Table Of Content

JOURNAL OF AIRCRAFT Vol. 43, No. 6, November—December 2006 2006 Journal of Aircraft Index How to Use the Index In the Subject Index, pages 1960-1969, 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 1970-1972, lists all authors associated with a given technical paper. The locating numbers are identical to those in the Subject Index. The Chronological Index, pages 1973-1982, also lists all papers by their locating numbers. This listing contains titles, authors and their affiliations, and volume, issue number, and page where the paper appeared. It also gives the AIAA paper number, if any, on which the article was based. Comments, Replies, and Errata are listed directly beneath the paper to which they refer. If the paper to which they refer was published prior to 2006, 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, C06-069 Embedded Laser Doppler Veloc- C06-055 Unsteady-Aerodynamic Shape CONVENTIONAL, STOL/VTOL imetry Boundary-Layer Investigation on a Sensitivities for Airplane Aeroservoelastic Tilt-Rotor Blade Configuration Optimization Aerodynamics C06-129 Viscous-Inviscid Method for Air- C06-008 Aircraft Acceleration Prediction C06-005 Extensions of Overset Unstructured foil Analysis and Design for Aviation and Due to Atmospheric Disturbances with Grids to Multiple Bodies in Contact Windmills Flight Data Validation C06-041 Drag of Spheroid-Cone Shaped C06-077 Poststall Prediction of Multiple- C06-044 Low Speed Design and Analysis of Airship Lifting-Surface Configurations Using a Wing/Winglet Combinations Including Vis- C06-049 Oscillating Wing Loadings with Decambering Approach cous Effects Trailing-Edge Strips C06-116 Drag Reductions Possible with C06-149 Preliminary Parametric Study of C06-016 Computational Methods for Simu- Aircraft Employing Outboard Horizontal Gurney Flap Dependencies lation of Flow Around Helicopter Engine Stabilizers C06-202 Separation Control on a Trailing- Inlet C06-164 Stability and Control Character- Edge Flap Using Air Jet Vortex Generators C06-110 Aerodynamics of Formation Flight istics of a New FAR 23 Airplane C06-012 Active Multiple Winglets for C06-082 Origin of Exponential Solution for C06-103 Sting Deflection Model for Auto- Improved Unmanned-Aerial-Vehicle Per- Laminar Decay of Isolated Vortex matic Image Registration in Wind-Tunnel formance C06-013 Effect of Winglet Dihedral on a Tip Testing. C06-043 Classical Wing Theory and the Vortex C06-147 Flowfield Measurements About an Downward Velocity of Vortex Wakes C06-053 Coated Hot-Film Sensors for Tran- Airfoil with Leading-Edge Ice Shapes C06-047 Aerodynamic Loads on Airfoil with sition Detection in Cruise Flight C06-160 Additional Aerodynamic Features Trailing-Edge Flap Pitching with Different C06-007 Wind Tunnel Boundary Correc- of Wing-Gurney Flap Flows Frequencies tions for a Full Scale 1903 Wright Flyer C06-155 Effects of Free-Stream Turbulence C06-157 Robust Objective Functions for Replica on Wing-Tip Vortex Formation and Near Sonic-Boom Minimization C06-115 Methodology for Performance Field C06-190 Influence of Steady Pitch Rate on 2- Analysis of Aerospace Vehicles Using the C06-236 Model of the Aerodynamic Behav- D Airfoil Aerodynamic Characteristics at Laws of Thermodynamics ior of a Pararotor Incidence C06-072 Transonic Free-To-Roll Analysis of C06-231 Frequency Response Model for C06-167 Study of Delayed-Detached Eddy the F-35 (Joint Strike Fighter) Aircraft Branched Pneumatic Sensing Systems Simulation with Weakly Nonlinear Turbu- C06-134 Combining Passive Control Meth- C06-243 Interaction of a Streamwise Vortex lence Model od for Dynamic Stall Control with a Blade Tip Vortex C06-193 Application of Gurney Flap on a C06-100 Robust Airfoil Shape Optimization C06-241 Numerical Simulation of Helicopter Simplified Forward-Swept Aircraft Model Using Design For Six Sigma Engine Jet and Fuselage Temperature Field C06-107 Low Speed Wind Tunnel Buffet C06-105 Numerical Simulation and Physical C06-104 New Method for Evaluating the Testing on the F/A-22 Characteristics Analysis for Slender Wing Hemispheric Five-Hole Probes C06-170 Flight Testing a Simple Fix to Rock C06-001 Accurate Drag Prediction Using Lateral Stability Deficiencies C06-124 Analysis of General-Aviation Air- Cobalt C06-186 New Mixed Method for Unsteady craft Wing Sections with Drooped Leading C06-204 Kiissner’s Function in the Sharp Aerodynamic Force Approximations for Edges Edged Gust Problem—A Correction Aeroservoelasticity Studies C06-125 Hysteresis and Broad Flow Features C06-191 Effect of Full-Span Gurney Flap C06-175 Dynamics of Corotating Vortex on a Swept Wing at High Lift Height on Wing Wake Vortex Alleviation Filaments Part 1: Analytical Model C06-033 Wind-Tunnel Experimental Inves- C06-198 Simple Model for Turbulent Tip C06-173 Vortex-Free Flight Corridors for tigation on a Fixed-Wing Micro Air Vehicle Vortices Aircraft Executing Compressed Landing C06-122 Detached-Eddy Simulation of C06-011 Novel Taguchi-Simulated Anneal- Operations Three Airfoils with Different Stall Onset ing Method Applied to Airfoil and Wing C06-232 Aerodyamic Flow Control of an Mechanisms Planform Optimization Airfoil with Small Trailing-Edge Strips 1960 JOURNAL OF AIRCRAFT Vol. 43, No. 6, November—December 2006 2006 Journal of Aircraft Index How to Use the Index In the Subject Index, pages 1960-1969, 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 1970-1972, lists all authors associated with a given technical paper. The locating numbers are identical to those in the Subject Index. The Chronological Index, pages 1973-1982, also lists all papers by their locating numbers. This listing contains titles, authors and their affiliations, and volume, issue number, and page where the paper appeared. It also gives the AIAA paper number, if any, on which the article was based. Comments, Replies, and Errata are listed directly beneath the paper to which they refer. If the paper to which they refer was published prior to 2006, 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, C06-069 Embedded Laser Doppler Veloc- C06-055 Unsteady-Aerodynamic Shape CONVENTIONAL, STOL/VTOL imetry Boundary-Layer Investigation on a Sensitivities for Airplane Aeroservoelastic Tilt-Rotor Blade Configuration Optimization Aerodynamics C06-129 Viscous-Inviscid Method for Air- C06-008 Aircraft Acceleration Prediction C06-005 Extensions of Overset Unstructured foil Analysis and Design for Aviation and Due to Atmospheric Disturbances with Grids to Multiple Bodies in Contact Windmills Flight Data Validation C06-041 Drag of Spheroid-Cone Shaped C06-077 Poststall Prediction of Multiple- C06-044 Low Speed Design and Analysis of Airship Lifting-Surface Configurations Using a Wing/Winglet Combinations Including Vis- C06-049 Oscillating Wing Loadings with Decambering Approach cous Effects Trailing-Edge Strips C06-116 Drag Reductions Possible with C06-149 Preliminary Parametric Study of C06-016 Computational Methods for Simu- Aircraft Employing Outboard Horizontal Gurney Flap Dependencies lation of Flow Around Helicopter Engine Stabilizers C06-202 Separation Control on a Trailing- Inlet C06-164 Stability and Control Character- Edge Flap Using Air Jet Vortex Generators C06-110 Aerodynamics of Formation Flight istics of a New FAR 23 Airplane C06-012 Active Multiple Winglets for C06-082 Origin of Exponential Solution for C06-103 Sting Deflection Model for Auto- Improved Unmanned-Aerial-Vehicle Per- Laminar Decay of Isolated Vortex matic Image Registration in Wind-Tunnel formance C06-013 Effect of Winglet Dihedral on a Tip Testing. C06-043 Classical Wing Theory and the Vortex C06-147 Flowfield Measurements About an Downward Velocity of Vortex Wakes C06-053 Coated Hot-Film Sensors for Tran- Airfoil with Leading-Edge Ice Shapes C06-047 Aerodynamic Loads on Airfoil with sition Detection in Cruise Flight C06-160 Additional Aerodynamic Features Trailing-Edge Flap Pitching with Different C06-007 Wind Tunnel Boundary Correc- of Wing-Gurney Flap Flows Frequencies tions for a Full Scale 1903 Wright Flyer C06-155 Effects of Free-Stream Turbulence C06-157 Robust Objective Functions for Replica on Wing-Tip Vortex Formation and Near Sonic-Boom Minimization C06-115 Methodology for Performance Field C06-190 Influence of Steady Pitch Rate on 2- Analysis of Aerospace Vehicles Using the C06-236 Model of the Aerodynamic Behav- D Airfoil Aerodynamic Characteristics at Laws of Thermodynamics ior of a Pararotor Incidence C06-072 Transonic Free-To-Roll Analysis of C06-231 Frequency Response Model for C06-167 Study of Delayed-Detached Eddy the F-35 (Joint Strike Fighter) Aircraft Branched Pneumatic Sensing Systems Simulation with Weakly Nonlinear Turbu- C06-134 Combining Passive Control Meth- C06-243 Interaction of a Streamwise Vortex lence Model od for Dynamic Stall Control with a Blade Tip Vortex C06-193 Application of Gurney Flap on a C06-100 Robust Airfoil Shape Optimization C06-241 Numerical Simulation of Helicopter Simplified Forward-Swept Aircraft Model Using Design For Six Sigma Engine Jet and Fuselage Temperature Field C06-107 Low Speed Wind Tunnel Buffet C06-105 Numerical Simulation and Physical C06-104 New Method for Evaluating the Testing on the F/A-22 Characteristics Analysis for Slender Wing Hemispheric Five-Hole Probes C06-170 Flight Testing a Simple Fix to Rock C06-001 Accurate Drag Prediction Using Lateral Stability Deficiencies C06-124 Analysis of General-Aviation Air- Cobalt C06-186 New Mixed Method for Unsteady craft Wing Sections with Drooped Leading C06-204 Kiissner’s Function in the Sharp Aerodynamic Force Approximations for Edges Edged Gust Problem—A Correction Aeroservoelasticity Studies C06-125 Hysteresis and Broad Flow Features C06-191 Effect of Full-Span Gurney Flap C06-175 Dynamics of Corotating Vortex on a Swept Wing at High Lift Height on Wing Wake Vortex Alleviation Filaments Part 1: Analytical Model C06-033 Wind-Tunnel Experimental Inves- C06-198 Simple Model for Turbulent Tip C06-173 Vortex-Free Flight Corridors for tigation on a Fixed-Wing Micro Air Vehicle Vortices Aircraft Executing Compressed Landing C06-122 Detached-Eddy Simulation of C06-011 Novel Taguchi-Simulated Anneal- Operations Three Airfoils with Different Stall Onset ing Method Applied to Airfoil and Wing C06-232 Aerodyamic Flow Control of an Mechanisms Planform Optimization Airfoil with Small Trailing-Edge Strips 1960 J. AIRCRAFT, VOL. 43, NO. 6: 2006 INDEX 1961 C06-168 Longitudinal Dynamics of a Perch- C06-132 Numerical Simulations for Trans- C06-019 Chebyshev Polynomials for Un- ing Aircraft port Aircraft High-Lift Configurations steady Aerodynamic Calculations in Aero- C06-128 High-Lift Propulsive Airfoil with Using Adaptive Cartesian Grid Methods servoelasticity Integrated Crossflow Fan C06-099 Experimental Investigation of Vor- C06-065 New Hybrid Interpolation Method C06-200 Tip Vortex Dependence with Angle tex Flow over an 80 Degree/60 Degree for Motion Transfer in Fluid-Structure of Attack Double Delta Wing at Sideslip Interactions C06-201 Gust Resistant Fixed Wing Micro C06-113 Civil-Transport Wing Design Con- C06-121 On the Formulation of Minimum- Air Vehicle cept Exploiting New Technologies State Approximation as a Nonlinear C06-223 Hybrid Inverse Design Method for C06-203 Ejection Seat Test Techniques in a Optimization Problem Nonlifting Bodies in Incompressible Flow High-Speed Wind Tunnel C06-095 Multi-Objective and Multidiscipli- C06-224 Synthetic Jet Control Effectiveness C06-133 Rolling Moment Characteristics of nary Design Optimization of Supersonic on Stationary and Pitching Airfoils Supersonic Transport Configurations at Fighter Wing C06-230 Aerodynamic Design of Complex High Incidence Angles C06-021 Design-Oriented Structural Model Configurations with Junctions C06-108 Investigating Correlations Between Order Reduction for Strain-Actuated Flight C06-196 Unsteady Rolling Moment Charac- Reynolds-Averaged Flowfields and Noise Vehicle Structures teristics for a Fighter Oscillating with for Forced Mixed Jets C06-087 Aeroelasticity of Nonlinear Struc- Yawing-Rolling Coupled Motion C06-084 Oscillating-Wing Tip Vortex with tures Using the Corotational Method C06-014 Constant Altitude—Constant Mach Passive Short-Span Trailing-Edge Flaps C06-039 Swashplateless Helicopter Rotor Number Cruise Range of Transport Aircraft C06-138 Tip Vortex Control via an Active System with Trailing-Edge Flaps for Flight with Compressibility Effects Trailing-Edge Tab and Vibration Controls C06-050 Minimizing Induced Drag with C06-153 Effect of Flap and Slat Riggings on Wing Twist, Computational-Fluid-Dynam- 2-D High-Lift Aerodynamics C06-058 Estimating the Probability of Fail- ics Validation C06-194 Preliminary Investigation of Arc ure of a Nonlinear Aeroelastic System C06-085 Rotor Airloads Prediction Using Wing Pitch Characteristics C06-086 Flutter of High-Speed Civil Trans- Loose Aerodynamic/Structural Coupling C06-165 Effects of Canard Sweep and port Flexible Semispan Model: Time C06-042 New Hybrid Method for Predicting Canard-Spanwise Blowing Magnitude on Frequency Analysis the Flowfields of Helicopter Rotors Lift Increment C06-226 Analysis and Wind Tunnel Testing C06-009 Wing Drag Prediction and Decom- C06-120 Numerical Simulation of the Effects of a Piezoelectric Tab for Aeroelastic position of Spanwise Blowing on Wing-tip Vortex Control Applications C06-097 Design Exploration of Aerodynam- Formation and Evolution C06-225 Flight Dynamics of Highly Flexible ic Wing Shape for Reusable Launch Vehicle C06-237 Vortex Behaviors of Rolled Super- Flying Wings Flyback Booster sonic Transport Configuration with Lead- C06-186 New Mixed Method for Unsteady C06-015 Drag Reduction on Gurney Flaps by ing-Edge Flaps Aerodynamic Force Approximations for Three-Dimensional Modifications C06-119 Effect of Injection Slot Size on the Aeroservoelasticity Studies C06-032 Response of a Free-to-Roll Slender Performance of Coflow Jet Airfoil C06-023 Experimental and Analytical Study Delta Wings to Pitching and Plunging C06-159 Error Estimation and Grid Adapta- of Blade Lag Damping Augmentation using C06-121 On the Formulation of Minimum- tion Using Euler Adjoint Method Chordwise Absorbers State Approximation as a Nonlinear C06-182 Temperature Correction of Pres- C06-055 Unsteady-Aerodynamic Shape Optimization Problem sure-Sensitive Paint for Industrial Wind Sensitivities for Airplane Aeroservoelastic C06-150 Preliminary Flight Tests of aH inge- Tunnel Testing Configuration Optimization Less Roll Control Effecter C06-229 Effects of Tail Dihedral on Static C06-018 Induced Drag Reduction Using C06-140 Control of Rotorcraft Retreating Stability Aeroelastic Tailoring with Adaptive Control Blade Stall Using Air-Jet Vortex Generators C06-199 Active Boundary-Layer Separation Surfaces C06-034 Shape Optimization of Stratosphere Control on a Multi-Element Airfoil C06-222 Efficient Computation of Robust Airship C06-233 Phase-Locked Particle Image Ve- Flutter Boundaries Using the .-k Method C06-046 Validation of | Computations locimetry Measurements of a Flapping Wing C06-184 Sensitivities and Approximations Around High-Lift Configurations by Struc- C06-242 Vortex Interactions Between for Aeroservoelastic Shape Optimization tured- and Unstructured-Mesh Chined Forebody and Strake with Gust Response Constraints C06-019 Chebyshev Polynomials for Un- C06-204 Kiissner’s Function in the Sharp steady Aerodynamic Calculations in Aero- servoelasticity Aeroelasticity and Aeroservoelasticity Edged Gust Problem—A Correction C06-088 Unified Aeroelastic and Flight C06-040 Two-Dimensional Simulation of C06-126 Stochastic Analysis of a Nonlinear Dynamic Surface Roughness for Aerody- Aeroelastic Model Using the Response Dynamic Formulation via Rational Function namic Flow Control Surface Method Approximations C06-078 Induced Drag Minimization: A C06-183 Sensitivity Study of Downwash C06-130 Analysis Tools for the Detection of Variational Approach Using the Acceler- Weighting Methods for Transonic Aeroe- Intermittent Nonlinear Aeroelastic Phenom- ation Potential lastic Stability Analysis ena C06-080 Aerodynamic Development of a C06-211 Optimal Scheduling of Control C06-056 Active Flutter Control with a V- Ground Run-Up Enclosure for Propeller Surfaces on a Flexible Wing to Reduce Stack Piezoelectric Flap Actuator Transport Aircraft Induced Drag C06-002 Small Disturbance Navier-Stokes C06-083 Numerical Investigation of Low- C06-148 Aeroservoelastic Modeling and Method: Efficient Tool for Predicting Aspect-Ratio Wings at Low Reynolds Sensitivity Analysis with Strain Actuators Unsteady Air Loads Numbers C06-102 Mathematical Modeling for Modal C06-106 Static/Dynamic Correction Ap- C06-066 Trailing Vortex Rollup from a Wing Computations Concerning a Morphable proach for Reduced-Order Modeling of Equipped with a Gurney Flap Wing Unsteady Aerodynamics 1962 J. AIRCRAFT, VOL. 43, NO. 6: 2006 INDEX Aerospace Plane Civil Missions and Transportation C06-228 Sonic Boom Minimization Using C06-097 Design Exploration of Aerodynam- C06-037 Multidisciplinary Approach to In- Inverse Design and Probabilistic Acoustic ic Wing Shape for Reusable Launch Vehicle telligent Unmanned-Airborne-Vehicles Propagation Flyback Booster Mission Planning Deceleration Systems C06-086 Flutter of High-Speed Civil Trans- Air Transportation port Flexible Semispan Model: Time C06-118 Stability Analysis of a Free Falling Pararotor C06-014 Constant Altitude—Constant Mach Frequency Analysis C06-197 Experimental Investigation of Number Cruise Range of Transport Aircraft with Compressibility Effects Collision Avoidance Three Rotating Parachutes C06-236 Model of the Aerodynamic Behav- C06-205 Overview of the Small Aircraft C06-206 Small Aircraft Transportation Sys- Transportation System Project Four En- tem Higher Volume Operations Flight ior of a Pararotor abling Operating Capabilities Experiment Economics C06-187 Bréguet Range Equation? C06-163 Decision Support Approach to Fleet C06-026 Piloting Strategies for Controlling a Communication and Air Traffic Control Maintenance Requirements in the Aviation Transport Aircraft After Vertical-Tail Loss C06-209 Improving Aircraft Sequencing and Industry C06-048 Aerodynamic Analysis of a Jet Separation at a Small Aircraft Trans- C06-031 Numerical Method for Cost-Weight Transport in Windshear Encounter During portation System Airport Optimization of Stringer-Skin Panels Landing Configuration Design C06-123 DATUM Project: Cost Estimating C06-116 Drag Reductions Possible with Environment for Support of Aerospace Aircraft Employing Outboard Horizontal C06-179 Joined-Wing Sensor-Craft Confi- Design Decision Making Stabilizers guration Design C06-111 Value-Based Multidisciplinary Op- C06-206 Small Aircraft Transportation Sys- C06-223 Hybrid Inverse Design Method for timization for Commercial Aircraft Design tem Higher Volume Operations Flight Nonlifting Bodies in Incompressible Flow and Business Risk Assessment Experiment C06-097 Design Exploration of Aerodynam- C06-098 Preliminary Evaluation of Noise ic Wing Shape for Reusable Launch Vehicle Flight Control Integration Reduction Approaches for a Functionally Flyback Booster C06-019 Chebyshev Polynomials for Un- Silent Aircraft C06-075 Transonic Airfoil Shape Optimiza- steady Aerodynamic Calculations in Aero- C06-191 Effect of Full-Span Gurney Flap tion in Preliminary Design Environment servoelasticity Height on Wing Wake Vortex Alleviation C06-095 Multi-Objective and Multidiscipli- C06-207 A Primary Flight Display Vastly C06-202 Separation Control on a Trailing- nary Design Optimization of Supersonic Improves Situational Awareness and Accu- Edge Flap Using Air Jet Vortex Generators Fighter Wing racy of Flight C06-195 Cable-Supported Sliding Payload C06-111 Value-Based Multidisciplinary Op- C06-127 Prognostics and Health Manage- Deployment from a Circling Fixed-Wing timization for Commercial Aircraft Design ment as Design Variable in Air-Vehicle Aircraft and Business Risk Assessment Conceptual Design C06-113 Civil-Transport Wing Design Con- Airframe-Propulsion Integration cept Exploiting New Technologies Flight Mechanics C06-027 Infrared Signatures of Low-Flying C06-099 Experimental Investigation of Vor- C06-077 Poststall Prediction of Multiple- Aircraft and Their Rear Fuselage Skin’s tex Flow over an 80 Degree/60 Degree Lifting-Surface Configurations Using a Emissivity Optimization Double Delta Wing at Sideslip Decambering Approach C06-180 Designing and Testing a Blended C06-066 Trailing Vortex Rollup from a Wing C06-026 Piloting Strategies for Controlling a Wing Body with Boundary-Layer Ingestion Equipped with a Gurney Flap Transport Aircraft After Vertical-Tail Loss Nacelles C06-194 Preliminary Investigation of Arc C06-029 Multidisciplinary Design Optimi- C06-115 Methodology for Performance Wing Pitch Characteristics zation for Aeromechanics and Handling Analysis of Aerospace Vehicles Using the C06-127 Prognostics and Health Manage- Qualities Laws of Thermodynamics ment as Design Variable in Air-Vehicle C06-219 Data Analysis of Phoenix Reusable C06-045 General Aviation Propeller-Air- Conceptual Design Launch Vehicle Demonstrator Flight Test frame Integration Simulations C06-164 Stability and Control Character- C06-169 Effect of Propeller Torque on C06-119 Effect of Injection Slot Size on the istics of aN ew FAR 23 Airplane Minimum-Control Airspeed Performance of Coflow Jet Airfoil C06-100 Robust Airfoil Shape Optimization C06-187 Bréguet Range Equation? C06-230 Aerodynamic Design of Complex Using Design For Six Sigma C06-158 Flight Handling Qualities of the Configurations with Junctions C06-157 Robust Objective Functions for Wright Brothers’ 1905 Flyer 3 C06-201 Gust Resistant Fixed Wing Micro Sonic-Boom Minimization C06-229 Effects of Tail Dihedral on Static Air Vehicle C06-123 DATUM Project: Cost Estimating Stability Environment for Support of Aerospace C06-014 Constant Altitude—Constant Mach Airframe-Weapon System Integration Design Decision Making Number Cruise Range of Transport Aircraft C06-139 Establishment of Gun Blast Wave C06-149 Preliminary Parametric Study of with Compressibility Effects Model and Structural Analysis for Blast Gurney Flap Dependencies C06-196 Unsteady Rolling Moment Charac- Load C06-044 Low Speed Design and Analysis of teristics for a Fighter Oscillating with Wing/Winglet Combinations Including Vis- Yawing-Rolling Coupled Motion Cabin Environment, Crew Training, and cous Effects Life Support C06-011 Novel Taguchi-Simulated Anneal- Flight Operations C06-203 Ejection Seat Test Techniques in a ing Method Applied to Airfoil and Wing C06-004 Noise-Minimum Runway-Inde- High-Speed Wind Tunnel Planform Optimization pendent Aircraft Approach Design for C06-154 Aircraft Accident Statistics and C06-240 Multidisciplinary Optimization Baltimore-Washington International Airport Knowledge Database: Analyzing Passenger Framework for Control-Configuration In- C06-114 Optimization of Flexible Approach Behavior in Aviation Accidents tegration in Aircraft Conceptual Design Trajectories Using a Genetic Algorithm J. AIRCRAFT, VOL. 43, NO. 6: 2006 INDEX Flow Control C06-209 Improving Aircraft Sequencing and Military Missions C06-032 Response of a Free-to-Roll Slender Separation at a Small Aircraft Trans- C06-227 Cooperative Control of Multiple Delta Wings to Pitching and Plunging portation System Airport Unmanned Aerial Vehicles Using the C06-150 Preliminary Flight Tests of aH inge- Ground Support Potential Field Theory Less Roll Control Effecter C06-140 Control of Rotorcraft Retreating C06-109 Development and Experimental Noise Blade Stall Using Air-Jet Vortex Generators Validation of a Shipboard Helicopter On- C06-098 Preliminary Evaluation of Noise C06-040 Two-Dimensional Simulation of Deck Maneuvering Simulation Reduction Approaches for a Functionally Dynamic Surface Roughness for Aerody- C06-090 Diagnostics of Tool—Part Interac- Silent Aircraft namic Flow Control tions During Riveting on an Aluminum C06-157 Robust Objective Functions for C06-013 Effect of Winglet Dihedral on a Tip Aircraft Fuselage Sonic-Boom Minimization Vortex Landing Dynamics C06-131 Response Surface Method Optimi- C06-015 Drag Reduction on Gurney Flaps by C06-025 Progressive Certification Process zation of Uniform and Axially Segmented Three-Dimensional Modifications Based on Living Systems Architecture Duct Acoustics Liners C06-224 Synthetic Jet Control Effectiveness Using Learning Capable Controllers C06-108 Investigating Correlations Between on Stationary and Pitching Airfoils C06-063 Design of Skid Landing Gears by Reynolds-Averaged Flowfields and Noise C06-199 Active Boundary-Layer Separation Means of Multibody Optimization for Forced Mixed Jets Control on a Multi-Element Airfoil C06-010 Flight Envelope Expansion in C06-073 Elegant Concept for Reduction of C06-099 Experimental Investigation of Vor- Landing Phase Using Classic, Intelligent Jet Noise from Turbofan Engines tex Flow over an 80 Degree/60 Degree and Adaptive Controllers C06-074 Noise of Dual-Stream Beveled Double Delta Wing at Sideslip Nozzles at Supercritical Pressure Ratios C06-113 Civil-Transport Wing Design Con- Lighter-Than-Air Systems C06-217 Fan Noise Reduction with In- cept Exploiting New Technologies C06-041 Drag of Spheroid-Cone Shaped creased Bypass Nozzle Area C06-165 Effects of Canard Sweep and Airship C06-036 Experimental Study on Aircraft Canard-Spanwise Blowing Magnitude on C06-034 Shape Optimization of Stratosphere Landing Gear Noise Lift Increment Airship C06-117 Nonlinear Response and Fatigue C06-119 Effect of Injection Slot Size on the C06-142 Study of a Multitethered Aerostat Life of Isotropic Panels Subjected to Performance of Coflow Jet Airfoil System: Experimental Observations and Nonwhite Noise C06-138 Tip Vortex Control via an Active Model Validation C06-080 Aerodynamic Development of a Trailing-Edge Tab C06-141 Estimation of Flyable Regions for Ground Run-Up Enclosure for Propeller C06-084 Oscillating-Wing Tip Vortex with Planetary Airships Transport Aircraft Passive Short-Span Trailing-Edge Flaps C06-004 Noise-Minimum Runway-Inde- Man/Machine Interface C06-178 Unsteady Computational Investiga- pendent Aircraft Approach Design for tions of Deploying Load Control Microtabs C06-166 Human—Computer Interaction Baltimore-Washington International Airport Analysis of Flight Management System C06-235 Design of Vortex Generator Flow Messages Performance Control in Inlets C06-090 Diagnostics of Tool—Part Interac- C06-024 Evaluation of Takeoff Performance C06-202 Separation Control on a Trailing- tions During Riveting on an Aluminum Monitoring Algorithm in Large Jet Trans- Edge Flap Using Air Jet Vortex Generators Aircraft Fuselage port Operations C06-018 Induced Drag Reduction Using C06-092 Analysis of Human Pilot Control C06-147 Flowfield Measurements About an Aeroelastic Tailoring with Adaptive Control Inputs Using Neural Network Airfoil with Leading-Edge Ice Shapes Surfaces C06-116 Drag Reductions Possible with C06-193 Application of Gurney Flap on a Manufacturing Aircraft Employing Outboard Horizontal Simplified Forward-Swept Aircraft Model C06-090 Diagnostics of Tool—Part Interac- Stabilizers C06-134 Combining Passive Control Meth- tions During Riveting on an Aluminum C06-012 Active Multiple Winglets for od for Dynamic Stall Control Aircraft Fuselage Improved Unmanned-Aerial-Vehicle Per- C06-123 DATUM Project: Cost Estimating formance Fuels and Fuel Systems Environment for Support of Aerospace Propeller and Rotor Systems C06-161 Optimal Conceptual Design of Design Decision Making Aircraft Fuel Transfer Systems Micro Air Vehicles C06-241 Numerical Simulation of Helicopter Engine Jet and Fuselage Temperature Field C06-064 Design, Fabrication, and Perform- C06-198 Simple Model for Turbulent Tip General Aviation ance Test of a Rotary-Wing Micro Aerial Vortices C06-228 Sonic Boom Minimization Using Vehicle C06-045 General Aviation Propeller-Air- Inverse Design and Probabilistic Acoustic C06-033 Wind-Tunnel Experimental Inves- frame Integration Simulations Propagation tigation on a Fixed-Wing Micro Air Vehicle C06-061 Failure-Rate Prediction for De C06-035 Challenges Facing Future Micro- Rotorcraft Havilland Dash-8 Tires Employing Neural- Air-Vehicle Development C06-094 Investigation of External Airbags Network Technique C06-201 Gust Resistant Fixed Wing Micro for Rotorcraft Crashworthiness C06-124 Analysis of General-Aviation Air- Air Vehicle 06-134 Combining Passive Control Meth- craft Wing Sections with Drooped Leading 06-233 Phase-Locked Particle Image Ve- od for Dynamic Stall Control Edges locimetry Measurements of a Flapping Wing 06-029 Multidisciplinary Design Optimi- C06-049 Oscillating Wing Loadings with C06-083 Numerical Investigation of Low- zation for Aeromechanics and Handling Trailing-Edge Strips Aspect-Ratio Wings at Low Reynolds Qualities C06-210 Trajectory Management Concepts Numbers C06-016 Computational Methods for Simu- For Future Small Aircraft Transportation C06-067 Flexible- and Rigid-Wing Micro lation of Flow Around Helicopter Engine Systems Air Vehicle: Lift and Drag Comparison Inlet 1964 J. AIRCRAFT, VOL. 43, NO. 6: 2006 INDEX 06-064 Design, Fabrication, and Perform- C06-145 Emergency Flight Planning Ap- System Effectiveness ance Test of a Rotary-Wing Micro Aerial plied to Total Loss of Thrust C06-174 Two General Methods for Calculat- Vehicle ing the Aircraft Equivalent Singly Vulner- Simulation C06-069 Embedded Laser Doppler Veloc- able Area imetry Boundary-Layer Investigation on a 06-016 Computational Methods for Simu- C06-136 Aircraft Vulnerable-Area Decom- Tilt-Rotor Blade lation of Flow Around Helicopter Engine position Method in the Overlapping Region 06-241 Numerical Simulation of Helicopter Inlet of Components Engine Jet and Fuselage Temperature Field C06-137 Study of the Residual Strain in Lap C06-143 Solving the Combinatorial Explo- C€06-112 Development of Mach Scale Rotors Joints sion Problem When Calculating the Multi- with Tailored Composite Coupling for C06-109 Development and Experimental ple-Hit Vulnerability of Aircraft Vibration Reduction Validation of a Shipboard Helicopter On- C06-023 Experimental and Analytical Study Deck Maneuvering Simulation of Blade Lag Damping Augmentation using C06-001 Accurate Drag Prediction Using Testing, Flight and Ground Chordwise Absorbers Cobalt C06-182 Temperature Correction of Pres- C06-140 Control of Rotorcraft Retreating C06-008 Aircraft Acceleration Prediction sure-Sensitive Paint for Industrial Wind Blade Stall Using Air-Jet Vortex Generators Due to Atmospheric Disturbances with Tunnel Testing C06-063 Design of Skid Landing Gears by Flight Data Validation C06-221 Evaluation of a Three-Degree-of- Means of Multibody Optimization C06-186 New Mixed Method for Unsteady Freedom Test Rig for Stability Derivative C06-039 Swashplateless Helicopter Rotor Aerodynamic Force Approximations for Estimation System with Trailing-Edge Flaps for Flight Aeroservoelasticity Studies C06-080 Aerodynamic Development of a C06-195 Cable-Supported Sliding Payload and Vibration Controls Ground Run-Up Enclosure for Propeller Deployment from a Circling Fixed-Wing C06-079 Performance and Stability Analysis Transport Aircraft Aircraft of a Shrouded-Fan Unmanned Aerial C06-170 Flight Testing a Simple Fix to C06-185 Icing Encounter Flight Simulator Vehicle Lateral Stability Deficiencies C06-168 Longitudinal Dynamics of a Perch- C06-085 Rotor Airloads Prediction Using C06-103 Sting Deflection Model for Auto- ing Aircraft Loose Aerodynamic/Structural Coupling matic Image Registration in Wind-Tunnel C06-158 Flight Handling Qualities of the 06-042 New Hybrid Method for Predicting Testing. Wright Brothers’ 1905 Flyer 3 the Flowfields of Helicopter Rotors C06-101 Refining Satellite Methods for C06-161 Optimal Conceptual Design of C06-215 CFD/CSD Prediction of Rotor Pitot-Static Calibration Aircraft Fuel Transfer Systems Vibratory Loads in High-Speed Flight C06-206 Small Aircraft Transportation Sys- Stealth tem Higher Volume Operations Flight Safety C06-027 Infrared Signatures of Low-Flying Experiment C06-089 Stress and Fatigue Analysis of Aircraft and Their Rear Fuselage Skin’s C06-041 Drag of Spheroid-Cone Shaped Modified Wing—Fuselage Connector for the Emissivity Optimization Airship Agricultural Aircraft C06-110 Aerodynamics of Formation Flight STOL/VTOL/STOVL C06-203 Ejection Seat Test Techniques in a High-Speed Wind Tunnel C06-194 Preliminary Investigation of Arc Uninhabited and Unmanned Air Vehicles Wing Pitch Characteristics C06-152 Verification and Validation of C06-181 Conceptual Design and Simulation C06-128 High-Lift Propulsive Airfoil with NASA LEWICE 2.2 Icing Software Code of aS mall Hybrid-Electric Unmanned Aerial Integrated Crossflow Fan C06-185 Icing Encounter Flight Simulator Vehicle 06-079 Performance and Stability Analysis C06-010 Flight Envelope Expansion in C06-012 Active Multiple Winglets for of a Shrouded-Fan Unmanned Aerial Landing Phase Using Classic, Intelligent Vehicle Improved Unmanned-Aerial-Vehicle Per- and Adaptive Controllers formance C06-025 Progressive Certification Process Structural Design (Including Loads) C06-037 Multidisciplinary Approach to In- Based on Living Systems Architecture C06-151 Time-Related Procedure to Struc- telligent Unmanned-Airborne-Vehicles Using Learning Capable Controllers tural Column Failure Mission Planning C06-154 Aircraft Accident Statistics and C06-172 Stability of Cyclically Symmetric C06-227 Cooperative Control of Multiple Knowledge Database: Analyzing Passenger Strained Pumpkin Balloons and the For- Unmanned Aerial Vehicles Using the Behavior in Aviation Accidents mation of Undesired Equilibria Potential Field Theory C06-171 Proposed Methodology for the Use C06-211 Optimal Scheduling of Control C06-235 Design of Vortex Generator Flow of Computer Simulation to Enhance Aircraft Surfaces on a Flexible Wing to Reduce Control in Inlets Evacuation Certification Induced Drag C06-079 Performance and Stability Analysis C06-213 Damage Tolerance Management C06-089 Stress and Fatigue Analysis of of a Shrouded-Fan Unmanned Aerial for Aircraft and Rotorcraft Structural Modified Wing—Fuselage Connector for the Vehicle Components Agricultural Aircraft C06-035 Challenges Facing Future Micro- C06-048 Aerodynamic Analysis of a Jet C06-031 Numerical Method for Cost-Weight Air-Vehicle Development Transport in Windshear Encounter During Optimization of Stringer-Skin Panels Landing C06-020 Structural Design Process Improve- C06-062 Solution for Aircraft Anti-Icing ment Using Evolutionary Finite Element Vibration System Simulation by a Modified Perturba- Models C06-039 Swashplateless Helicopter Rotor tion Method System with Trailing-Edge Flaps for Flight C06-026 Piloting Strategies for Controlling a Structural Materials and Vibration Controls Transport Aircraft After Vertical-Tail Loss C06-216 Some Recommendations for Char- C06-112 Development of Mach Scale Rotors C06-094 Investigation of External Airbags acterization of Composite Panels by Means with Tailored Composite Coupling for for Rotorcraft Crashworthiness of Drop Tower Impact Testing Vibration Reduction J. AIRCRAFT, VOL. 43, NO. 6: 2006 INDEX 1965 COMPUTING, INFORMATION, C06-038 Nozzle Orientation Effects and C06-132 Numerical Simulations for Trans- AND COMMUNICATION Nonlinear Interactions Between Twin Jets port Aircraft High-Lift Configurations of Complex Geometry Using Adaptive Cartesian Grid Methods Artificial Intelligence Systems C06-217 Fan Noise Reduction with In- C06-083 Numerical Investigation of Low- C06-028 Aircraft Ice Accretion Prediction creased Bypass Nozzle Area. Aspect-Ratio Wings at Low Reynolds Based on Neurai Networks C06-074 Noise of Dual-Stream Beveled Numbers C06-145 Emergency Flight Planning Ap- Nozzles at Supercritical Pressure Ratios C06-159 Error Estimation and Grid Adapta- plied to Total Loss of Thrust C06-073 Elegant Concept for Reduction of tion Using Euler Adjoint Method C06-061 Failure-Rate Prediction for De Jet Noise from Turbofan Engines C06-087 Aeroelasticity of Nonlinear Struc- Havilland Dash-8 Tires Employing Neural- C06-108 Investigating Correlations Between tures Using the Corotational Method Network Technique Reynolds-Averaged Flowfields and Noise C06-162 Validation of Implicit Algorithms C06-208 Flight Segment Identification as a for Forced Mixed Jets for Unsteady Flows Including Moving and Basis for Pilot Advisory Systems Deforming Grids Avionics Systems Boundary-Layer Stability and Transition C06-040 Two-Dimensional Simulation of Dynamic Surface Roughness for Aerody- C06-207 A Primary Flight Display Vastly C06-188 Experimental Investigation on namic Flow Control Improves Situational Awareness and Accu- Forced Boundary-Layer Transition of C06-046 Validation of | Computations racy of Flight Axisymmetric Inlet and Numerical Verifi- Around High-Lift Configurations by Struc- C06-166 Human—Computer Interaction cation ~ tured- and Unstructured-Mesh Analysis of Flight Management System C06-053 Coated Hot-Film Sensors for Tran- C06-230 Aerodynamic Design of Complex Messages sition Detection in Cruise Fiight Configurations with Junctions Controls and Displays C06-009 Wing Drag Prediction and Decom- C06-101 Refining Satellite Methods for Computational Fluid Dynamics position Pitot-Static Calibration C06-002 Small Disturbance Navier-Stokes C06-015 Drag Reduction on Gurney Flaps by Three-Dimensional Modifications Digital Avionics Systems Method: Efficient Tool for Predicting C06-085 Rotor Airloads Prediction Using Unsteady Air Loads C06-208 Flight Segment Identification as a Loose Aerodynamic/Structural Coupling Basis for Pilot Advisory Systems C06-005 Extensions of Overset Unstructured C06-050 Minimizing Induced Drag with Grids to Multiple Bodies in Contact ENERGY C06-124 Analysis of General-Aviation Air- Wing Twist, Computational-Fluid-Dynam- ics Validation craft Wing Sections with Drooped Leading Fuel Economy Edges Hypersonic Flow C06-181 Conceptual Design and Simulation C06-105 Numerical Simulation and Physical C06-192 Drag Reduction by Controlled Base of a Small Hybrid-Electric Unmanned Aerial Characteristics Analysis for Slender Wing Flow Separation. Vehicle Rock FLIGHT SIMULATOR SYSTEMS C06-034 Shape Optimization of Stratosphere Inlet, Nozzle, Diffuser, and Channel Flows Airship Guidance, Navigation, and Control C06-045 General Aviation Propeller-Air- C06-188 Experimental Investigation on Systems frame Integration Simulations Forced Boundary-Layer Transition of C06-238 Effect of Simulator Motion on Pilot C06-146 Numerical Investigation of Flow in Axisymmetric Inlet and Numerical Verifi- Behavior and Perception an Overexpanded Nozzle with Porous cation Human-Computer Interactions Surfaces C06-235 Design of Vortex Generator Flow C06-122 Detached-Eddy Simulation of Control in Inlets C06-209 Improving Aircraft Sequencing and Three Airfoils with Different Stall Onset C06-146 Numerical Investigation of Flow in Separation at a Small Aircraft Trans- an Overexpanded Nozzle with Porous Mechanisms portation System Airport Surfaces C06-129 Viscous-Inviscid Method for Air- Intelligent Systems foil Analysis and Design for Aviation and C06-038 Nozzle Orientation Effects and C06-048 Aerodynamic Analysis of a Jet Windmills Nonlinear Interactions Between Twin Jets Transport in Windshear Encounter During C06-135 Numerical Simulation of Flare Safe of Complex Geometry Landing Separation Jets, Wakes, and Viscid-Inviscid Flow FLUID DYNAMICS C06-071 Aero-Optic Performance of an Interactions Aircraft Forward-Facing Optical Turret C€06-081 Probabilistic Two-Phase Aircraft Aeroacoustics C06-167 Study of Delayed-Detached Eddy Wake-Vortex Model: Further Development C06-131 Response Surface Method Optimi- Simulation with Weakly Nonlinear Turbu- and Assessment zation of Uniform and Axially Segmented lence Model C06-073 Elegant Concept for Reduction of Duct Acoustics Liners C06-232 Aerodyamic Flow Control of an Jet Noise from Turbofan Engines C06-098 Preliminary Evaluation of Noise Airfoil with Small Trailing-Edge Strips C06-074 Noise of Dual-Stream’ Beveled Reduction Approaches for a Functionally C06-178 Unsteady Computational Investiga- Nozzles at Supercritical Pressure Ratios Silent Aircraft tions of Deploying Load Control Microtabs C06-160 Additional Aerodynamic Features C06-228 Sonic Boom Minimization Using C06-180 Designing and Testing a Blended of Wing-Gurney Flap Flows Inverse Design and Probabilistic Acoustic Wing Body with Boundary-Layer Ingestion C06-156 Computational Investigation and Propagation Nacelles Design Optimization of a Lateral-Jet- C06-231 Frequency Response Model for C06-153 Effect of Flap and Slat Riggings on Controlled Missile Branched Pneumatic Sensing Systems 2-D High-Lift Aerodynamics C06-173 Vortex-Free Flight Corridors for C06-189 Forward Flight Effects on Fan C06-152 Verification and Validation of Aircraft Executing Compressed Landing Noise from Supersonic 2-D Inlets NASA LEWICE 2.2 Icing Software Code Operations 1966 J. AIRCRAFT, VOL. 43, NO. 6: 2006 INDEX C06-043 Classical Wing Theory and the Unsteady Flows C06-138 Tip Vortex Control via an Active Downward Velocity of Vortex Wakes 06-069 Embedded Laser Doppler Veloc- Trailing-Edge Tab imetry Boundary-Layer Investigation on a C06-032 Response of a Free-to-Roll Slender Separated Flows Tilt-Rotor Blade Delta Wings to Pitching and Plunging C06-192 Drag Reduction by Controlled Base C06-002 Small Disturbance Navier-Stokes C06-081 Probabilistic Two-Phase Aircraft Flow Separation. Method: Efficient Tool for Predicting Wake-Vortex Model: Further Development C06-167 Study of Delayed-Detached Eddy Unsteady Air Loads and Assessment Simulation with Weakly Nonlinear Turbu- C06-106 Static/Dynamic Correction Ap- lence Model proach for Reduced-Order Modeling of GUIDANCE, CONTROL, AND C06-190 Influence of Steady Pitch Rate on 2- Unsteady Aerodynamics DYNAMICS TECHNOLOGY D Airfoil Aerodynamic Characteristics at C06-105 Numerical Simulation and Physical Incidence Characteristics Analysis for Slender Wing Aircraft Dynamics C06-243 Interaction of a Streamwise Vortex Rock C06-054 Free-to-Roll Investigation of the with a Blade Tip Vortex C06-178 Unsteady Computational Investiga- Preproduction F/A-18E Powered-Approach C06-122 Detached-Eddy Simulation of tions of Deploying Load Control Microtabs Wing Drop Three Airfoils with Different Stall Onset C06-047 Aerodynamic Loads on Airfoil with C06-225 Flight Dynamics of Highly Flexible Mechanisms Trailing-Edge Flap Pitching with Different Flying Wings C06-147 Flowfield Measurements About an Frequencies C06-168 Longitudinal Dynamics of a Perch- Airfoil with Leading-Edge Ice Shapes C06-107 Low Speed Wind Tunnel Buffet ing Aircraft C06-125 Hysteresis and Broad Flow Features Testing on the F/A-22 C06-118 Stability Analysis of a Free Falling on a Swept Wing at High Lift C06-162 Validation of Implicit Algorithms Pararotor C06-067 Flexible- and Rigid-Wing Micro for Unsteady Flows Including Moving and C06-005 Extensions of Overset Unstructured Air Vehicle: Lift and Drag Comparison Deforming Grids Grids to Multiple Bodies in Contact C06-199 Active Boundary-Layer Separation C06-183 Sensitivity Study of Downwash C06-072 Transonic Free-To-Roll Analysis of Control on a Multi-Element Airfoil Weighting Methods for Transonic Aeroe- the F-35 (Joint Strike Fighter) Aircraft C06-242 Vortex _ Interactions Between lastic Stability Analysis Chined Forebody and Strake Aircraft Guidance C06-224 Synthetic Jet Control Effectiveness Viscous Non-Boundary-Layer Flows C06-145 Emergency Flight Planning Ap- on Stationary and Pitching Airfoils plied to Total Loss of Thrust C06-071 Aero-Optic Performance of an C06-093 Monitoring Global Positioning Subsonic Flow Aircraft Forward-Facing Optical Turret System Satellite Orbit Errors for Aircraft C06-046 Validation of | Computations Landing Systems Around High-Lift Configurations by Struc- Vortices C06-207 A Primary Flight Display Vastly tured- and Unstructured-Mesh C06-155 Effects of Free-Stream Turbulence Improves Situational Awareness and Accu- C06-013 Effect of Winglet Dihedral on a Tip on Wing-Tip Vortex Formation and Near racy of Flight Vortex Field C06-210 Trajectory Management Concepts C06-047 Aerodynamic Loads on Airfoil with C06-160 Additional Aerodynamic Features For Future Small Aircraft Transportation Trailing-Edge Flap Pitching with Different of Wing-Gurney Flap Flows Systems Frequencies C06-082 Origin of Exponential Solution for Laminar Decay of Isolated Vortex Aircraft Stability and Control Supersonic Flow C06-051 Near-Field Wing-Tip Vortices and C06-229 Effects of Tail Dihedral on Static C06-038 Nozzle Orientation Effects and Exponential Vortex Solution Stability Nonlinear Interactions Between Twin Jets C06-107 Low Speed Wind Tunnel Buffet C06-158 Flight Handling Qualities of the of Complex Geometry Testing on the F/A-22 Wright Brothers’ 1905 Flyer 3 C06-212 Non-Gaussian Analysis of Turbu- C06-175 Dynamics of Corotating Vortex C06-221 Evaluation of a Three-Degree-of- lent Boundary Layer Fluctuating Pressure on Filaments Part 1: Analytical Model Freedom Test Rig for Stability Derivative Aircraft Skin Panels C06-173 Vortex-Free Flight Corridors for Estimation Aircraft Executing Compressed Landing C06-054 Free-to-Roll Investigation of the Transonic Flow Operations Preproduction F/A-18E Powered-Approach C06-182 Temperature Correction of Pres- C06-043 Classical Wing Theory and the Wing Drop sure-Sensitive Paint for Industrial Wind Downward Velocity of Vortex Wakes C06-164 Stability and Control Character- Tunnel Testing C06-198 Simple Model for Turbulent Tip istics of a New FAR 23 Airplane C06-183 Sensitivity Study of Downwash Vortices C06-056 Active Flutter Control with a V- Weighting Methods for Transonic Aeroe- C06-191 Effect of Full-Span Gurney Flap Stack Piezoelectric Flap Actuator lastic Stability Analysis Height on Wing Wake Vortex Alleviation C06-118 Stability Analysis of a Free Falling C06-009 Wing Drag Prediction and Decom- C06-242 Vortex Interactions Between Pararotor position Chined Forebody and Strake C06-169 Effect of Propeller Torque on C06-180 Designing and Testing a Blended C06-233 Phase-Locked Particle Image Ve- Minimum-Control Airspeed Wing Body with Boundary-Layer Ingestion locimetry Measurements of a Flapping Wing C06-240 Multidisciplinary Optimization Nacelles C06-066 Trailing Vortex Rollup from a Wing Framework for Control-Configuration In- C06-130 Analysis Tools for the Detection of Equipped with a Gurney Flap tegration in Aircraft Conceptual Design Intermittent Nonlinear Aeroelastic Phenom- C06-133 Rolling Moment Characteristics of C06-088 Unified Aeroelastic and Flight ena } Supersonic Transport Configurations at Dynamic Formulation via Rational Function C06-144 Robust Drag Minimization of High Incidence Angles Approximations Aerodynamic Wings in Engineering Envi- C06-084 Oscillating-Wing Tip Vortex with C06-170 Flight Testing a Simple Fix to ronment Passive Short-Span Trailing-Edge Flaps Lateral Stability Deficiencies J. AIRCRAFT, VOL. 43, NO. 6: 2006 INDEX 1967 Autonomous Vehicles Optimization Techniques C06-151 Time-Related Procedure to Struc- 06-227 Cooperative Control of Multiple C06-144 Robust Drag Minimization of tural Column Failure Unmanned Aerial Vehicles Using the Aerodynamic Wings in Engineering Envi- C06-065 New Hybrid Interpolation Method Potential Field Theory ronment for Motion Transfer in Fluid-Structure C06-131 Response Surface Method Optimi- Interactions Avionics Systems zation of Uniform and Axially Segmented C06-075 Transonic Airfoil Shape Optimiza- C06-024 Evaluation of Takeoff Performance Duct Acoustics Liners tion in Preliminary Design Environment Monitoring Algorithm in Large Jet Trans- C06-100 Robust Airfoil Shape Optimization C06-136 Aircraft Vulnerable-Area Decom- port Operations Using Design For Six Sigma position Method in the Overlapping Region Control System Design C06-011 Novel Taguchi-Simulated Anneal- of Components C06-064 Design, Fabrication, and Perform- ing Method Applied to Airfoil and Wing C06-143 Solving the Combinatorial Explo- ance Test of a Rotary-Wing Micro Aerial Planform Optimization sion Problem When Calculating the Multi- Vehicle C06-004 Noise-Minimum —Runway-Inde- ple-Hit Vulnerability of Aircraft C06-017 Load Alleviation for a Tilt-Rotor pendent Aircraft Approach Design for C06-028 Aircraft Ice Accretion Prediction Aircraft in Airplane Mode Baltimore-Washington International Airport Based on Neural Networks C06-174 Two General Methods for Calculat- C06-121 On the Formulation of Minimum- Redundancy Management ing the Aircraft Equivalent Singly Vulner- State Approximation as a Nonlinear C06-052 Air Data Computation in Fly-By- able Area Optimization Problem Wire Flight-Control Systems 06-239 Principal Component Regression Control System Sensors Robotics for Fitting Wing Weight Data of Subsonic C06-052 Air Data Computation in Fly-By- Transports C06-142 Study of a Multitethered Aerostat Wire Flight-Control Systems System: Experimental Observations and Atmospheric and Space Sciences C06-053 Coated Hot-Film Sensors for Tran- sition Detection in Cruise Flight Model Validation C06-177 New Ground Deicing Hazard Signal Processing Associated with Freezing Drizzle Ingestion Flight Displays by Jet Engines C06-212 Non-Gaussian Analysis of Turbu- C06-185 Icing Encounter Flight Simulator lent Boundary Layer Fluctuating Pressure on CAD/CAM Flight Mechanics Aircraft Skin Panels C06-096 Automated Scheme Adjustment for C06-017 Load Alleviation for a Tilt-Rotor Soft Computing Conceptual Aircraft Design and Optimiza- Aircraft in Airplane Mode tion C06-092 Analysis of Human Pilot Control C06-072 Transonic Free-To-Roll Analysis of the F-35 (Joint Strike Fighter) Aircraft Inputs Using Neural Network Environmental Effects C06-169 Effect of Propeller Torque on Structural Control C06-177 New Ground Deicing Hazard Minimum-Control Airspeed C06-017 Load Alleviation for a Tilt-Rotor Associated with Freezing Drizzle Ingestion C06-149 Preliminary Parametric Study of Aircraft in Airplane Mode by Jet Engines Gurney Flap Dependencies C06-081 Probabilistic Two-Phase Aircraft C06-008 Aircraft Acceleration Prediction System Identification Wake-Vortex Model: Further Development Due to Atmospheric Disturbances with C06-219 Data Analysis of Phoenix Reusable and Assessment Flight Data Validation Launch Vehicle Demonstrator Flight Test Human Factors Handling Qualities Trajectory Optimization C06-238 Effect of Simulator Motion on Pilot C06-238 Effect of Simulator Motion on Pilot C06-114 Optimization of Flexible Approach Behavior and Perception Behavior and Perception Trajectories Using a Genetic Algorithm C06-166 Human—Computer Interaction C06-054 Free-to-Roll Investigation of the C06-210 Trajectory Management Concepts Analysis of Flight Management System Preproduction F/A-18E Powered-Approach For Future Small Aircraft Transportation Messages Wing Drop Systems C06-171 Proposed Methodology for the Use of Computer Simulation to Enhance Aircraft information Processing UAVs Evacuation Certification C06-208 Flight Segment identification as a C06-150 Preliminary Flight Tests of aH inge- C06-154 Aircraft Accident Statistics and Basis for Pilot Advisory Systems Less Roll Control Effecter Knowledge Database: Analyzing Passenger C06-037 Multidisciplinary Approach to In- Intelligent Control Behavior in Aviation Accidents telligent Unmanned-Airborne- Vehicles C06-025 Progressive Certification Process C06-092 Analysis of Human Pilot Control Mission Planning Based on Living Systems Architecture Inputs Using Neural Network Using Learning Capable Controllers Lasers and Laser Applications INTERDISCIPLINARY TOPICS C06-010 Flight Envelope Expansion in C06-071 Aero-Optic Performance of an Landing Phase Using Classic, Intelligent Aerospace Technology Utilization Aircraft Forward-Facing Optical Turret and Adaptive Controllers C06-030 Integrated Multidisciplinary Top- C06-125 Hysteresis and Broad Flow Features Missile Guidance and Control ology Optimization Approach to Adaptive on a Swept Wing at High Lift C06-156 Computational Investigation and Wing Design Multidisciplinary Design Optimization Design Optimization of a _Lateral-Jet- Analytical and Numerical Methods C06-115 Methodology for Performance Controlled Missile C06-030 Integrated Multidisciplinary Top- Analysis of Aerospace Vehicles Using the Navigation ology Optimization Approach to Adaptive Laws of Thermodynamics C06-093 Monitoring Global Positioning Wing Design C06-020 Structural Design Process Improve- System Satellite Orbit Errors for Aircraft C06-234 Simulation of the Electroimpulse ment Using Evolutionary Finite Element Landing Systems De-Icing Process of Aircraft Wings Models 1968 J. AIRCRAFT, VOL. 43, NO. 6: 2006 INDEX C06-029 Multidisciplinary Design Optimi- C06-171 Proposed Methodology for the Use Gas Turbine Engines zation for Aeromechanics and Handling of Computer Simulation to Enhance Aircraft C06-163 Decision Support Approach to Fleet Qualities Evacuation Certification Maintenance Requirements in the Aviation C06-144 Robust Drag Minimization of C06-028 Aircraft Ice Accretion Prediction Industry Aerodynamic Wings in Engineering Envi- Based on Neural Networks Wind Power ronment C06-143 Solving the Combinatorial Explo- C06-127 Prognostics and Health Manage- sion Problem When Calculating the Multi- C06-129 Viscous-Inviscid Method for Air- ment as Design Variable in Air-Vehicle ple-Hit Vulnerability of Aircraft foil Analysis and Design for Aviation and Conceptual Design C06-136 Aircraft Vulnerable-Area Decom- Windmills 06-031 Numerical Method for Cost-Weight position Method in the Overlapping Region REAL-TIME SYSTEMS Optimization of Stringer-Skin Panels of Components C06-240 Multidisciplinary Optimization Robotic Systems Sensor Systems Framework for Control-Configuration In- C06-035 Challenges Facing Future Micro- tegration in Aircraft Conceptual Design C06-052 Air Data Computation in Fly-By- Air-Vehicle Development C06-184 Sensitivities and Approximations Wire Flight-Control Systems for Aeroservoelastic Shape Optimization Signal Processing with Gust Response Constraints LAUNCH VEHICLE AND C06-231 Frequency Response Model for C€06-096 Automated Scheme Adjustment for MISSILE (LV/M) TECHNOLOGY Branched Pneumatic Sensing Systems Conceptual Aircraft Design and Optimiza- tion Aerodynamics SPACE TECHNOLOGY C06-018 Induced Drag Reduction Using C06-156 Computational Investigation and Global Positioning System Aeroelastic Tailoring with Adaptive Control Design Optimization of a Lateral-Jet- Surfaces C06-093 Monitoring Global Positioning Controlled Missile System Satellite Orbit Errors for Aircraft C06-055 Unsteady-Aerodynamic Shape C06-219 Data Analysis of Phoenix Reusable Sensitivities for Airplane Aeroservoelastic Landing Systems Launch Vehicle Demonstrator Flight Test Configuration Optimization C06-192 Drag Reduction by Controlled Base STRUCTURAL MECHANICS C06-211 Optimal Scheduling of Control Surfaces on a Flexible Wing to Reduce Flow Separation. AND MATERIALS Induced Drag Launch Vehicle and Sounding Rocket Aeroelasticity and Control C06-187 Bréguet Range Equation? Systems C06-076 Bifurcation Analysis of Airfoil in C06-148 Aeroservoelastic Modeling and C06-068 Flight Testing of a New Earth-to- Subsonic Flow with Coupled Cubic Restor- Sensitivity Analysis with Strain Actuators Orbit Air Launch Method ing Forces C06-161 Optimal Conceptual Design of Aircraft Fuel Transfer Systems Testing, Flight and Ground C06-106 Static/Dynamic Correction Ap- proach for Reduced-Order Modeling of C06-111 Value-Based Multidisciplinary Op- C06-068 Flight Testing of a New Earth-to- Unsteady Aerodynamics timization for Commercial Aircraft Design Orbit Air Launch Method C06-088 Unified Aeroelastic and Flight and Business Risk Assessment Dynamic Formulation via Rational Function C06-021 Design-Oriented Structural Model PROPULSION Approximations Order Reduction for Strain-Actuated Flight C06-204 Kiissner’s Function in the Sharp Vehicle Structures Airbreathing Propulsion Edged Gust Problem—A Correction C06-095 Multi-Objective and Multidiscipli- C06-146 Numerical Investigation of Flow in C06-059 Response of Damaged and Un- nary Design Optimization of Supersonic an Overexpanded Nozzle with Porous damaged Tailored Extension-Shear- Fighter Wing Surfaces Coupled Composite Panels C06-030 Integrated Multidisciplinary Top- C06-217 Fan Noise Reduction with In- C06-021 Design-Oriented Structural Model ology Optimization Approach to Adaptive creased Bypass Nozzle Area Order Reduction for Strain-Actuated Flight Wing Design C06-128 High-Lift Propulsive Airfoil with Vehicle Structures C06-179 Joined-Wing Sensor-Craft Confi- Integrated Crossflow Fan C06-086 Flutter of High-Speed Civil Trans- guration Design C06-188 Experimental Investigation on port Flexible Semispan Model: Time Reliability, Maintainability, and Logistics Forced Boundary-Layer Transition of Frequency Analysis Support Axisymmetric Inlet and Numerical Verifi- C06-225 Flight Dynamics of Highly Flexible C06-163 Decision Support Approach to Fleet cation Flying Wings Maintenance Requirements in the Aviation C06-102 Mathematical Modeling for Modal Electric Propulsion Industry Computations Concerning a Morphable C06-061 Failure-Rate Prediction for De C06-181 Conceptual Design and Simulation Wing Havilland Dash-8 Tires Employing Neural- of a Smal! Hybrid-Electric Unmanned Aerial C06-148 Aeroservoelastic Modeling and Network Technique Vehicle Sensitivity Analysis with Strain Actuators Research Facilities and Instrumentation Engine Materials Dynamic Model Analysis C06-103 Sting Deflection Model for Auto- C06-218 Simulation of Soft Projectiles C06-234 Simulation of the Electroimpulse matic Image Registration in Wind-Tunnel Impacting Composite Targets using an De-Icing Process of Aircraft Wings Testing. Arbitrary Lagrangian-Eulerian Formulation C06-142 Study of a Multitethered Aerostat System: Experimental Observations and Safety Engine Performance Model Validation C06-024 Evaluation of Takeoff Performance C06-177 New Ground Deicing Hazard C06-109 Development and Experimental Monitoring Algorithm in Large Jet Trans- Associated with Freezing Drizzle Ingestion Validation of a Shipboard Helicopter On- port Operations by Jet Engines Deck Maneuvering Simulation