JOURNAL OF AIRCRAFT Vol. 47, No. 6, November—December 2009 2010 Journal of Aircraft Index How to Use the Index In the Subject Index, pages 2188-2196, each technicai 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 2197-2199, lists all authors associated with a given technical paper. The locating numbers are identical to those in the Subject Index. The Chronological Index, pages 2200-2207, 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 2010, 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, C10-057 Nonlinear-Aerodynamics/Nonlinear- C10-040 Effects of Local Flow Variations on CONVENTIONAL, STOL/VTOL Structure Interaction Methodology for a High- Landing Gear Noise Prediction and Analysis Altitude Long-Endurance Wing C10-204 Inverse Aerodynamic Design Procedure Aerodynamics C10-042 Interaction of Synthetic Jet with for Propellers Having a Prescribed Chord-Length C09-162E Erratum on Drag Extrapolation to Boundary Layer Using Microscopic Particle Distribution Higher Reynolds Number Image Velocimetry C10-234 Minimizing Induced Drag with Span- C10-186 Influence of Differential Spoiler Settings C10-031 Bat-Inspired Wing Aerodynamics and wise Blowing Variation on Circulation-Controlled on the Wake Vortex Characterization and Optimization Wing Alleviation C10-027 Advanced Experimental and Numerical C10-221 Examination of Rotor Loads due to On- 10-187 Evaluation of a Potential Flow Model for Validation and Analysis of Propeller Slipstream Blade Active Controls for Performance Enhance- Propeller and Wind Turbine Design Flows ment C10-184 Airfoil Optimization Using Practical C10-116 Investigation into the Aerodynamic C10-136 FENSAP-ICE: Analytical Model for Aerodynamic Design Requiremerts Performance of the Tiltrotor Unmanned Aerial Spatial and Temporal Evolution of In-Flight Icing C10-161 Experimental Investigations on Aerody- Vehicle Proprotor Roughness namic Characteristics of the ZHITYUAN-1 Airship C10-100 Stability of Hybrid-Wing-Body-Type C10-085 Hybrid Reynolds-Average Navier— C10-157 Bodies Having Minimum Pressure Drag Aircraft with Centerbody Leading-Edge Carving Stokes and Kinetic Eddy Simulation of External in Supersonic Flow: Investigating Nonlinear C10-096 Modeling and Testing of a Morphing and Internal Flows Effects Wing in Open-Loop Architecture C10-164 Joined-Wing Wind-Tunnel Test for C10-153 Experimental Investigation of Double- C10-037 Lift Enhancement at Low Reynolds Longitudinal Control via Aftwing Twist Hinged Vortex Flap Configurations Numbers Using Self-Activated Movable Flaps C10-064 Prediction of Ballistic Separation Effect C10-120 Improving the Aerodynamic Perform- C10-076 Experimental Studies on Transitional by Direct Calculation of Incremental Coefficients ance of Micro-Air-Vehicle-Scale Cycloidal Rotor: and Closed Cavity Configurations Including Flow C10-142 Computation of Flow over a High- An Experimental Approach Control Performance Parafoil Canopy C10-121 Laminar Airfoil Modification Attaining C10-113 Preliminary Experimental Investigation C10-084 Identification and Attenuation of a Optimum Drag Reduction by Use of Airfoil of a Morphable Biplane: The X-Wing Tonal-Noise Source on an Aircraft’s Landing Gear Morphing C10-044 Numerical Study of Flow Past a Circular C10-061 Optimization of Active Flow Control C€10-065 Adjoint-Based Design of Rotors in a Cylinder Using Hybrid Turbulence Formulations over an Airfoil Using a Surrogate-Management Noninertial Reference Frame C10-043 Modeling, Simulation, and Flight Tests Framework C10-051 Aerodynamic-Structural Design Studies for a T-38 Talon with Wing Fences C10-073 Numerical Investigation of Wind-Tun- of Low-Sweep Transonic Wings C10-032 Fast Large-Eddy Simulation of Low nel Model Deformations Caused by the Twin- C10-129 Rapid Estimation of Impaired-Aircraft Reynolds Number Flows over a NACA0025 Sting Support System Aerodynamic Parameters C10-098 Computational Investigation of Micro- C10-125 Numerical Simulation of Rotor Using C10-102 Aerodynamic Performance of the Three- scale Coaxial-Rotor Aerodynamics in Hover Coupled Computational Fluid Dynamics and Free Dimensional Lifting Supersonic Biplane C10-144 Full-Configuration Drag Estimation Wake C10-067 Aircraft Vortex Wake and Flight Safety C10-155 Quick Access Recorder Data Analysis C10-068 Gurney Flaps on Slender and Nons- Problems Software for Windshear and Turbulence Studies lender Delta Wings C10-078 Effect of Captive Stores on Internal C10-143 Real Time Morphing Wing Optimiza- C10-139 Closed-Loop Control Validation of a Weapons Bay Floor Pressure Distributions tion Validation Using Wind-Tunnel Tests Morphing Wing Using Wind Tunnel Tests C10-035 Effect of a Perturbed Shear Layer on C10-054 Multidisciplinary Considerations in the C10-107 Influence of Wing Configurations on Cavity Resonance Design of Wings and Wing Tip Devices Aerodynamic Characteristics of Wings in Ground C10-048 Aeroelastic Behavior of Flat Plates C10-038 Almost 40 Years of Airframe Noise Effect Moving Near the Ground Research: What Did We Achieve? C10-001 Fuzzy Logic Method Use in F/A-18 C10-075 Determining Direction for Optimization C10-236 Comparison of Potential Flow-Based Aircraft Model Identification of Movable Wing Tip Strake P and Measured Pressure Distributions over Up- C10-060 Effects of Unsteady Trailing-Edge C10-036 Drag Force Balance of a Blunt and wind Sails Blowing on Delta Wing Aerodynamics Divergent Trailing-Edge Airfoil C10-019 Toward Real-Time Aero-Icing Simula- C10-097 Aerodynamic Simulation of Runback C10-112 Supercruise Aircraft Range tion of Complete Aircraft via FENSAP-ICE Ice Accretion 2188 JOURNAL OF AIRCRAFT Vol. 47, No. 6, November—December 2009 2010 Journal of Aircraft Index How to Use the Index In the Subject Index, pages 2188-2196, each technicai 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 2197-2199, lists all authors associated with a given technical paper. The locating numbers are identical to those in the Subject Index. The Chronological Index, pages 2200-2207, 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 2010, 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, C10-057 Nonlinear-Aerodynamics/Nonlinear- C10-040 Effects of Local Flow Variations on CONVENTIONAL, STOL/VTOL Structure Interaction Methodology for a High- Landing Gear Noise Prediction and Analysis Altitude Long-Endurance Wing C10-204 Inverse Aerodynamic Design Procedure Aerodynamics C10-042 Interaction of Synthetic Jet with for Propellers Having a Prescribed Chord-Length C09-162E Erratum on Drag Extrapolation to Boundary Layer Using Microscopic Particle Distribution Higher Reynolds Number Image Velocimetry C10-234 Minimizing Induced Drag with Span- C10-186 Influence of Differential Spoiler Settings C10-031 Bat-Inspired Wing Aerodynamics and wise Blowing Variation on Circulation-Controlled on the Wake Vortex Characterization and Optimization Wing Alleviation C10-027 Advanced Experimental and Numerical C10-221 Examination of Rotor Loads due to On- 10-187 Evaluation of a Potential Flow Model for Validation and Analysis of Propeller Slipstream Blade Active Controls for Performance Enhance- Propeller and Wind Turbine Design Flows ment C10-184 Airfoil Optimization Using Practical C10-116 Investigation into the Aerodynamic C10-136 FENSAP-ICE: Analytical Model for Aerodynamic Design Requiremerts Performance of the Tiltrotor Unmanned Aerial Spatial and Temporal Evolution of In-Flight Icing C10-161 Experimental Investigations on Aerody- Vehicle Proprotor Roughness namic Characteristics of the ZHITYUAN-1 Airship C10-100 Stability of Hybrid-Wing-Body-Type C10-085 Hybrid Reynolds-Average Navier— C10-157 Bodies Having Minimum Pressure Drag Aircraft with Centerbody Leading-Edge Carving Stokes and Kinetic Eddy Simulation of External in Supersonic Flow: Investigating Nonlinear C10-096 Modeling and Testing of a Morphing and Internal Flows Effects Wing in Open-Loop Architecture C10-164 Joined-Wing Wind-Tunnel Test for C10-153 Experimental Investigation of Double- C10-037 Lift Enhancement at Low Reynolds Longitudinal Control via Aftwing Twist Hinged Vortex Flap Configurations Numbers Using Self-Activated Movable Flaps C10-064 Prediction of Ballistic Separation Effect C10-120 Improving the Aerodynamic Perform- C10-076 Experimental Studies on Transitional by Direct Calculation of Incremental Coefficients ance of Micro-Air-Vehicle-Scale Cycloidal Rotor: and Closed Cavity Configurations Including Flow C10-142 Computation of Flow over a High- An Experimental Approach Control Performance Parafoil Canopy C10-121 Laminar Airfoil Modification Attaining C10-113 Preliminary Experimental Investigation C10-084 Identification and Attenuation of a Optimum Drag Reduction by Use of Airfoil of a Morphable Biplane: The X-Wing Tonal-Noise Source on an Aircraft’s Landing Gear Morphing C10-044 Numerical Study of Flow Past a Circular C10-061 Optimization of Active Flow Control C€10-065 Adjoint-Based Design of Rotors in a Cylinder Using Hybrid Turbulence Formulations over an Airfoil Using a Surrogate-Management Noninertial Reference Frame C10-043 Modeling, Simulation, and Flight Tests Framework C10-051 Aerodynamic-Structural Design Studies for a T-38 Talon with Wing Fences C10-073 Numerical Investigation of Wind-Tun- of Low-Sweep Transonic Wings C10-032 Fast Large-Eddy Simulation of Low nel Model Deformations Caused by the Twin- C10-129 Rapid Estimation of Impaired-Aircraft Reynolds Number Flows over a NACA0025 Sting Support System Aerodynamic Parameters C10-098 Computational Investigation of Micro- C10-125 Numerical Simulation of Rotor Using C10-102 Aerodynamic Performance of the Three- scale Coaxial-Rotor Aerodynamics in Hover Coupled Computational Fluid Dynamics and Free Dimensional Lifting Supersonic Biplane C10-144 Full-Configuration Drag Estimation Wake C10-067 Aircraft Vortex Wake and Flight Safety C10-155 Quick Access Recorder Data Analysis C10-068 Gurney Flaps on Slender and Nons- Problems Software for Windshear and Turbulence Studies lender Delta Wings C10-078 Effect of Captive Stores on Internal C10-143 Real Time Morphing Wing Optimiza- C10-139 Closed-Loop Control Validation of a Weapons Bay Floor Pressure Distributions tion Validation Using Wind-Tunnel Tests Morphing Wing Using Wind Tunnel Tests C10-035 Effect of a Perturbed Shear Layer on C10-054 Multidisciplinary Considerations in the C10-107 Influence of Wing Configurations on Cavity Resonance Design of Wings and Wing Tip Devices Aerodynamic Characteristics of Wings in Ground C10-048 Aeroelastic Behavior of Flat Plates C10-038 Almost 40 Years of Airframe Noise Effect Moving Near the Ground Research: What Did We Achieve? C10-001 Fuzzy Logic Method Use in F/A-18 C10-075 Determining Direction for Optimization C10-236 Comparison of Potential Flow-Based Aircraft Model Identification of Movable Wing Tip Strake P and Measured Pressure Distributions over Up- C10-060 Effects of Unsteady Trailing-Edge C10-036 Drag Force Balance of a Blunt and wind Sails Blowing on Delta Wing Aerodynamics Divergent Trailing-Edge Airfoil C10-019 Toward Real-Time Aero-Icing Simula- C10-097 Aerodynamic Simulation of Runback C10-112 Supercruise Aircraft Range tion of Complete Aircraft via FENSAP-ICE Ice Accretion 2188 J. AIRCRAFT, VOL. 47, NO. 6: 2010 INDEX 2189 C10-045 Computational Fluid Dynamics Valida- C10-072 Transition-Flow-Occurrence Estima- C10-222 Nonlinear Modeling and Aeroelastic tion Study of Wake-Capturing Capability for Flat- tion: A New Method Analysis of an Adaptive Camber Wing Plate Wake C10-151 Numerical Simulation of Rotor-Fuse- C10-152 Vibration Analysis of Elastic Uniform C10-012 Span Efficiencies of Wings at Low lage-Cylinder Interaction in Forward Flight Cantilever Rotor Blades in Unsteady Aerody- Reynolds Numbers C10-122 Propeller Empennage Interaction Ef- namics Modeling C10-083Design fects on the Vertical Tail Design of Multiengine C10-146 Helicopter Rotor Load Prediction Using and Test of the UW-5006 Transonic Natural- Aircraft a Geometrically Exact Beam with Multicompo- Laminar-Flow Wing C10-074 Experimental Investigation of Separa- nent Model C10-011 Patch Assembly: An Automated Over- tion Control Using Upper-Surface Spoilers C10-134 Evaluation of Aeroelastic Uncertainty lapping Grid Assembly Strategy C10-066 Analytical Sensitivity Analysis of an Analysis Methods C10-022 Limits of Continuum Aerodynamics Unsteady Vortex-Lattice Method for Flapping- C10-130 Transonic Aeroelastic Stability Predic- C10-093 Experimental Investigation of a Circu- Wing Optimization tions Under the Influence of Structural Variability lar-Planform Concept Aircraft C10-039 Mean Flowfield Structure of a Super- C10-128 Prediction and Analysis of Main Rotor C10-237 Flow-Separation Lines on Axisymmet- sonic Three-Dimensional Base Flow Loads in a Prescribed Pull-Up Maneuver ric Bodies with Tapered Tails Aerospace Plane C10-024 Effect of High-Fidelity Ice-Accretion Aeroelasticity and Aeroservoelasticity Simulations on Fuil-Scale Airfoil Performance C10-210 Approximate Modeling of Unsteady C10-026 Small Rotor Design Optimization Using C10-135 Incorporation of Feedback Control into Aerodynamics for Hypersonic Aeroelasticity a High-Fidelity Aeroservoelastic Fighter Aircraft Blade Element Momentum Theory and Hover Model Air Transportation Tests C10-233 Decay of Aircraft Wake Vortices Under C10-117 Design Optimization for Improved Soft C10-067 Aircraft Vortex Wake and Flight Safety Daytime Free Convective Conditions In-Plane Tiltrotor Aeroelastic in Airplane Mode Problems C10-238 Wingtip Vortex Simulation by Using C10-057 Nonlinear-Aerodynamics/Nonlinear- C10-175 Potential Effects of Blended Wing Nonequilibrium Eddy Viscosity Model Structure Interaction Methodology for a High- Bodies on the Air Transportation System C10-211 Nature of Wakelike and Jetlike Axial Tip Altitude Long-Endurance Wing C10-232 Gauss Pseudospectral Method for Less C10-048 Aeroelastic Behavior of Flat Plates Noise and Fuel Consumption of Aircraft Vortex Flows Moving Near the Ground Operations C10-214 Small and Micro Aerial Vehicles: How C10-106 Design of an Adaptive Gust Response C10-025 Intelligent Flight-Trajectory Generation Much Span is Teo Much Span? Alleviation Control System: Simulations and to Maximize Safe-Outcome Probability After a C10-215 Prediction of Flow Dynamics over Experiments Distress Event Cavities by Detached Eddy Simulation C10-079 Small Disturbance Navier-Stokes Com- C10-050 Aircraft Decompression with Installed C10-224 Declining Angle Effects of the Trailing putations for Low-Aspect-Ratio Wing Pitching Cockpit Security Door Edge of a Microramp Vortex Generator Oscillations C10-016 Probabilistic Sensitivity-Based Ranking C10-230 Helicopter Tail Rotor Thrust and Main C10-006 Effects of Rolling Maneuver on of Damage Tolerance Analysis Elements Rotor Wake Coupling in Crosswind Flight Divergence and Flutter of Aircraft Wing Store C10-123 Ionospheric Threat Parameterization for C10-197 Experimental Investigation into Articu- C10-034 Efficient Numerical Aeroelastic Analy- Local Area Global-Positioning-System-Based lated Winglet Effects on Flying Wing Surface sis of a High-Aspect-Ratio Wing Considering Aircraft Landing Systems Pressure Aerodynamics Geometric Nonlinearity C10-173 Wind-Optimal Routing in the National C10-185 Stochastic Modeling of Incident Gust C10-090 Computational-Fluid-Dynamics- and Airspace System Effects on Aerodynamic Lift Computational-Structural-Dynamics-Based C10-218 Arrival Time Controllability of Tailored C10-109 Segmented-Freewing Concept for Gust Time-Accurate Aeroelasticity of Helicopter Rotor Arrival Subjected to Flight-Path Constraints Alleviation Blades C10-092 Impact of an Innovative Quiet Regional C10-115 Effect of Jet-Exhaust Streams on C10-103 Reliability-Based Design Optimization Aircraft on the Air Transportation System Structure of Vortex Wakes of Nonlinear Aeroelasticity Problems C10-233 Decay of Aircraft Wake Vortices Under C10-165 Aerostructural Optimization of Non- C10-041 Airborne Lidar for Automatic Feedfor- Daytime Free Convective Conditions planar Lifting Surfaces ward Control of Turbulent In-Flight Phenomena C10-223 Computational-Fiuid-Dynamics-Based C10-049 Multilevel Structural Optimization for Airframe-Propulsion Integration Twist Optimization of Hovering Rotors Preliminary Wing-Box Weight Estimation C10-122 Propeller Empennage Interaction Ef- C10-198 Analysis of Leading-Edge Separation C10-235 Verification of H Flutter Analysis fects on the Vertical Tail Design of Multiengine Bubbles on Rotating Blades C10-138 Experimental Characterization of Limit Aircraft C10-176 Computational Fluid Dynamics Analy- Cycle Oscillations in Membrane Wing Micro Air ses of Flow over Weapons-Bay Geometries Vehicles Airframe-Weapon System Integration C10-201 Flight Control Using Wing-Tip Plasma Ci0-131 Validation Studies for Aeroelastic Trim C10-064 Prediction of Ballistic Separation Effect Actuation and Stability of Highly Flexible Aircraft by Direct Calculation of Incremental Coefficients C10-196 Yaw Control of a Tailless Aircraft C10-169 Nonlinear Aeroelasticity of a Very C10-078 Effect of Captive Stores on Internal Configuration Flexible Blended-Wing-Body Aircraft Weapons Bay Floor Pressure Distributions C10-228 Optimizing Spanwise Lift Distributions C10-005 Parallel Multigrid Algorithm for Aero- Yacht Sails Using Extended Lifting Line Analysis elasticity Simulations Cabin Environment, Crew Training, and C10-159 Induced-Drag Compressibility Correc- C10-139 Closed-Loop Control Validation of a Life Support tion for Three-Dimensional Vortex-Lattice Meth- Morphing Wing Using Wind Tunnel Tests C10-050 Aircraft Decompression with Installed ods C10-210 Approximate Modeling of Unsteady Cockpit Security Door C10-188 Closed-Loop Stall Control System Aerodynamics for Hypersonic Aeroelasticity C10-226 Airfoil Lift Augmentation at Low C10-001 Fuzzy Logic Method Use in F/A-18 Collision Avoidance Reynolds Number Aircraft Model Identification C10-013 Near-Optimal Trajectories to Manage C10-152 Vibration Analysis of Elastic Uniform C10-156 Flutter Analysis: Using Piecewise Landing Sequence in the Vicinity of Controlled Cantilever Rotor Blades in Unsteady Aerody- Quadratic Interpolation with Mode Tracking and Aerodromes namics Modeling Wind-Tunnel Tests C10-127 Effect of Normal Blowing on Compres- C10-216 Load Alleviation on a Joined-Wing Communication and Air Traffic Control sible Convex-Corner Flows Unmanned Aircraft C10-013 Near-Optimal Trajectories to Manage C10-148 Low-Reynolds-Number Airfoil Inves- C10-158 Uncertainty Quantification in Flutter Landing Sequence in the Vicinity of Controlled tigation of Lower-Surface Leading-Edge Flaps Analysis for an Airfoil with Preloaded Freeplay Aerodromes 2190 J. AIRCRAFT, VOL. 47, NO. 6: 2010 INDEX Configuration Design C10-230 Helicopter Tail Rotor Thrust and Main C10-154 Bubble Burst Control Using Smart C10-100 Stability of Hybrid-Wing-Body-Type Rotor Wake Coupling in Crosswind Flight Structure Sensor Actuators for Stall Suppression Aircraft with Centerbody Leading-Edge Carving C10-197 Experimental Investigation into Articu- C10-051 Aerodynamic-Structural Design Studies lated Winglet Effects on Flying Wing Surface General Aviation of Low-Sweep Transonic Wings Pressure Aerodynamics C10-123 Ionospheric Threat Parameterization for C10-175 Potential Effects of Blended Wing C10-195 Analytical Criterion for Aircraft Spin Local Area Global-Positioning-System-Based Bodies on the Air Transportation System Susceptibility Aircraft Landing Systems C10-054 Multidisciplinary Considerations in the C10-109 Segmented-Freewing Concept for Gust C10-190 Autonomous Soaring: The Montague Design of Wings and Wing Tip Devices Alleviation Cross-Country Challenge C10-144 Full-Configuration Drag Estimation C10-182 Theoretical Framework for the Simu- C10-217 Probabilities for Severe and Fatal C10-099 Airframe Design for Silent Fuel- lation of Transport Aircraft Flight Injuries in General Aviation Accidents Efficient Aircraft C10-196 Yaw Control of a Tailless Aircraft C10-056 Flight Determination of Partial-Span- C10-193 Designing for a Green Future: A Unified Configuration Flap Parasite Drag With Flap Deflection Aircraft Design Methodology C10-140 Flight Performance Analysis of Hybrid Ground Effect Machines C10-093 Experimental Investigation of a Circu- Airship: Revised Analytical Formulation lar-Planform Concept Aircraft Flight |O perations C10-107 Influence of Wing Configurations on C10-231 Conceptual Design of an Aerospace C10-086 Modeling Performance and Emissions Aerodynamic Characteristics of Wings in Ground Vehicle Controller Using Axiomatic Theory from Aircraft in the Aviation Integrated Modelling Effect C10-194 Improved Fuel Capacity Estimation Project C10-048 Aeroelastic Behavior of Flat Plates Method C10-182 Theoretical Framework for the Simu- Moving Near the Ground C10-214 Small and Micro Aerial Vehicles: How lation of Transport Aircraft Flight Ground Support Much Span is Too Much Span? C10-232 Gauss Pseudospectral Method for Less C10-191 Helicopter Rotor Shape Optimization Noise and Fuel Consumption of Aircraft C10-218 Arrival Time Controllability of Tailored for the Improvement of Aeroacoustic Performance Operations Arrival Subjected to Flight-Path Constraints in Hover C10-013 Near-Optimal Trajectories to Manage C10-177 Feasibility Study of Global-Positioning- C10-092 Impact of an Innovative Quiet Regional Landing Sequence in the Vicinity of Controlled System-Based Aircraft-Carrier Flight-Deck Per- Aircraft on the Air Transportation System Aerodromes sistent Monitoring System C10-167 Parametric Study for Hovering Perform- Lighter-Than-Air Systems ance of a Coaxial Rotor Unmanned Aerial Vehicle Flow Control C10-208 Design Optimization of a Truss-Braced- C10-168 Dynamic Stability Analysis of a Wing Transonic Transport Aircraft C10-186 Influence of Differential Spoiler Settings Tethered Aerostat C€10-070 Tool Development for Low-Noise Air- on the Wake Vortex Characterization and C10-114 Multidisciplinary Shape Optimization craft Design Alleviation of Aerostat Envelopes C10-063 Optimal Sizing and Cruise Speed C10-042 Interaction of Synthetic Jet with C10-140 Flight Performance Analysis of Hybrid Determination for a Solar-Powered Airplane Boundary Layer Using Microscopic Particle Airship: Revised Analytical Formulation C10-109 Segmented-Freewing Concept for Gust Image Velocimetry C10-089 Exploring the Stability Landscape of Alleviation C10-091 Roll Contrial via Active Flow Control: Constant-Stress Pumpkin Balloon Designs Economics From Concept to Flight C10-141 Effective Approach to Characterization C10-193 Designing for a Green Future: A Unified C10-121 Laminar Airfoil Modification Attaining of Prediction Errors for Balloon Ascent Aircraft Design Methodology Optimum Drag Reduction by Use of Airfoil Trajectories Morphing C10-173 Wind-Optimal Routing in the National C10-037 Lift Enhancement at Low Reynolds Manufacturing Airspace System Flight Control Integration Numbers Using Self-Activated Movable Flaps C10-172 Yield Strength and Residual Stress C10-143 Real Time Morphing Wing Optimiza- C10-076 Experimental Studies on Transitional Measurements on Friction-Stir-Welded Alumi- tion Validation Using Wind-Tunnel Tests and Closed Cavity Configurations Including Flow num Alloys C10-094 Propulsion and Flight Controls Integra- Control C10-229 Integration of Three-Dimensional Print- tion for a Blended-Wing-Body Transport Aircraft C10-096 Modeling and Testing of a Morphing ing Technology for Wind-Tunnel Model Fab- Wing in Open-Loop Architecture rication C10-202 Integrated Framework for Artificial Immunity-Based Aircraft Failure Detection, C10-084 Identification and Attenuation of a C10-030 Use of Digital Manufacturing to Identification, and Evaluation Tonal-Noise Source on an Aircraft’s Landing Gear Improve Management Learning in Aerospace C10-139 Closed-Loop Control Validation of a C10-234 Mirimizing Induced Drag with Span- Assembly wise Blowin Variation on Circulation-Controlled Morphing Wing Using Wind Tunnel Tests Wing Micro Air Vehicles C10-077 Development and Conversion Flight Test of a Small Tiltrotor Unmanned Aerial Vehicle C10-213 Active Flow Control Systems Architec- C10-031 Bat-Inspired Wing Aerodynamics and tures for Civil Transport Aircraft Optimization C10-023 Numerical Study of Suction-Blowing C10-120 Improving the Aerodynamic Perform- Flight Mechanics Flow Control Technology for an Airfoil ance of Micro-Air-Vehicle-Scale Cycloidal Rotor: C10-091 Roll Contrial via Active Flow Control: C10-212 Particle Swarm Optimization of Suction An Experimental Approach From Concept to Flight and Blowing on an Airfoils at Transonic Speeds C10-008 Characteristics of Pitching and Plunging C10-021_ Comparison of Two Kite Force Models C10-061 Optimization of Active Flow Control Airfoils Under Dynamic-Stall Conditions with Experiment over an Airfoil Using a Surrogate-Management C10-037 Lift Enhancement at Low Reynolds C10-110 Optimization of Hover-to-Cruise Tran- Framework Numbers Using Self-Activated Movable Flaps sition Maneuver Using Variable-Incidence Wing C10-188 Closed-Loop Stall Control System C10-113 Preliminary Experimental Investigation C10-058 Characterizing Wing Rock with Varia- C10-218 Arrival Time Controllability of Tailored of a Morphable Biplane: The X-Wing tions in Size and Configuration of Vertical Tail Arrival Subjected to Flight-Path Constraints C10-062 Planform and Camber Effects on the C10-168 Dynamic Stability Analysis of a C10-201 Flight Control Using Wing-Tip Plasma Aerodynamics of Low-Reynolds-Number Wings Tethered Aerostat Actuation C10-098 Computational Investigation of Micro- Ci0-012 Span Efficiencies of Wings at Low C10-074 Experimental Investigation of Separa- scale Coaxial-Rotor Aerodynamics in Hover Reynolds Numbers tion Control Using Upper-Surface Spoilers C10-055 Panel-Method-Based Path Planning and C10-126 Flight “Vest of Stable Automated Cruise C10-072 Transition-Flow-Occurrence __Estima- Collaborative Target Tracking for Swarming Flap for an Adaptive Wing Aircraft tion: A New Method Micro Air Vehicles J. AIRCRAFT, VOL. 47, NO. 6: 2010 INDEX 2191 C10-026 Small Rotor Design Optimization Using C10-024 Effect of High-Fidelity Ice-Accretion C10-230 Helicopter Tail Rotor Thrust and Main Blade Element Momentum Theory and Hover Simulations on Full-Scale Airfoil Performance Rotor Wake Coupling in Crosswind Flight Tests C10-056 Flight Determination of Partial-Span- C10-004 Helicopter Thickness Noise Reduction C10-012 Span Efficiencies of Wings at Low Flap Parasite Drag With Flap Deflection Possibilities Through Active On-Blade Acoustic Reynolds Numbers C10-020 Current Methods Modeling and Simu- Control C10-137 Pitch and Heave Control of Robotic lating Icing Effects on Aircraft Performance, C10-128 Prediction and Analysis of Main Rotor Samara Micro Air Vehicles Stability, Control Loads in a Prescribed Pull-Up Maneuver C10-226 Airfoil Lift Augmentation at Low C10-148 Low-Reynolds-Number Airfoil Inves- C10-151 Numerical Simulation of Rotor-Fuse- Reynolds Number tigation of Lower-Surface Leading-Edge Flaps lage-Cylinder Interaction in Forward Flight C10-105 Unsteady Lift Generation on Rotating C10-182 Theoretical Framework for the Simu- Wings at Low Reynolds Numbers lation of Transport Aircraft Flight Safety C10-214 Small and Micro Aerial Vehicles: How C10-217 Probabilities for Severe and Fatal Much Span is Too Much Span? Propeller and Rotor Systems Injuries in General Aviation Accidents C10-066 Analytical Sensitivity Analysis of an C10-024 Effect of High-Fidelity Ice-Accretion C10-116 Investigation into the Aerodynamic Unsteady Vortex-Lattice Method for Flapping- Simulations on Full-Scale Airfoil Performance Performance of the Tiltrotor Unmanned Aerial Wing Optimization C10-050 Aircraft Decompression with Installed Vehicle Proprotor C10-148 Low-Reynolds-Number Airfoil Inves- Cockpit Security Door C10-027 Advanced Experimental and Numerical tigation of Lower-Surface Leading-Edge Flaps C10-134 Evaluation of Aeroelastic Uncertainty Validation and Analysis of Propeller Slipstream C10-206 Lift Enhancement of Flapping Airfoils Analysis Methods Flows by Generalized Pitching Motion C10-104 Damage of Carbon/Epoxy Composite C10-187 Evaluation of a Potential Flow Model for Plates Subjected to Mechanical Impact and Military Missions Propeller and Wind Turbine Design Simulated Lightning C10-204 Inverse Aerodynamic Design Procedure C10-177 Feasibility Study of Global-Positioning- C10-115 Effect of Jet-Exhaust Streams on for Propellers Having a Prescribed Chord-Length System-Based Aircraft-Carrier Flight-Deck Per- Structure of Vortex Wakes Distribution sistent Monitoring System C10-088 Tonal and Broadband Noise Calcula- Simulation Noise tions for Aeroacoustic Optimization of a Pusher C10-071 Computational Workflow Management Propeller C10-038 Almost 40 Years of Airframe Noise for Conceptual Design of Complex Systems C10-122 Propeller Empennage Interaction Ef- Research: What Did We Achieve? C10-086 Modeling Performance and Emissions fects on the Vertical Tail Design of Multiengine C10-175 Potential Effects of Blended Wing from Aircraft in the Aviation Integrated Modelling Aircraft Bodies on the Air Transportation System Project C10-084 Identification and Attenuation of a C10-170 Modeling of Pilot Landing Approach Tonal-Noise Source on an Aircraft’s Landing Gear Rotorcraft Control Using Stochastic Switched Linear C10-232 Gauss Pseudospectral Method for Less C10-117 Design Optimization for Improved Soft Regression Model Noise and Fuel Consumption of Aircraft In-Plane Tiltrotor Aeroelastic in Airplane Mode C10-069 Optimizing the Performance of the Pilot Operations C10-187 Evaluation of a Potential Flow Model for Control Loaders at NASA Vertical Motion C10-040 Effects of Local Flow Variations on Propeller and Wind Turbine Design Simulator Landing Gear Noise Prediction and Analysis C10-065 Adjoint-Based Design of Rotors in a C10-132 Application of Bifurcation Methods to C10-080 Computational-Fluid-Dynamics-Based Noninertial Reference Frame the Prediction of Low-Speed Aircraft Ground Clean-Wing Aerodynamic Noise Model for C10-101 Hybrid Navier—Stokes/Free-Wake Performance Design Method for Modeling Blade-Vortex Interactions C10-030 Use of Digital Manufacturing to C10-119 Frequency Selection Mechanism of C10-120 Improving the Aerodynamic Perform- Improve Management Learning in Aerospace Airfoil Trailing-Edge Noise ance of Micro-Air-Vehicle-Scale Cycloidal Rotor: Assembly C10-191 Helicopter Rotor Shape Optimization An Experimental Approach C10-128 Prediction and Analysis of Main Rotor for the Improvement of Aeroacoustic Performance C10-221 Examination of Rotor Loads due to On- Loads in a Prescribed Pull-Up Maneuver in Hover Blade Active Controls for Performance Enhance- C10-199 Coaxial Rotor Helicopter in Hover C10-004 Helicopter Thickness Noise Reduction ment B.sed on Unstructured Dynamic Overset Grids Possibilities Through Active On-Blade Acoustic C10-090 Computational-Fluid-Dynamics- and C10-171 Tandem Helicopter Trim and Flight Control Computational-Structural-Dynamics-Based Characteristics in the Icing Condition C10-070 Tool Development for Low-Noise Air- Time-Accurate Aeroelasticity of Helicopter Rotor craft Design Blades Stealth C10-081 Framework for a Landing-Gear Model C10-033 Bistable Composite Flap for an Airfoil C10-091 Roll Contrial via Active Flow Control: and Acoustic Prediction C10-015 Effect of Uncertainty on Hub Vibration From Concept to Flight Response of Composite Helicopter Rotor Blades Performance C10-077 Development and Conversion Flight STOL/VTOL/STOVL C10-144 Full-Configuration Drag Estimation Test of a Small Tiltrotor Unmanned Aerial Vehicle C10-117 Design Optimization for Improved Soft C10-095 Characterization of Aerospace Vehicle C10-137 Pitch and Heave Control of Robotic In-Plane Tiltrotor Aeroelastic in Airplane Mode Performance and Mission Analysis Using Samara Micro Air Vehicles C10-179 Ground Resonance Analysis for an Thermodynamic Availability C10-191 Helicopter Rotor Shape Optimization Eight-Degrees-of-Freedom Rotorcraft with Dou- C10-086 Modeling Performance and Emissions for the Improvement of Aeroacoustic Performance ble-Stage Oleo-Pneumatic Shock Absorbers from Aircraft in the Aviation Integrated Modelling in Hover C10-171 Tandem Helicopter Trim and Flight Project C10-026 Small Rotor Design Optimization Using Characteristics in the Icing Condition C10-097 Aerodynamic Simulation of Runback Blade Element Momentum Theory and Hover C10-029 Novel, Bidirectional, Variable-Camber Ice Accretion Tests Airfoil via Macro-Fiber Composite Actuators C10-126 Flight Test of Stable Automated Cruise C10-007 Prediction of Tiltrotor Vibratory Loads C10-234 Minimizing Induced Drag with Span- Flap for an Adaptive Wing Aircraft with Inclusion of Wing-Proprotor Aerodynamic wise Blowing Variation on Circulation-Controlled C10-221 Examination of Rotor Loads due to On- Interaction Wing Blade Active Controls for Performance Enhance- C10-223 Computational-Fluid-Dynamics-Based ment Twist Optimization of Hovering Rotors Structural Design (Including Loads) C10-192 Inlet Stagnation Pressure Loss Estimate C10-167 Parametric Study for Hovering Perform- C10-207 Optimal Design of Unitized Structures for a Simplified Thrust Model ance of a Coaxial Rotor Unmanned Aerial Vehicle Using Response Surface Approaches 2192 J. AIRCRAFT, VOL. 47, NO. 6: 2010 INDEX C10-103 Reliability-Based Design Optimization C10-147 Three-Dimensional Curvature-Con- C10-020 Current Methods Modeling and Simu- of Nonlinear Aeroelasticity Problems strained Trajectory Planning Based on In-Flight lating Icing Effects on Aircraft Performance, C10-009 Bifurcation Analysis of Nose-Landing- Waypoints Stability, Control Gear Shimmy with Lateral and Longitudinal C10-077 Development and Conversion Flight C10-136 FENSAP-ICE: Analytical Model for Bending Test of a Small Tiltrotor Unmanned Aerial Vehicle Spatial and Temporal Evolution of In-Flight Icing C10-046 Mechanism for Warp-Controlled Twist C10-169 Nonlinear Aeroelasticity of a Very Roughness of a Morphing Wing Flexible Blended-Wing-Body Aircraft COMPUTING, INFORMATION, C10-164 Joined-Wing Wind-Tunrel Test for C10-110 Optimization of Hover-to-Cruise Tran- AND COMMUNICATION Longitudinal Control via Aftwing Twist sition Maneuver Using Variable-Incidence Wing C10-180 Optimization and Postbuckling Analy- C10-029 Novel, Bidirectional, Variable-Camber Aerospace Electronics sis of Curvilinear-Stiffened Panels Under Multi- Airfoil via Macro-Fiber Composite Actuators ple-Load Cases C10-068 Gurney Flaps on Slender and Nons- C10-108 Fusion of Smart-Sensor Standards and C10-216 Load Alleviation on a Joined-Wing lender Delta Wings Sensors with Self-Validating Abilities Unmanned Aircraft C10-216 Load Alleviation on a Joined-Wing Artificial Intelligence Systems C10-016 Probabilistic Sensitivity-Based Ranking Unmanned Aircraft C10-225 Feasibility Demonstration of Diagnostic of Damage Tolerance Analysis Elements C10-002 Neural-Network-Based Flush Air Data Decision Tree for Validating Aircraft Navigation Sensing System Demonstrated on a Mini Air System Accuracy Structural Materials Vehicle C16-071 Computational Workflow Management C10-149 Lifetime Assessment of Aircraft Struc- C10-017 Videogrammetry Dynamics Measure- for Conceptual Design of Complex Systems tural Components in Coastal Environments ments of a Lightweight Flexible Wing in a Wind Autonomous Systems C10-227 Air-Vessel Corrosion Damage Distribu- Tunnel tion and Reliability Modeling C10-063 Optimal Sizing and Cruise Speed C10-177 Feasibility Study of Global-Positioning- C10-172 Yield Strength and Residual Stress Determination for a Solar-Powered Airplane System-Based Aircraft-Carrier Flight-Deck Per- Measurements on Friction-Stir-Welded Alumi- C10-167 Parametric Study for Hovering Perform- sistent Monitoring System num Alloys ance of a Coaxial Rotor Unmanned Aerial Vehicle Controls and Displays C10-190 Autonomous Soaring: The Montague C10-225 Feasibility Demonstration of Diagnostic System Effectiveness Cross-Country Challenge Decision Tree for Validating Aircraft Navigation C10-i12 Supercruise Aircraft Range C10-226 Airfoil Lift Augmentation at Low System Accuracy Reynolds Number Testing, Flight and Ground C10-176 Computational Fluid Dynamics Analy- Distributed Systems and Networking ses of Flow over Weapons-Bay Geometries C09-162E Erratum on Drag Extrapolation to C10-108 Fusion of Smart-Sensor Standards and Higher Reynolds Number C10-074 Experimental Investigation of Separa- Sensors with Self-Validating Abilities tion Control Using Upper-Surface Spoilers C10-043 Modeling, Simulation, and Flight Tests ENERGY C10-166 Using Multiobjective Evolutionary Al- for a T-38 Talon with Wing Fences gorithms and Data-Mining Methods to Optimize C10-116 Investigation into the Aerodynamic Fuel Cells Ornithopters’ Kinematics Performance of the Tiltrotor Unmanned Aerial C10-160 Micro Air Vehicle Trajectory Planning C10-200 First Fuel-Cell Manned Aircraft Vehicle Proprotor C10-096 Modeling and Testing of a Morphing in Winds Hydrogen and Unique Fuels Wing in Open-Loop Architecture C10-200 First Fuel-Cell Manned Aircraft C10-203 Calibration Modeling of Nonmonolithic Vibration Wind Power Wind-Tunnel Force Balances C10-179 Ground Resonance Analysis for an C10-143 Real Time Morphing Wing Optimiza- Eight-Degrees-of-Freedom Rotorcraft with Dou- C10-021 Comparison of Two Kite Force Models tion Validation Using Wind-Tunnel Tests ble-Stage Oleo-Pneumatic Shock Absorbers with Experiment C10-021 Comparison of Two Kite Force Models C10-118 Design Optimization for Minimum C10-032 Fast Large-Eddy Simulation of Low with Experiment Reynolds Number Flows over a NACA0025 Sound Radiation from Point-Excited Curvili- C10-126 Flight Test of Stable Automated Cruise C10-036 Drag Force Balance of a Blunt and Flap for an Adaptive Wing Aircraft nearly Stiffened Panel Divergent Trailing-Edge Airfoil C10-209 Targeted Energy Transfer Between a C10-073 Numerical Investigation of Wind-Tun- Model Flexible Wing and Nonlinear Energy Sink FLIGHT SIMULATOR SYSTEMS nel Model Deformations Caused by the Twin- C10-034 Efficient Numerical Aeroelastic Analy- Sting Support System Guidance, Navigation, and Control sis of a High-Aspect-Ratio Wing Considering C10-164 Joined-Wing Wind-Tunnel Test for Systems Geometric Nonlinearity Longitudinal Control via Aftwing Twist C10-007 Prediction of Tiltrotor Vibratory Loads C10-069 Optimizing the Performance of the Pilot C10-083 Design and Test of the UW-5006 with Inclusion of Wing-Proprotor Aerodynamic Control Loaders at NASA Vertical Motion Transonic Natural-Laminar-Flow Wing Interaction Simulator C10-047 Application of Design of Experiments to C10-015 Effect of Uncertainty on Hub Vibration Flight Test: A Case Study Human-Computer Interactions Response of Composite Helicopter Rotor Blades C10-001 Fuzzy Logic Method Use in F/A-18 C10-220 Perception Coherence Zones in Flight C10-009 Bifurcation Analysis of Nose-Landing- Aircraft Model Identification Simulation Gear Shimmy with Lateral and Longitudinal C10-108 Fusion of Smart-Sensor Standards and Bending Intelligent Systems Sensors with Self-Validating Abilities C10-056 Flight Determination of Partial-Span- C10-025 Intelligent Flight-Trajectory Generation Flap Parasite Drag With Flap Deflection Weather Hazards to Maximize Safe-Outcome Probability After a C10-093 Experimental Investigation of a Circu- C10-155 Quick Access Recorder Data Analysis Distress Event lar-Planform Concept Aircraft Software for Windshear and Turbulence Studies FLUID DYNAMICS C10-003 Longitudinal Handling Quality Analysis Uninhabited and Unmanned Air Vehicles of a Civil Transport Aircraft Encountering Aeroacoustics C10-113 Preliminary Experimental Investigation Turbulence C10-035 Effect of a Perturbed Shear Layer on of a Morphable Biplane: The X-Wing C10-104 Damage of Carbon/Epoxy Composite Cavity Resonance C10-145 Reynolds-Stress Model Flow Prediction Plates Subjected to Mechanical Impact and C10-101 Hybrid Navier—Stokes/Free-Wake in Aircraft-Engine Intake Double-S-Shaped Duct Simulated Lightning Method for Modeling Blade-Vortex Interactions J. AIRCRAFT, VOL. 47, NO. 6: 2010 INDEX C10-038 Almost 40 Years of Airframe Noise C10-085 Hybrid Reynolds-Average Navier— Rarefied Flows Research: What Did We Achieve? Stokes and Kinetic Eddy Simulation of External C10-022 Limits of Continuum Aerodynamics C10-088 Tonal and Broadband Noise Calcula- and Internal Flows Subsonic Flows tions for Aeroacoustic Optimization of a Pusher C10-107 Influence of Wing Configurations on Propeller Aerodynamic Characteristics of Wings in Ground C10-153 Experimental Investigation of Double- C10-099 Airframe Design for Silent Fuel- Effect Hinged Vortex Flap Configurations Efficient Aircraft C10-061 Optimization of Active Flow Control C10-085 Hybrid Reynolds-Average Navier- C10-215 Prediction of Flow Dynamics over over an Airfoil Using a Surrogate-Management Stokes and Kinetic Eddy Simulation of External Cavities by Detached Eddy Simulation Framework and Internal Flows C10-040 Effects of Local Flow Variations on C10-124 In Pursuit of Grid Convergence for Two- C10-008 Characteristics of Pitching and Plunging Landing Gear Noise Prediction and Analysis Dimensional Euler Solutions Airfoils Under Dynamic-Stall Conditions C10-111 Pressure Waves Generated at the C10-011 Patch Assembly: An Automated Over- C10-145 Reynolds-Stress Model Flow Prediction Downstream Corner of a Rectangular Cavity lapping Grid Assembly Strategy in Aircraft-Engine Intake Double-S-Shaped Duct C10-004 Helicopter Thickness Noise Reduction C10-045 Computational Fluid Dynamics Valida- C10-206 Lift Enhancement of Flapping Airfoils Possibilities Through Active On-Blade Acoustic tion Study of Wake-Capturing Capability for Flat- by Generalized Pitching Motion Control Plate Wake C10-198 Analysis of Leading-Edge Separation C10-és: Framework for a Landing-Gear Model C10-083 Design and Test of the UW-5006 Bubbles on Rotating Blades auc Acoustic Prediction Transonic Natural-Laminar-Flow Wing C10-028 Vortex Dynamics of Free-to-Roll Slen- C10-119 Frequency Selection Mechanism of C10-215 Prediction of Flow Dynamics over der and Nonslender Delta Wings Airfoil Trailing-Edge Noise Cavities by Detached Eddy Simulation Shock Waves and Detonations C10-224 Declining Angle Effects of the Trailing Boundary-Layer Stability and Transition Edge of a Microramp Vortex Generator C10-102 Aerodynamic Performance of the Three- C10-121 Laminar Airfoil Modification Attaining C10-014 Computation of Unsteady Low Rey- Dimensional Lifting Supersonic Biplane Optimum Drag Reduction by Use of Airfoil nolds Number Free-Flight Aerodynamics of Subsonic Flow Morphing Flapping Wings C10-162 Span Efficiency Prediction Using Ad- C10-119 Frequency Selection Mechanism of C10-199 Coaxial Rotor Helicopter in Hover joint-Driven Mesh Refinement Airfoil Trailing-Edge Noise Based on Unstructured Dynamic Overset Grids C10-159 Induced-Drag Compressibility Correc- C10-044 Numerical Study of Flow Past a Circular C10-176 Computational Fluid Dynamics Analy- tion for Three-Dimensional Vortex-Lattice Meth- Cylinder Using Hybrid Turbulence Formulations ses of Flow over Weapons-Bay Geometries ods C10-036 Drag Force Balance of a Blunt and C10-080 Computational-Fluid-Dynamics-Based C10-124 In Pursuit of Grid Convergence for Two- Divergent Trailing-Edge Airfoil Clean-Wing Aerodynamic Noise Model for Dimensional Euler Solutions Design Computational Fluid Dynamics C10-151 Numerical Simulation of Rotor-Fuse- C10-075 Determining Direction for Optimization of Movable Wing Tip Strake C10-157 Bodies Having Minimum Pressure Drag lage-Cylinder Interaction in Forward Flight in Supersonic Flow: Investigating Nonlinear C10-184 Airfoil Optimization Using Practical Supersonic Flow Effects Aerodynamic Design Requirements C10-102 Aerodynamic Performance of the Three- C10-162 Span Efficiency Prediction Using Ad- C10-223 Computational-Fluid-Dynamics-Based Dimensional Lifting Supersonic Biplane joint-Driven Mesh Refinement Twist Optimization of Hovering Rotors C10-065 Adjoint-Based Design of Rotors in a C10-130 Transonic Aeroelastic Stability Predic- Transonic Flow Noninertial Reference Frame tions Under the Influence of Structural Variability C10-163 Evaluation of the Thrust Recovery of an C10-101 Hybrid Navier—Stokes/FreWea-ke C10-039 Mean Flowfield Structure of a Super- Aircraft Flapped Outflow Valve Method for Modeling Blade-Vortex Interactions sonic Three-Dimensional Base Flow C10-127 Effect of Normal Blowing on Compres- C10-135 Incorporation of Feedback Control into C10-072 Transition-Flow-Occurrence Estima- sible Convex-Corner Flows a High-Fidelity Aeroservoelastic Fighter Aircraft tion: A New Method C10-212 Particle Swarm Optimization of Suction Model Hydrodynamics and Blowing on an Airfoils at Transonic Speeds C10-032 Fast Large-Eddy Simulation of Low C10-124 In Pursuit of Grid Convergence for Two- C10-237 Flow-Separation Lines on Axisymmet- Reynolds Number Flows over a NACA0025 Dimensional Euler Solutions ric Bodies with Tapered Tails C10-079 Small Disturbance Navier-Stokes Com- putations for Low-Aspect-Ratio Wing Pitching Hypersonic Unsteady Flows Flow Oscillations C10-035 Effect of a Perturbed Shear Layer on C10-210 Approximate Modeling of Unsteady C10-067 Aircraft Vortex Wake and Flight Safety Cavity Resonance Problems Aerodynamics for Hypersonic Aeroelasticity C10-111 Pressure Waves Generated at the C10-090 Computational-Fluid-Dynamics- and Inlet, Nozzle, Diffuser, and Channel Downstream Corner of a Rectangular Cavity Computational-Structural-Dynamics-Based Flows C10-008 Characteristics of Pitching and Plunging Time-Accurate Aeroelasticity of Helicopter Rotor Airfoils Under Dynamic-Stall Conditions C10-192 Inlet Stagnation Pressure Loss Estimate Blades C10-079 Small Disturbance Navier-Stokes Com- for a Simplified Thrust Model C10-044 Numerical Study of Flow Past a Circular putations for Low-Aspect-Ratio Wing Pitching C10-059 Crosswind Effects on Engine Inlets: The Cylinder Using Hybrid Turbulence Formulations Oscillations Inlet Vortex C10-043 Modeling, Simulation, and Flight Tests C10-060 Effects of Unsteady Trailing-Edge C10-145 Reynolds-Stress Model Flow Prediction for a T-38 Talon with Wing Fences Blowing on Delta Wing Aerodynamics in Aircraft-Engine Intake Double-S-Shaped Duct C10-010 Toward Real-Time Aero-Icing Simula- C10-005 Parallel Multigrid Algorithm for Aero- tion of Complete Aircraft via FENSAP-ICE Jets, Wakes, and Viscid—Inviscid Flow elasticity Simulations C10-062 Planform and Camber Effects on the Interactions C10-235 Verification of H Flutter Analysis Aerodynamics of Low-Reynolds-Number Wings C10-127 Effect of Normal Blowing on Compres- C10-028 Vortex Dynamics of Free-to-Roll Slen- C10-098 Computational Investigation of Micro- sible Convex-Corner Flows der and Nonslender Delta Wings scale Coaxial-Rotor Aerodynamics in Hover C10-042 Interaction of Synthetic Jet with C10-014 Computation of Unsteady Low Rey- C10-142 Computation of Flow over a High- Boundary Layer Using Microscopic Particle nolds Number Free-Flight Aerodynamics of Performance Parafoil Canopy Image Velocimetry Flapping Wings C10-136 FENSAP-ICE: Analytical Model for C10-045 Computational Fluid Dynamics Valida- Spatial and Temporal Evolution of In-Flight Icing Plasmadynamics and MHD tion Study of Wake-Capturing Capability for Flat- Roughness C10-188 Closed-Loop Stall Control System Plate Wake 2194 J. AIRCRAFT, VOL. 47, NO. 6: 2010 INDEX C10-206 Lift Enhancement of Flapping Airfoils C10-106 Design of an Adaptive Gust Response Handling Qualities by Generalized Pitching Motion Alleviation Control System: Simulations and C10-132 Application of Bifurcation Methods to C10-199 Coaxial Rotor Helicopter in Hover Experiments the Prediction of Low-Speed Aircraft Ground Based on Unstructured Dynamic Overset Grids C10-100 Stability of Hybrid-Wing-Body-Type Performance C10-105 Unsteady Lift Generation on Rotating Aircraft with Centerbody Leading-Edge Carving C10-003 Longitudinal Handling Quality Analysis Wings at Low Reynolds Numbers C10-058 Characterizing Wing Rock with Varia- of a Civil Transport Aircraft Encountering Vortices tions in Size and Configuration of Vertical Tail Turbulence C10-169 Nonlinear Aeroelasticity of a Very Ci0-153 Experimental Investigation of Double- Flexible Blended-Wirg-Body Aircraft Navigation Hinged Vortex Flap Configurations C10-168 Dynamic Stability Analysis ofa C10-055 Panel-Method-Based Path Planning and C10-186 Influence of Differential Spoiler Settings Tethered Aerostat Collaborative Target Tracking for Swarming on the Wake Vortex Characterization and C10-137 Pitch and Heave Control of Robotic Micro Air Vehicies Alleviation Samara Micro Air Vehicles 10-123 Ionospheric Threat Parameterization for C10-125 Numerical Simulation of Rotor Using C10-020 Current Methods Modeling and Simu- Local Area Global-Positioning-System-Based Coupled Computational Fluid Dynamics and Free lating Icing Effects on Aircraft Performance, Aircraft Landing Systems Wake Stability, Control C10-062 Planform and Camber Effects on the C10-195 Analytical Criterion for Aircraft Spin Optimization Techniques Aerodynamics of Low-Reynolds-Number Wings Susceptibility C10-166 Using Multiobjective Evolutionary Al- C10-075 Determining Direction for Optimization C10-205 Dynamic Sensitivity to Atmospheric gorithms and Data-Mining Methods to Optimize of Movable Wing Tip Strake Turbulence of Unmanned Aerial Vehicles with Ornithopters’ Kinematics C10-014 Computation of Unsteady Low Rey- Varying Configuration C10-160 Micro Air Vehicle Trajectory Planning nolds Number Free-Flight Aerodynamics of C10-052 Controllable Drogue for Automated in Winds Flapping Wings Aerial Refueling C10-060 Effects of Unsteady Trailing-Edge Artificial Intelligence State Estimation Blowing on Delta Wing Aerodynamics C10-202 Integrated Framework for Artificial C10-129 Rapid Estimation of Impaired-Aircraft C10-059 Crosswind Effects on Engine Inlets: The Immunity-Based Aircraft Failure Detection, Aerodynamic Parameters Inlet Vortex Identification, and Evaluation C10-233 Decay of Aircraft Wake Vortices Under C10-002 Neural-Network-Based Flush Air Data Trajectory Optimization Daytime Free Convective Conditions Sensing System Demonstrated on a Mini Air C10-133 Airspace Constraints in Aircraft Emis- C10-211 Nature of Wakelike and Jetlike Axial Tip Vehicle sion Trajectory Optimization Vortex Flows C10-147_ Three-Dimensional Curvature-Con- C10-028 Vortex Dynamics of Free-to-Roll Slen- Autonomous Vehicles strained Trajectory Planning Based on In-Flight der and Nonslender Delta Wings Waypoints C10-199 Autonomous Soaring: The Montague C10-201 Flight Control Using Wing-Tip Plasma C10-160 Micro Air Vehicle Trajectory Planning Cross-Country Challenge Actuation in Winds C10-055 Panel-Method-Based Path Planning and C10-105 Unsteady Lift Generation on Rotating C10-110 Optimization of Hover-to-Cruise Tran- Collaborative Target Tracking for Swarming Wings at Low Reynolds Numbers sition Maneuver Using Variable-Incidence Wing Micro Air Vehicles C10-115 Effect of Jet-Exhaust Streams on C10-025 Intelligent Flight-Trajectory Generation Structure of Vortex Wakes to Maximize Safe-Outcome Probability After a Avionics Systems Distress Event C10-002 Neural-Network-Based Flush Air Data GUIDANCE, CONTROL, AND Sensing System Demonstrated on a Mini Air UAVs DYNAMICS TECHNOLOGY Vehicle C10-205 Dynamic Sensitivity to Atmospheric Turbulence of Unmanned Aerial Vehicles with Aircraft Dynamics Control System Effectors Varying Configuration C10-006 Effects of Rolling Maneuver on C10-052 Controllable Drogue for Automated Divergence and Flutter of Aircraft Wing Store Aerial Refueling INTERDISCIPLINARY TOPICS 10-058 Characterizing Wing Rock with Varia- Ci0-068 Gurney Flaps on Slender and Nons- tions in Size and Configuration of Vertical Tail lender Delta Wings Aerospace Management C10-132 Application of Bifurcation Methods to the Prediction of Low-Speed Aircraft Ground C10-092 Impact of an Innovative Quiet Regional Control System Sensors Performance Aircraft on the Air Transportation System C10-003 Longitudinal Handling Quality Analysis C10-041 Airborne Lidar for Automatic Feedfor- of a Civil Transport Aircraft Encountering ward Control of Turbulent In-Flight Phenomena Analytical and Numerical Methods Turbulence C10-049 Multilevel Structural Optimization for C10-052 Controllable Drogue for Automated Dynamics Preliminary Wing-Box Weight Estimation Aerial Refueling C10-183 Influence of Tire Inflation Pressure on C10-189 Data Mining of Pareto-Optimal Tran- sonic Airfoil Shapes Using Proper Orthogonal C10-196 Yaw Control of a Tailless Aircraft Nose Landing Gear Shimmy Configuration Decomposition C10-017 Videogrammetry Dynamics Measure- Fault-Tolerant Control C10-228 Optimizing Spanwise Lift Distributions ments of a Lightweight Flexible Wing in a Wind C10-202 Integrated Framework for Artificial Yacht Sails Using Extended Lifting Line Analysis Tunnel Immunity-Based Aircraft Failure Detection, C10-047 Application of Design of Experiments to Flight Test: A Case Study Aircraft Guidance Identification, and Evaluation C10-141 Effective Approach to Characterization C10-147 Three-Dimensional Curvature-Con- of Prediction Errors for Balloon Ascent Flight Mechanics strained Trajectory Planning Based on In-Flight Trajectories Waypoints C10-205 Dynamic Sensitivity to Atmospheric Turbulence of Unmanned Aerial Vehicles with Atmospheric and Space Sciences Aircraft Stability and Control Varying Configuration C10-155 Quick Access Recorder Data Analysis C10-170 Modeling of Pilot Landing Approach C10-141 Effective Approach to Characterization Software for Windshear and Turbulence Studies Control Using Stochastic Switched Linear of Prediction Errors for Balloon Ascent C10-097 Aerodynamic Simulation of Runback Regression Model Trajectories Ice Accretion J. AIRCRAFT, VOL. 47, NO. 6: 2010 INDEX 2195 CAD/CAM Research Facilities and Instrumentation €10-130 Transonic Aeroelastic Stability Predic- C10-229 Integration of Three-Dimensional Print- C10-203 Calibration Modeling of Nonmonolithic tions Under the Influence of Structural Variability ing Technology for Wind-Tunnel Model Fab- Wind-Tunnel Force Balances C10-134 Evaluation of Aeroelastic Uncertainty rication Safety Analysis Methods C10-156 Flutter Analysis: Using Piecewise Human Factors C10-227 Air-Vessel Corrosion Damage Distribu- Quadratic Interpolation with Mode Tracking and C10-217 Probabilities for Severe and Fatal tion and Reliability Modeling Wind-Tunnel Tests Injuries in General Aviation Accidents C10-173 Wind-Optimal Routing in the National C10-170 Modeling of Pilot Landing Approach Airspace System Dynamic Model Analysis Control Using Stochastic Switched Linear C10-019 Free Vibration Analysis of Curvilinear- LAUNCH VEHICLE AND Regression Model Stiffened Plates and Experimental Validation MISSILE (LV/M) TECHNOLOGY C10-209 Targeted Energy Transfer Between a Lasers and Laser Applications Model Flexible Wing and Nonlinear Energy Sink Aerodynamics C10-041 Airborne Lidar for Automatic Feedfor- ward Control of Turbulent In-Flight Phenomena C10-229 Integration of Three-Dimensional Print- Flexible and Active Structures ing Technology for Wind-Tunnel Model Fab- C10-033 Bistable Composite Flap for an Airfoil Multidisciplinary Design Optimization rication C10-222 Nonlinear Modeling and Aeroelastic C10-157 Bodies Having Minimum Pressure Drag C10-150 Prediction of Nonlinear Rolling and Analysis of an Adaptive Camber Wing in Supersonic Flow: Investigating Nonlinear Magnus Coefficients of Cruciform-Finned Mis- C10-029 Novel, Bidirectional, Variable~Camber Effects siles Airfoil via Macro-Fiber Composite Actuators C10-189 Data Mining of Pareto-Optimal Tran- C10-046 Mechanism for Warp-Controlled Twist PROPULSION sonic Airfoil Shapes Using Proper Orthogonal of a Morphing Wing Decomposition Airbreathing Propulsion C10-099 Airframe Design for Silent Fuel- Materials Structural Properties Efficient Aircraft C10-192 Inlet Stagnation Pressure Loss Estimate C10-071 Computational Workflow Management for a Simplified Thrust Model C10-112 Super- C10-172 Yield Strength and Residual Stress for Conceptual Design of Complex Systems cruise Aircraft Range Measurements on Friction-Stir-Welded Alumi- num Alloys C10-095 Characterization of Aerospace Vehicle Electric Propulsion C10-149 Lifetime Assessment of Aircraft Struc- Performance and Mission Analysis Using C10-200 First Fuel-Cell Manned Aircraft tural Components in Coastal Environments Thermodynamic Availability C10-178 Crack-Tip Behavior in Fiber/Metal C10-088 Tonal and Broadband Noise Calcula- Engine Materials Laminates dy Means of Digital-Image Correlation tions for Aeroacoustic Optimization of a Pusher C10-149 Lifetime Assessment of Aircraft Struc- C10-174 Adding Additional Load Paths in a Propeller tural Components in Coastal Environments Bonded/Bolted Hybrid Joint C10-114 Multidisciplinary Shape Optimization Hypersonic Propulsion of Aerostat Envelopes Structural Composite Materials C10-054 Multidisciplinary Considerations in the C10-095 Characterization of Aerospace Vehicle Design of Wings and Wing Tip Devices Performance and Mission Analysis Using C10-053 Compression Failure of Carbon Fiber- C10-049 Multilevel Structural Optimization for Thermodynamic Availability Epoxy Laminates in Fire C10-033 Bistable Composite Flap for an Airfoil Preliminary Wing-Box Weight Estimation Solar Power C10-178 Crack-Tip Behavior in Fiber/Metal C10-118 Design Optimization for Minimum C10-063 Optimal Sizing and Cruise Speed Laminates by Means of Digital-Image Correlation Sound Radiation from Point-Excited Curvili- Determination for a Solar-Powered Airplane C10-104 Damage of Carbon/Epoxy Composite nearly Stiffened Panel Plates Subjected to Mechanical Impact and C10-194 Improved Fuel Capacity Estimation REAL-TIME SYSTEMS Simulated Lightning Method C10-082 Optimal Design of Tow-Placed Fuselage C10-212 Particle Swarm Optimization of Suction Sensor Systems Panels for Maximum Strength with Buckling and Blowing on an Airfoils at Transonic Speeds C10-017 Videogrammetry Dynamics Measure- Considerations C10-208 Design Optimization of a Truss-Braced- ments of a Lightweight Flexible Wing in a Wind Wing Transonic Transport Aircraft Tunnel Structural Design C10-080 Computational-Fluid-Dynamics-Based Clean-Wing Aerodynamic Noise Model for Systems Engineering C10-016 Probabilistic Sensitivity-Based Ranking of Damage Tolerance Analysis Elements Design C10-193 Designing for a Green Future: A Unified C10-207 Optimal Design of Unitized Structures C10-165 Aerostructural Optimization of Non- Aircraft Design Methodology Using Response Surface Approaches planar Lifting Surfaces C10-231 Conceptual Design of an Aerospace C10-174 Adding Additional Load Paths in a C10-184 Airfoil Optimization Using Practical Vehicle Controller Using Axiomatic Theory Bonded/Bolted Hybrid Joint Aerodynamic Design Requirements C19-228 Optimizing Spanwise Lift Distributions STRUCTURAL MECHANICS C10-082 Optimal Design of Tow-Placed Fuselage Yacht Sails Using Extended Lifting Line Analysis AND MATERIALS Panels for Maximum Strength with Buckling Considerations C10-180 Optimization and Postbuckling Analy- sis of Curvilinear-Stiffened Panels Under Multi- Aeroelasticity and Control Structural Durability (Including Fatigue, ple-Load Cases C10-135 Incorporation of Feedback Control into C10-066 Analytical Sensitivity Analysis of an a High-Fidelity Aeroservoelastic Fighter Aircraft Fracture, and Environmental Unsteady Vortex-Lattice Method for Flapping- Model Degradation) Wing Optimization C10-007 Prediction of Tiltrotor Vibratory Loads C10-219 Uncertainty Reduction of Damage C10-166 Using Multiobjective Evolutionary Al- with Inclusion of Wing-Proprotor Aerodynamic Growth Properties Using Structural Health gorithms and Data-Mining Methods to Optimize Interaction Monitoring Ornithopters’ Kinematics C10-034 Efficient Numerical Aeroelastic Analy- C10-181 Estimation of Aircraft Structural Fatigue sis of a High-Aspect-Ratio Wing Considering Life Using the Crack Severity Index Methodology Reliability, Maintainability, and Logistics Geometric Nonlinearity C10-174 Adding Additional Load Paths in a Support C10-106 Design of an Adaptive Gust Response Bonded/Bolted Hybrid Joint C10-227 Air-Vessel Corrosion Damage Distribu- Alleviation Control System: Simulations and C10-018 Fatigue-Based Severity Factors for tion and Reliability Modeling Experiments Shear-Loaded Fastener Joints 2196 J. AIRCRAFT, VOL. 47, NO. 6: 2010 INDEX Structural Dynamics and C10-019 Free Vibration Analysis of Curvilinear- Structural Stability Characterization Stiffened Plates and Experimental Validation C10-089 Exploring the Stability Landscape of C10-015 Effect of Uncertainty on Hub Vibration Constant-Stress Pumpkin Balloon Designs Response of Composite Helicopter Rotor Blades Structural Optimization C10-131 Validation Studies for Aeroelastic Trim C10-131 Validation Studies for Aeroelastic Trim and Stability of Highly Flexible Aircraft and Stability of Highly Flexible Aircraft C10-118 Design Optimization for Minimum C10-006 Effects of Rolling Maneuver on Sound Radiation from Point-Excited Curvili- C10-183 Influence of Tire Inflation Pressure on Divergence and Flutter of Aircraft Wing Store Nose Landing Gear Shimmy nearly Stiffened Panel C10-207 Optimal Design of Unitized Structures Thermal Effects Structural Finite Elements Using Response Surface Approaches C10-053 Compression Failure of Carbon Fiber- C10-222 Nonlinear Modeling and Aeroelastic C10-103 Reliability-Based Design Optimization Epoxy Laminates in Fire Analysis of an Adaptive Camber Wing of Nonlinear Aeroelasticity Problems Structural Modeling C10-180 Optimization and Postbuckling Analy- THERMOPHYSICS AND HEAT sis of Curvilinear-Stiffened Panels Under Multi- C10-089 Exploring the Stability Landscape of TRANSFER Constant-Stress Pumpkin Balloon Designs ple-Load Cases C10-183 Influence of Tire Inflation Pressure on C10-165 Aerostructural Optimization of Non- Nose Landing Gear Shimmy planar Lifting Surfaces Ablation, Pyrolysis, Thermal C10-009 Bifurcation Analysis of Nose-Landing- C10-082 Optimal Design of Tow-Placed Fuselage Decomposition and Degradation Gear Shimmy with Lateral and Longitudinal Panels for Maximum Strength with Buckling C10-053 Compression Failure of Carbon Fiber- Bending Considerations Epoxy Laminates in Fire