardier Aerospace, Canada (37, 2, p. 356) Article
266) Article based on AIAA Paper 97-0490
C00-054 Simulation of Store Separation for the F/A-18C Using
C00-039 Acoustics and Unsteady Flow of Telescope Cavity in
Cobalt,¢9. Robert F. Tomaro, Frank C. Witzeman, and William Z.
an Airplane. G. R. Srinivasan, NASA Ames Research Center (37, 2,
Strang, Air Force Research Laboratory (37, 3, p. 361) Article
p. 274) Article based on AIAA Paper 98-0413
C00-055 Wind-Tunnel Tests of an Aircraft Turret Model. C. H.
C00-040 Evaluation of Computational Algorithms Suitable for
Snyder and M. E. Franke, Air Force Institute of Technology; and M.
Fluid-Structure Interactions. Marilyn J. Smith and Dewey H.
L. Masquelier, U.S. Air Force Research Laboratory (37, 3, p. 368)
Hodges, Georgia Institute of Technology; and Carlos E. S. Cesnik,
Article based on AIAA Paper 99-0939
Massachusetts Institute of Technology (37, 2, p. 282) Article
C00-056 Robust Low Cost Airport Wake Vortex Sensor.
C00-041 Aerodynamics of Gurney Flaps on a Single-Element William L. Rubin, WLR Research, Inc.; David C. Burnham,
High-Lift Wing. David Jeffrey and Xin Zhang, University of Scientific and Engineering Solutions, Inc.; and Edward A. Spitzer
Southampton, England, UK; and David W. Hurst, Glasgow and Robert P. Rudis, Volpe National Transportation Systems Center
University, Scotland, UK (37, 2, p. 295) Article (37, 3, p. 377) Article based on AIAA Paper 2000-0627
C00-042 Effects of Anhedral and Dihedral on a 75-deg Sweep C00-057 Wind-Tunnel Tests of a High Lift Generation and
Delta Wing. Lance W. Traub, Texas A&M University (37, 2, p. Stall/Spin Recovery System. D. K. Nowak, Micron Corporation;
302) Article and U. P. Solies, University of Tennessee Space Institute (37, 3, p.
383) Article
C00-043 Nonlinear Design Loads for Maneuvering Elastic
Aircraft. D. E. Raveh and M. Karpel, Technion—lIsrael Institute of C00-058 Fixed-Pitch Propeller Selection for Light Airplanes. E.
Technology, Israel; and S. Yaniv, Israel Military Industries, Ltd., V. Laitone, University of California (37, 3, p. 390) Article
Israel (37, 2, p. 313) Article
C00-059 Important Scaling Parameters for Testing Model-
C00-044 Failure Criteria Development for Dynamic High- Scale Helicopter Rotors. Jeffrey D. Singleton, William T. Yeager,
Cycle Fatigue of Ceramic Matrix Composites. Howard F. Wolfe, Jr., NASA Langley Research Center (37, 3, p. 396) Article
Michael P. Camden, Larry W. Byrd, Donald B. Paul, Larry W.
Simmons, U.S. Air Force Research Laboratory; and Ran Y. Kim, C00-060 Validation of a Rotorcraft Mathematical Model for
University of Dayton (37, 2, p. 319) Article based on AIAA Paper Autogyro Simulation. S. S. Houston, University of Glasgow,
98-0263 Scotland (37, 3, p. 403) Article
