Journal of Aircraft 2007: Vol 44 Index

2007·8 MB·English

JOURNAL OF AIRCRAFT
Vol. 44, No. 6, December 2007
2007 Journal of Aircraft Index
How to Use the Index
In the Subject Index, pages 2091-2099, 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 2100-2102, lists all authors associated with a given technical paper. The locating numbers are identical to
those in the Subject Index. The Chronological Index, pages 2103-2110, 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 2007, 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, C07-031 Drag and Flutter Characteristics of Loop C07-224 Upstream Blowing Jet on Transonic
CONVENTIONAL, STOL/VTOL Membranes Convex-Corner Flow
C07-098 Drag Prediction in Transitional Flow C07-197 Development and Testing of the Mentor
Aerodynamics Over Airfoils Flapping-Wing Micro Air Vehicle
C07-105 Predicting Maximum Lift Coefficient C07-218 Effect of Thrust-Vectoring Jets on Delta
c07-008 Investigation on the Conditions of
for Twisted Wings Using Lifting-Line Theory Wing Aerodynamics
Minimum Induced Drag of Closed Wing Systems
C07-034 Effect of Flap Motion on Unsteady C07-092 Extension of Projectile Range Using
and C-Wings
Aerodynamic Loads Oblique-Wing Concept
co7-058 Autonomous Sensing and Control of
C07-039 Exploratory Investigation of Geometry C07-018 Computational Analysis on Flow
Wing Stall Using a Smart Plasma Slat
Effects on Gurney Flap Performance Through Transition s-Diffusers: Effect of Inlet
C07-026 Effect of a Winglet on Normal Blade-
Vortex Interaction C07-075 Thin-Airfoil Theoretical Interpretation Shape
for Gurney Flap Lift Enhancement C07-021 Experimental Investigation of Vectoring
c07-030 Effect of a Porosity Strength on Drag
C07-037 Unified Approximation for Nonpara- Jet on Aerodynamic Characteristics of Aircraft
Reduction of a Transonic Projectile
bolic Drag Polars C€07-025 Design Guidelines of Rotary Wings in
c07-060 Experimental Investigation into the
C07-111 Dynamic Wing Airloads with Higher Hover for Insect-Scale Micro Air Vehicle
Aerodynamics of Battie Damaged Airfoils
C07-100 Development of a Trailing Vortex Harmonic Flap Motion Applications
Formed with Spanwise Tip Jets 07-200 Steep-Descent Maneuver of Transport C07-011 Automatic Transition Prediction and
C07-041 Iterative Response Surface Based Aircraft Application to Three-Dimensional Wing Confi-
Optimization Scheme for Transonic Airfoil 07-112 Aerodynamic Characteristics of Para- gurations
Design drogue Assembly in an Aerial Refueling System C07-009 Dynamics of Corotating Vortex Fila-
C€07-023 Design and Numerical Optimization of C07-178 Compressible Unsteady Vortex Lattice ments Part 2: Experimental Results
Thick Airfoils Including Blunt Trailing Edges Method for Arbitrary Two-Dimensional Motion C07-012 Reynolds Number Effects on Off-
C€07-159 Adaptive Airfoil Dynamic Stall Control of Thin Profiles Design Stability and Control Characteristics of
C07-106 Predicting Maximum Lift Coefficient C07-208 High Resolution Turbulence Treatment Supersonic Transports
for Twisted Wings Using Computational Fluid of F/A-18 Tail Buffet C07-017 Comparison of Reynolds-Averaged
Dynamics C07-202 Two Aspects of Use of Full- and Partial- Navier-Stokes Simulations of Multi-Element
C07-033 Method Based on Chebyshev Polyno- Span Gurney Flaps High-Lift Configurations
mials for Aerservoelastic Interactions on an F/A- C07-215 Unsteady Numerical Simulation of C07-063 Two-Dimensional Wind Tunnel and
18 Aircraft Wings with Flaperon Flying Over Nonplanar Computational Investigation of a Microtab
C€07-035 Flow Control by Spanwise Blowing ona Ground Surface Modified Airfoil
NACA 0012 C07-216 Return from Aerofoil Stall During C07-072 Flight Control Using Synthetic Jets on a
C€07-099 Post-Stall Motions Evolving Toward Ramp-Down Pitching Motions Cessna 182 Model
Chaos C07-223 Lift Enhancement by Static Extended C07-015 Robust Design of an Aerodynamic
C07-028 Aerodynamic Performance of a Biplane Trailing Edge Compensation Pitot-Static Tube for Supersonic
Micro Air Vehicle C07-225 Error Quantification for Computational Aircraft
C07-145 Hybrid Design for Aircraft Wind- Aerodynamics Using an Error Transport Equation 07-038 Weight Criterion on Flow Control in
Tunnel Testing Using Response Surface Method- 07-174 Actuator-Work Concepts Applied to Level Flight
ologies Unconventional Aerodynamic Control Devices C07-113 Multipoint Aerodynamic Design of
C07-170 Lift and Drag Characteristics of a C07-220 Drag Decomposition-Based Adaptive Wing-Body Configurations for Minimum Drag
Blended-Wing Body Aircraft Mesh Refinement C07-102 Active Separation Control on the Flap of
C07-219 Aerodynamic Control of Using Wind- C07-242 Evaluation of Effectiveness of Periodic a Two-Dimensional Generic High-Lift Configu-
ward-Surface Plasma Actuators on a Separation Flight by a Hypersonic Vehicle ration
Ramp C07-222 Aerodynamic and Mission Performance C07-077 Wave Drag Characteristics of a Low-
C07-001 Aerodynamic Modeling of Morphing of a Winged Balloon Guidance System Drag Supersonic Formation Flying Concept
Wings Using an Extended Lifting-Line Analysis 07-211 Design of a Passively Reefed, Collaps- 07-024 Wake Vorticity Measurements for Low
C07-016 Effect of Microvortex Generators On ible Drogue Parachute System Aspect Ratio Wings at Low Reynolds Number
Seperated Normal Shock/ Boundary Layer C07-244 Experimental Studies on Unsteady 07-052 Time-Area-Averaged Momentum
Interactions Lateral Blowing on NACA 0012 Stream Tube Model for Flapping Flight
2091
2092 J. AIRCRAFT, VOL. 44, NO. 6: 2007 INDEX
C07-079 Trailing Vortex Filament: A Novel C07-213 Aerodynamic Characteristics of Bodies C07-234 Assessment of Critical Fuel Configura-
Similarity Analysis of Revolution at Near-Sonic Speeds tions Using Robust Flutter Analysis
C07-083 Generalized Empirical Airfoil Stagna- C07-164 Hub Drag-Reduction Strategies of C07-181 Nonlinear Flight Dynamics of Very
tion Point Location Prediction Canard Rotor/Wing Unmanned Aerial Vehicles Flexible Aircraft
C07-190 Investigation of Surface Roughness on C07-142 Response Surface Methods for Efficient C07-117 Reduced Order Aerodynamic Model for
Aerodynamics Properties Complex Aircraft Configuration Aerodynamic Aeroelastic Analysis of Complex Configurations
C07-185 Computational Study of Submerged Air Characterization in Incompressible Flow
Inlet Performance Improvement Using Vortex 07-147 Flowfield of aR otating-Wing Micro Air C07-066 Nonlinear Aeroelastic Analysis for a
Generators Vehicle Control Fin with an Actuator
C€07-177 Navier-Stokes Analysis of Airfoils with C07-169 Experimental Evaluation of Sinusoidal C07-002 Gust Loads Alleviation Using Special
Gurney Flap Leading Edges Control Surfaces
C07-135 Computational Fluid Dynamics Study C07-214 Effects of Strake Planform Change on C07-005 Computational Aeroelastic Analysis of
of Three-Dimensional Dynamic Stall of Various Vortex Flow of a Double-Delta Wing Store-Induced Limit-Cycle Oscillation
Planform Shapes C07-217 Effect of Streamwise Slots on the Drag 07-033 Method Based on Chebyshev Polyno-
C07-149 Effect of Acoustic Slat Modifications on of a Transonic Projectile mials for Aerservoelastic Interactions on an F/A-
Aerodynamic Properties of High-Lift Systerms C07-203 Effect of Leading-Edge Form on 18 Aircraft
C07-128 Problems with Leading-Edge Flow Performance of Wing-Movable Tip Strake C07-014 Volterra Kernel Extrapolation for Mod-
Control Experiments Configurations eling Nonlinear Aeroelastic Systems at Novel
C07-121 Experimental Study of a Telescopic C07-141 Evaluation of a Simplified Grid Treat- Flight Conditions
Morphing Aspect Ratio Wing Inside a Channel ment for Oscillating Trailing-Edge Control C07-067 Case of Explosive Wing-Flaperon
C07-127 Improved Dynamic-Stall-Onset Criteri- Surfaces Flutter
on at Low Mach Numbers C07-204 Passive Control of Bluff Body Using C07-246 Reduced-Order-Model-Based Flutter
Stepped-Nose Obstacle Analysis at High Angle of Attack
C07-162 Unsteady Aerodynamic Forces Mixed
C07-206 Sensitivity of Aircraft Performance to
Method for Aeroservoelasticity Studies on an F/ Air Transportation
Icing Parameter Variations
A-18 Aircraft
C07-239 Improving the Stability and Efficiency C07-176 Coupled Vehicle Design and Network
C07-107 Automatic Transition Prediction and
of the Pseudocompressibility Method Flow Optimization for Air Transportation
Application to Three-Dimensional High-Lift
C07-245 Aerodynamic Hysteresis of a Low- Systems
Configurations
Reynolds-Number Airfoil C€07-146 System-of-Systems Inspired Aircraft
C07-116 Aerodynamic Performance Analysis of
Sizing and Airline Resource Allocation via
a Gurney Flap for Rotorcraft Application Aeroelasticity and Aeroservoelasticity Decomposition
C07-049 Advancements in Aircraft Model Force
C07-104 CFD-Based Models of Aerodynamic C07-077 Wave Drag Characteristics of a Low-
and Attitude Instrumentation by Integrating
Gust Response Drag Supersonic Formation Flying Concept
Statistical Methods
C07-141 Evaluation of a Simplified Grid Treat- C07-156 Potential Impacts of Very Light Jets in
C07-191 Early Flight-Test and Other Boundary-
ment for Oscillating Trailing-Edge Control the National Airspace System
Layer Research at Mississippi State 1949-1960
Surfaces C07-062. Wake of Transport Flying Wings
C07-132 Design and Testing of a Pneumatic C07-137 Supersonic Nonlinear Panel Flutter C07-140 Methodology for Optimizing Parame-
Telescopic Wing for Unmanned Aerial Vehicles Suppression Using Shape Memory Alloys ters of Noise-Abatement Approach Procedures
C€07-189 Aerodynamic Characteristics of a Free-
07-172 Active Tiltrotor Whirl-Flutter Stability
Wing Tilt-Body Unmanned Aerial Vehicle Airframe-Propulsion Integration
Augmentation Using Wing-Flaperon and Swash-
C07-036 Planform Variations and Aerodynamic Plate Actuation C07-175 Shape Memory Alloy Based Smart
Efficiency of Movable Tip Strakes C07-163 Modeling the Benchmark Active Con- Landing Gear for an Airship
C07-179 Application of CFD-Based Unsteady C07-237 Proposal to Use Reaction Jets for
trols Wing Through Linear and Computational
Forces for Efficient Aeroelastic Stability Analyses Aeroelastic Analyses Variable Stability Airplanes
C07-139 Why Birds and Miniscale Airplanes
Need No Vertical Tail C07-088 Investigation of Membrane Actuation Airframe-Weapon System Integration
for Roll Control of a Micro Air Vehicle
07-195 Analysis of Wind Tunnel Wall Interfer- C07-118 Comparison of Computational Fluid
C07-114 Fuzzy-Logic-Based Health Monitoring
ence Effects on Subsonic Unsteady Airfoil Flows Dynamics Approaches for Simulating Weapons
and Residual-Life Prediction for Composite
C07-096 Study on the Induced Velocity and Bay Flow
Helicopter Rotor
Noise Characteristics of a Scissors Rotor
C07-179 Application of CFD-Based Unsteady Civil Missions and Transportation
C07-165 Prediction of Hovering Rotor Noise Forces for Efficient Aeroelastic Stability Analyses
Based on Reynolds-Averaged Navier-Stokes C07-043 Improved Algorithm for Takeoff Mon-
C07-162 Unsteady Aerodynamic Forces Mixed
Simulation itoring
Method for Aeroservoelasticity Studies on an F/
C07-168 Harmonic Representation of Aerody- A-18 Aircraft C07-210 Determination of Minimum Thrust
namic Lift and Drag Coefficients Requirement for a Passenger Aircraft
C07-119 Surface Splines Generalization and
C07-158 Optimization of Aifoil Flow Control Large Deflection Interpolation C07-077_ Wave Drag Characteristics of a Low-
Using a Genetic Algorithm with Diversity Control C07-073 Cantilevered Plate Rayleigh-Ritz Trial Drag Supersonic Formation Flying Concept
C07-167 Effect of Gurney Flap on Unsteady Function Selection for von Karman’s Plate Collision Avoidance
Wake Vortex Equations C07-061 On the Probability of Collision Between
C07-166 Performance of Articulated Flapping C07-006 Transient and Limit Cycle Simulation of Climbing and Descending Aircraft
Wings with Partial Leading-Edge Suction a Nonlinear Aeroelastic System
C07-148 Aerodynamic Loading for an Airfoil 07-174 Actuator-Work Concepts Applied to Communication and Air Traffic Control
with an Oscillating Gurney Flap Unconventional Aerodynamic Control Devices C07-156 Potential Impacts of Very Light Jets in
C07-152 Experimental Investigation of Unsteady C07-208 High Resolution Turbulence Treatment the National Airspace System
Flow Separation on a Maneuvering Axisymmetric of F/A-18 Tail Buffet
Body 07-188 Thermal Buckling and Nonlinear Flutter Configuration Design
C07-180 Optimum Shape Design for Unsteady Behavior of Functionally Graded Material Panels 07-078 Particle Swarm Approach in Finding
Three-Dimensional Viscous Flows Using a C07-240 Bending-Torsion Divergence of a Optimum Aircraft Configuration
Nonlinear Frequency-Domain Method Clamped-Clamped Composite Wing 07-056 Aeromechanics Analysis of aH eavy Lift
C07-192 Experimental Aerodynamic Study of C07-236 Parametric Studies on Ground Vibration Slowed-Rotor Compound Helicopter
Tandem Flapping Membrane Wings Test Modeling for Highly Flexible Aircraft C07-062 Wake of Transport Flying Wings
J. AIRCRAFT, VOL. 44, NO. 6: 2007 INDEX 2093
C07-101 Multi-Objective Aerodynamic Explora- Flight Mechanics C07-050 Reynolds-Averaged Navier-Stokes
tion of Elements’ Setting for High-Lift Airfoil C07-237 Proposal to Use Reaction Jets for Analysis of Zero Efflux Flow Control over a
Using Kriging Model Variable Stability Airplanes Hump Model
C07-036 Planform Variations and Aerodynamic C07-200 Steep-Descent Maneuver of Transport C07-102 Active Separation Control on the Flap of
Efficiency of Movable Tip Strakes Aircraft a Two-Dimensional Generic High-Lift Configu-
C07-084 Tradeoffs in Jet Inlet Design: A C07-109 Simplified Rotor Inflow Model for ration
Historical Perspective Descent Flight C07-038 Weight Criterion on Flow Control in
C07-210 Determination of Minimum Thrust C07-037 Unified Approximation for Nonpara- Level Flight
Requirement for a Passenger Aircraft bolic Drag Polars C07-128 Problems with Leading-Edge Flow
C07-226 New Computational Procedure for C07-061 On the Probability of Collision Between Control Experiments
Incorporating Computational Fluid Dynamics Climbing and Descending Aircraft C07-167 Effect of Gurney Flap on Unsteady
into Sonic Boom Prediction C07-060 Experimental Investigation into the Wake Vortex
C07-203 Effect of Leading-Edge Form on Aerodynamics of Battle Damaged Airfoils C07-148 Aerodynamic Loading for an Airfoil
Performance of Wing-Movable Tip Strake with an Oscillating Gurney Flap
C07-081 Momentum-Impulse Balance and Para-
Configurations C07-150 Plasma Actuators for Hingeless Aero-
chute Inflation: Disreefing
C07-171 Preliminary Aerostructural Optimiza- dynamic Control of an Unmanned Air Vehicle
C07-120 Momentum-Impulse Balance and Para-
tion of a Large Business Jet C07-214 Effects of Strake Planform Change on
chute Inflation: Fixed Point Drops
C07-192 Experimental Aerodynamic Study of Vortex Flow of a Double-Delta Wing
C07-168 Harmonic Representation of Aerody-
Tandem Flapping Membrane Wings C07-217 Effect of Streamwise Slots on the Drag
namic Lift and Drag Coefficients
C07-164 Hub Drag-Reduction Strategies of of a Transonic Projectile
C07-124 Momentum-Impulse Balance and Para-
Canard Rotor/Wing Unmanned Aerial Vehicles C07-204 Passive Control of Bluff Body Using
chute Inflation: Rocket-Propelled Payloads
C07-169 Experimental Evaluation of Sinusoidal Stepped-Nose Obstacle
C07-139 Why Birds and Miniscale Airplanes
Leading Edges C07-245 Aerodynamic Hysteresis of a Low-
Need No Vertical Tail
C07-028 Aerodynamic Performance of a Biplane Reynolds-Number Airfoil
C07-080 Momentum-Impulse Balance and Para-
Micro Air Vehicle
chute Inflation: Clusters
C07-039 Exploratory Investigation of Geometry Fuels and Fuel Systems
C07-128 Problems with Leading-Edge Flow
Effects on Gurney Flap Performance Control Experiments C07-112 Aerodynamic Characteristics of Para-
C07-055 Computational Analysis of Wake Vor- drogue Assembly in an Aerial Refueling System
tices Generated by Notched Wings C07-234 Assessment of Critical Fuel Configura-
C07-004 Aircraft Geometry Design and Optimi- Flight Operations tions Using Robust Flutter Analysis
zation for Sonic Boom Reduction C07-010 Implementing Time-Based Spacing for
07-174 Actuator-Work Concepts Applied to Decelerating Approaches General Aviation
Unconventional Aerodynamic Control Devices C07-242 Evaluation of Effectiveness of Periodic C07-027 Current Experimental Basis for Model-
C07-146 System-of-Systems Inspired Aircraft Flight by a Hypersonic Vehicle ing Ice Accretions on Swept Wings
Sizing and Airline Resource Allocation via
C07-067 Case of Explosive Wing-Flaperon
Decomposition
Flow Control Flutter
C07-211 Design of a Passively Reefed, Collaps-
ible Drogue Parachute System C07-221 Forebody Geometry Effects on the Flow C07-004 Aircraft Geometry Design and Optimi-
zation for Sonic Boom Reduction
C07-012 Reynolds Number Effects on Off- of a Blunt-Nose Projectile at High Alpha
C07-201 Comparative Flight Tests with and
Design Stability and Control Characteristics of C07-244 Experimental Studies on Unsteady
Without Tip Tanks
Supersonic Transports Lateral Blowing on NACA 0012
C07-156 Potential Impacts of Very Light Jets in
C07-072 Flight Control Using Synthetic Jets on a
the National Airspace System
Deceleration Systems Cessna 182 Model
C07-063 Two-Dimensional Wind Tunnel and
C07-042 Geometric Properties of Parachutes Ground Effect Machines
Computational Investigation of a Microtab
Using 3-D Laser Scanning Modified Airfoil C07-215 Unsteady Numerical Simulation of
C07-211 Design of a Passively Reefed, Collaps- C07-069 Adaptive Compensation Control of Wings with Flaperon Flying Over Nonplanar
ible Drogue Parachute System Synthetic Jet Actuator Arrays for Airfoil Virtual Ground Surface
C07-120 Momentum-Impulse Balance and Para-
Shaping
chute Inflation: Fixed Point Drops Landing Dynamics
C07-223 Lift Enhancement by Static Extended
C07-081 Momentum-Impulse Balance and Para-
Trailing Edge C07-228 Closed-Form Analytical Solution for the
chute Inflation: Disreefing
C07-159 Adaptive Airfoil Dynamic Stall Control Shimmy Instability of Nose-Wheel Landing Gears
C07-059 Universality Considerations for Graph-
C07-035 Flow Control by Spanwise Blowing ona C07-229 Lateral Response of Nonlinear Nose-
ing Parachute Opening Shock Factor Versus Mass
NACA 0012 Wheel Landing Gear Models with Torsional Free
Ratio
C07-054 Effect of Swirl Flows in Aeronautical Play
C07-031 Drag and Flutter Characteristics of Loop
Mix Manifolds C07-230 Lateral Response of Nose-Wheel Land-
Membranes
C07-124 Momentum-Impulse Balance and Para- C07-058 Autonomous Sensing and Control of ing Gear System to Ground-Induced Excitation
Wing Stall Using a Smart Plasma Slat C07-184 Application of Probability Methods to
chute Inflation: Rocket-Propelled Payloads
C07-080 Momentum-Impulse Balance and Para- C07-111 Dynamic Wing Airloads with Higher Assess Airframe Crash Modeling Uncertainty
chute Inflation: Clusters Harmonic Flap Motion
C07-020 Robust Multivariable Closed-Loop Lighter-Than-Air Systems
Economics Control of a Turbulent Backward-Facing Step C07-243 Effect of High-Altitude Airship’s Atti-
Flow tude on Performance of its Energy System
07-125 Method for Multivariate Analysis with C07-075 Thin-Airfoil Theoretical Interpretation C07-222 Aerodynamic and Mission Performance
Small Sample in Aircraft Cost Estimation for Gurney Flap Lift Enhancement of a Winged Balloon Guidance System
C07-219 Aerodynamic Control of Using Wind- 07-068 Near-Space Station-Keeping Perform-
Flight Control Integration ward-Surface Plasma Actuators on a Separation ance of a Large High-Altitude Notional Airship
C07-168 Harmonic Representation of Aerody- Ramp 07-173 Analysis and Design of Robust Helium
namic Lift and Drag Coefficients C07-016 Effect of Microvortex Generators On Aerostats
C07-072 Flight Control Using Synthetic Jets ona Seperated Normal Shock/ Boundary Layer 07-074 Structures of the Low-Altitude Sta-
Cessna 182 Model Interactions tionary Flight Test Vehicle
2094 J. AIRCRAFT, VOL. 44, NO. 6: 2007 INDEX
C07-091 Unstable, Cyclically Symmetric and C07-114 Fuzzy-Logic-Based Health Monitoring C07-053 Wake Vortex Model for Real-Time
Stable, Asymmetric Pumpkin-Balloon Configu- and Residual-Life Prediction for Composite Flight Simulation Based on Large Eddy
rations Helicopter Rotor Simulation
C07-116 Aerodynamic Performance Analysis of C07-151 Residual Stress/Strain in Three-Row,
Manufacturing
a Gurney Flap for Rotorcraft Application Countersunk, Riveted Lap Joints
C07-136 Automated Aircraft Sheet Metal Com- 07-056 Aeromechanics Analysis of aH eavy Lift 07-238 Ground Dynamics Model Validation by
ponent Production Technologies Slowed-Rotor Compound Helicopter Use of Landing Flight Test
Micro Air Vehicles C07-198 Flight Test Evaluation of a Helicopter C07-120 Momentum-Impulse Balance and Para-
Airborne Lidar chute Inflation: Fixed Point Drops
C07-129 Morphing Wing Flight Control Via C07-122 Semi-Active Control of Vertical Strok- C07-081 Momentum-Impulse Balance and Para-
Postbuckled Precompressed Piezoelectric Actua- ing Helicopter Crew Seat for Enhanced chute Inflation: Disreefing
tors Crashworthiness C07-109 Simplified Rotor Inflow Model for
C07-022 Modelization and Kinematics Optimi- C€07-094 Two-Dimensional Unsteady Aerody- Descent Flight
zation for a Flapping-Wing Microair Vehicle namic Application to Higher Harmonic Control C07-228 Closed-Form Analytical Solution for the
C07-197 Development and Testing of the Mentor Test Data Shimmy Instability of Nose-Wheel Landing Gears
Flapping-Wing Micro Air Vehicle C07-079 Trailing Vortex Filament: A Novel C07-243 Effect of High-Altitude Airship’s Atti-
C07-207 Experimental Study of a Micro Air Similarity Analysis tude on Performance of its Energy System
Vehicle with a Rotatable Tail C07-227 Distributed Rate-Dependent Elastoslide 07-230 Lateral Response of Nose-Wheel Land-
C07-028 Aerodynamic Performance of a Biplane Model for Elastomeric Lag Dampers ing Gear System to Ground-Induced Excitation
Micro Air Vehicle C07-238 Ground Dynamics Model Validation by C07-229 Lateral Response of Nonlinear Nose-
C07-088 Investigation of Membrane Actuation Use of Landing Flight Test Wheel Landing Gear Models with Torsional Free
for Roll Control of a Micro Air Vehicle 07-147 Flowfield of a Rotating-Wing Micro Air Play
C07-139 Why Birds and Miniscale Airplanes
Vehicle
Need No Vertical Tail
C07-024 Wake Vorticity Measurements for Low 07-172 Active Tiltrotor Whirl-Flutter Stability STOL/VTOL/STOVL
Augmentation Using Wing-Flaperon and Swash-
Aspect Ratio Wings at Low Reynolds Number C07-172 Active Tiltrotor Whirl-Flutter Stability
Plate Actuation
C07-147 Flowfield of aR otating-Wing Micro Air Augmentation Using Wing-Flaperon and Swash-
C€07-159 Adaptive Airfoil Dynamic Stall Control
Vehicle Plate Actuation
C€07-025 Design Guidelines of Rotary Wings in
C07-186 Streamwise Vorticity in Simple Me- C07-164 Hub Drag-Reduction Strategies of
Hover for Insect-Scale Micro Air Vehicle
chanical Flapping Wings Canard Rotor/Wing Unmanned Aerial Vehicles
Applications
C07-192 Experimental Aerodynamic Study of C07-189 Aerodynamic Characteristics of a Free-
C07-109 Simplified Rotor Inflow Model for
Tandem Flapping Membrane Wings Wing Tilt-Body Unmanned Aerial Vehicle
Descent Flight
C07-116 Aerodynamic Performance Analysis of
Noise C07-205 In-Flight GPS-Signal-Reception
a Gurney Flap for Rotorcraft Application
C07-140 Methodology for Optimizing Parame- Anomalies of Helicopters
ters of Noise-Abatement Approach Procedures Structural Design (Including Loads)
C07-143 Experimental Training and Validation Safety C07-184 Application of Probability Methods to
of a System for Aircraft Acoustic Signature C07-065 Finite Element Modeling of a Bird Assess Airframe Crash Modeling Uncertainty
Identification
Striking an Engine Fan Blade C07-126 Interval Analysis-Based Optimum De-
C07-096 Study on the Induced Velocity and
C07-043 Improved Algorithm for Takeoff Mon- sign of Wing Structures Under Taxiing Loads
Noise Characteristics of a Scissors Rotor
itoring C07-151 Residual Stress/Strain in Three-Row,
C07-004 Aircraft Geometry Design and Optimi-
C07-060 Experimental Investigation into the Countersunk, Riveted Lap Joints
zation for Sonic Boom Reduction
Aerodynamics of Battle Damaged Airfoils C07-183 Measured Statistics of Multicomponent
C07-200 Steep-Descent Maneuver of Transport
C07-095 Characterization of Aircraft Wake Gust Patterns in Atmospheric Turbulence
Aircraft
Vortices by Airborne Coherent Doppler Lidar 07-153 Residual Strength of Panels with Cracks
C07-003 Analysis of the Airframe Noise of an
C07-061 On the Probability of Collision Between Based on a Plastic Hinge
A320/A321 with a Parametric Method
Climbing and Descending Aircraft C07-173 Analysis and Design of Robust Helium
Performance C07-086 Ultrasonic Method for Aircraft Wake Aerostats
C07-068 Near-Space Station-Keeping Perform- Vortex Detection C07-019 A Tensile Stress Concentration Equa-
ance of a Large High-Altitude Notional Airship C07-122 Semi-Active Control of Vertical Strok- tion for Countersunk Holes
C07-043 Improved Algorithm for Takeoff Mon- ing Helicopter Crew Seat for Enhanced C07-196 Hybrid If] Numerical Model for Aircraft
itoring Crashworthiness Seat Crash Performance Assessment
C07-074 Structures of the Low-Altitude Sta-
C07-037 Unified Approximation for Nonpara- C07-090 Corrosion Pillowing in Aircraft Fuse-
bolic Drag Polars lage Lap Joints tionary Flight Test Vehicle
C07-044 Study of Near-Optimal Endurance- Structural Materials
Maximizing Periodic Cruise Trajectories Simulation
C07-074 Structures of the Low-Altitude Sta-
C07-201 Comparative Flight Tests with and
Without Tip Tanks C07-123 Dynamic Coupling of the KC-135 tionary Flight Test Vehicle
Tanker and Boom for Modeling and Simulation C07-175 Shape Memory Alloy Based Smart
Powerplant Integration C07-101 Multi-Objective Aerodynamic Explora- Landing Gear for an Airship
C07-210 Determination of Minimum Thrust tion of Elements’ Setting for High-Lift Airfoil C€07-090 Corrosion Pillowing in Aircraft Fuse-
Requirement for a Passenger Aircraft Using Kriging Model lage Lap Joints
C07-084 Tradeoffs in Jet Inlet Design: A C07-162 Unsteady Aerodynamic Forces Mixed
Historical Perspective Method for Aeroservoelasticity Studies on an F/ System Effectiveness
A-18 Aircraft C07-176 Coupled Vehicle Design and Network
Rotorcraft C07-108 Motion-Visual Phase-Error Detection in Flow Optimization for Air Transportation
C07-096 Study on the Induced Velocity and a Flight Simulator Systems
Noise Characteristics of a Scissors Rotor C07-080 Momentum-Impulse Balance and Para-
C07-165 Prediction of Hovering Rotor Noise chute Inflation: Clusters Testing, Flight and Ground
Based on Reynolds-Averaged Navier-Stokes C07-048 Perception Model Analysis of Flight C07-003 Analysis of the Airframe Noise of an
Simulation Simulator Motion for a Decrab Maneuver A320/A321 with a Parametric Method
J. AIRCRAFT, VOL. 44, NO. 6: 2007 INDEX 2095
C07-012 Reynolds Number Effects on Off- COMPUTING, INFORMATION, C07-070 Numerical Simulation of Airfoil Ther-
Design Stability and Control Characteristics of AND COMMUNICATION mal Anti-Ice Operation, Part 1: Mathematical
Supersonic Transports Modeling
C07-145 Hybrid Design for Aircraft} Wind- Avionics Systems
Tunnel Testing Using Response Surface Method- C07-160 Magnetometer Autocalibration Lever- Boundary-Layer Stability and Transition
ologies aging Measurement Locus Constraints C07-170 Lift and Drag Characteristics of a
C07-045 Fast Identification and Characterization Controls and Displays Blended-Wing Body Aircraft
of Nonlinearities in Experimental Modal Analysis C07-098 Drag Prediction in Transitional Flow
C07-085 Cueing System for Near-Term Imple-
of Large Aircraft Over Airfoils
mentation of Aircraft Noise Abatement Approach
C07-049 Advancements in Aircraft Model Force C07-011 Automatic Transition Prediction and
Procedures
and Attitude Instrumentation by Integrating Application to Three-Dimensional Wing Confi-
Statistical Methods gurations
ENERGY
C07-191 Early Flight-Test and Other Boundary- C07-245 Aerodynamic Hysteresis of a Low-
Layer Research at Mississippi State 1949-1960 Fuel Cells Reynolds-Number Airfoil
C€07-094 Two-Dimensional Unsteady Aerody- C07-191 Early Flight-Test and Other Boundary-
C07-241 Specific Weight: A Challenge for a Fuel-
namic Application to Higher Harmonic Control Layer Research at Mississippi State 1949-1960
Cell-Powered Electric Helicopter
Test Data C07-107 Automatic Transition Prediction and
C07-198 Flight Test Evaluation of a Helicopter Solar Power Application to Three-Dimensional High-Lift
Configurations
Airborne Lidar C07-243 Effect of High-Altitude Airship’s Atti-
C07-238 Ground Dynamics Model Validation by tude on Performance of its Energy System C07-103 Effect of Oscillation on Boundary-Layer
Development with Adverse Pressure Gradients
Use of Landing Flight Test C07-068 Near-Space Station-Keeping Perform-
C07-201 Comparative Flight Tests with and ance of a Large High-Altitude Notional Airship
Without Tip Tanks Wind Power Computational Fluid Dynamics
C07-142 Response Surface Methods for Efficient 07-177 Navier-Stokes Analysis of Airfoils with
C07-063 Two-Dimensional Wind Tunnel and
Complex Aircraft Configuration Aerodynamic Gurney Flap
Computational Investigation of a Microtab
Characterization Modified Airfoil C07-185 Computational Study of Submerged Air
Inlet Performance Improvement Using Vortex
C07-023 Design and Numerical Optimization of
Generators
Uninhabited and Unmanned Air Vehicles Thick Airfoils Including Blunt Trailing Edges
07-149 Effect of Acoustic Slat Modifications on
C07-150 Plasma Actuators for Hingeless Aero- Aerodynamic Properties of High-Lift Systems
FLIGHT SIMULATOR SYSTEMS
dynamic Control of an Unmanned Air Vehicle C07-113 Multipoint Aerodynamic Design of
C07-132 Design and Testing of a Pneumatic Wing-Body Configurations for Minimum Drag
Human-Computer Interactions
Telescopic Wing for Unmanned Aerial Vehicles C07-015 Robust Design of an Aerodynamic
C07-189 Aerodynamic Characteristics of a Free- C07-085 Cueing System for Near-Term Imple- Compensation Pitot-Static Tube for Supersonic
Wing Tilt-Body Unmanned Aerial Vehicle mentation of Aircraft Noise Abatement Approach Aircraft
C07-039 Exploratory Investigation of Geometry Procedures C07-107 Automatic Transition Prediction and
Effects on Gurney Flap Performance C07-108 Motion-Visual Phase-Error Detection in Application to Three-Dimensional High-Lift
C07-219 Aerodynamic Control of Using Wind- a Flight Simulator Configurations
C07-179 Application of CFD-Based Unsteady
ward-Surface Plasma Actuators on a Separation
MEMS Forces for Efficient Aeroelastic Stability Analyses
Ramp
C07-218 Effect of Thrust-Vectoring Jets on Delta C07-025 Design Guidelines of Rotary Wings in C07-195 Analysis of Wind Tunnel Wall Interfer-
Hover for Insect-Scale Micro Air Vehicle ence Effects on Subsonic Unsteady Airfoil Flows
Wing Aerodynamics
Applications C07-226 New Computational Procedure for
C07-197 Development and Testing of the Mentor
Incorporating Computational Fluid Dynamics
Flapping-Wing Micro Air Vehicle FLUID DYNAMICS into Sonic Boom Prediction
C07-235 Optimum Aeroelastic Design of a C07-239 Improving the Stability and Efficiency
Flapping Wing Aeroacoustics of the Pseudocompressibility Method
C07-112 Aerodynamic Characteristics of Para- C07-141 Evaluation of a Simplified Grid Treat-
C07-165 Prediction of Hovering Rotor Noise
drogue Assembly in an Aerial Refueling System ment for Oscillating Trailing-Edge Control
Based on Reynolds-Averaged Navier-Stokes
Surfaces
Simulation
Vibration C07-161 Influence of Vortex Core on Wake C07-158 Optimization of Aifoil Flow Control
Using a Genetic Algorithm with Diversity Control
C07-045 Fast Identification and Characterization Vortex Sound Emission
C07-180 Optimum Shape Design for Unsteady
of Nonlinearities in Experimental Modal Analysis C07-226 New Computational Procedure for Three-Dimensional Viscous Flows Using a
of Large Aircraft Incorporating Computational Fluid Dynamics Nonlinear Frequency-Domain Method
into Sonic Boom Prediction
C07-227 Distributed Rate-Dependent Elastoslide C07-208 High Resolution Turbulence Treatment
Model for Elastomeric Lag Dampers Boundary Layers and Heat Transfer- of F/A-18 Tail Buffet
Laminar C07-217 Effect of Streamwise Slots on the Drag
Weather Hazards C07-070 Numerical Simulation of Airfoil Ther- of a Transonic Projectile
mal Anti-Ice Operation, Part 1: Mathematical C07-213 Aerodynamic Characteristics of Bodies
C07-183 Measured Statistics of Multicomponent
Modeling of Revolution at Near-Sonic Speeds
Gust Patterns in Atmospheric Turbulence
C07-071_ Numerical Simulation of Airfoil Ther- C07-011 Automatic Transition Prediction and
C07-029 Calibration and Use of Goodrich Model mal Anti-Ice Operation, Part 2: Implementation Application to Three-Dimensional Wing Confi-
0871FA Ice Detectors in Icing Wind Tunnels and Results gurations
C07-027 Current Experimental Basis for Model- C07-018 Computational Analysis on Flow
ing Ice Accretions on Swept Wings Boundary Layers and Heat Transfer- Through Transition s-Diffusers: Effect of Inlet
C07-093 Local and Total Density Measurements Turbulent Shape
in Ice Shapes 07-071 Numerical Simulation of Airfoil Ther- C07-017 Comparison of Reynolds-Averaged
C07-212 Investigation of Relative Humidity and mal Anti-Ice Operation, Part 2: Implementation Navier-Stokes Simulations of Multi-Element
Induced-Vortex Effects on Aircraft Icing and Results High-Lift Configurations
2096 J. AIRCRAFT, VOL. 44, NO. 6: 2007 INDEX
C07-220 Drag Decomposition-Based Adaptive C07-106 Predicting Maximum Lift Coefficient C07-152 Experimental Investigation of Unsteady
Mesh Refinement for Twisted Wings Using Computational Fluid Flow Separation on a Maneuvering Axisymmetric
C07-092 Extension of Projectile Range Using Dynamics Body
Oblique-Wing Concept 07-050 Reynolds-Averaged Navier-Stokes C07-180 Optimum Shape Design for Unsteady
C07-212 Investigation of Relative Humidity and Analysis of Zero Efflux Flow Control over a Three-Dimensional Viscous Flows Using a
Induced-Vortex Effects on Aircraft Icing Hump Model Nonlinear Frequency-Domain Method
C07-225 Error Quantification for Computational C07-105 Predicting Maximum Lift Coefficient C07-161 Influence of Vortex Core on Wake
Aerodynamics Using an Error Transport Equation for Twisted Wings Using Lifting-Line Theory Vortex Sound Emission
C07-134 Unsteady Thermodynamic Computa- C07-020 Robust Multivariable Closed-Loop C07-103 Effect of Oscillation on Boundary-Layer
tional Fluid Dynamics Simulations of Aircraft Control of a Turbulent Backward-Facing Step Development with Adverse Pressure Gradients
Wing Anti-Icing Operation Flow C07-135 Computational Fluid Dynamics Study
C07-098 Drag Prediction in Transitional Flow C07-224 Upstream Blowing Jet on Transonic of Three-Dimensional Dynamic Stall of Various
Over Airfoils Convex-Corner Flow Planform Shapes
C€07-138 Analysis Method for Inertial Particle 07-221 Forebody Geometry Effects on the Flow C07-235 Optimum Aeroelastic Design of a
Separator of a Blunt-Nose Projectile at High Alpha Flapping Wing
C07-047 Transonic Computational Fluid Dynam- C07-102 Active Separation Control on the Flap of C07-215 Unsteady Numerical Simulation of
ics Calculations on Preproduction F/A-18E for a Two-Dimensional Generic High-Lift Configu- Wings with Flaperon Flying Over Nonplanar
Stability and Control ration Ground Surface
C07-187 Cartesian-Like Grids Using a Novel C07-152 Experimental Investigation of Unsteady C07-178 Compressible Unsteady Vortex Lattice
Grid-Stitching Algorithm for Viscous Flow Flow Separation on a Maneuvering Axisymmetric Method for Arbitrary Two-Dimensional Motion
Computations Body of Thin Profiles
C07-118 Comparison of Computational Fluid C07-204 Passive Control of Bluff Body Using C07-050 Reynolds-Averaged Navier-Stokes
Dynamics Approaches for Simulating Weapons Stepped-Nose Obstacle Analysis of Zero Efflux Flow Control over a
Bay Flow Hump Model
C07-170 Lift and Drag Characteristics of a Subsonic Flow C07-118 Comparison of Computational Fluid
Blended-Wing Body Aircraft C07-103 Effect of Oscillation on Boundary-Layer Dynamics Approaches for Simulating Weapons
C07-076 Enhancements of the Cut-Paste Algo- Development with Adverse Pressure Gradients Bay Flow
rithm in Overlapping Grid Generation C07-083 Generalized Empirical Airfoil Stagna- C07-111 Dynamic Wing Airloads with Higher
C07-001 Aerodynamic Modeling of Morphing tion Point Location Prediction Harmonic Flap Motion
Wings Using an Extended Lifting-Line Analysis C07-149 Effect of Acoustic Slat Modifications on C07-034 Effect of Flap Motion on Unsteady
C07-055 Computational Analysis of Wake Vor- Aerodynamic Properties of High-Lift Systems Aerodynamic Loads
tices Generated by Notched Wings C07-195 Analysis of Wind Tunnel Wall Interfer- C07-031 Drag and Flutter Characteristics of Loop
C07-030 Effect of a Porosity Strength on Drag ence Effects on Subsonic Unsteady Airfoil Flows Membranes
Reduction of a Transonic Projectile C07-244 Experimental Studies on Unsteady
C07-133 Multidisciplinary Design Optimization Lateral Blowing on NACA 0012
Vortices
and Data Mining for Transonic Regional-Jet Wing C07-017 Comparison of Reynolds-Averaged
C07-106 Predicting Maximum Lift Coefficient Navier-Stokes Simulations of Multi-Element C07-095 Characterization of Aircraft Wake
for Twisted Wings Using Computational Fluid High-Lift Configurations Vortices by Airborne Coherent Doppler Lidar
Dynamics C07-202 Two Aspects of Use of Full- and Partial- C07-055 Computational Analysis of Wake Vor-
C07-005 Computational Aeroelastic Analysis of Span Gurney Flaps tices Generated by Notched Wings
Store-Induced Limit-Cycle Oscillation C07-225 Error Quantification for Computational C07-026 Effect of a Winglet on Normal Blade-
Aerodynamics Using an Error Transport Equation Vortex Interaction
Hypersonic Flow 07-082 Aerodynamic Characterization of Grid C07-054 Effect of Swirl Flows in Aeronautical
C07-076 Enhancements of the Cut-Paste Algo- Fins at Subsonic Speeds Mix Manifolds
rithm in Overlapping Grid Generation C07-023 Design and Numerical Optimization of C07-100 Development of a Trailing Vortex
Thick Airfoils Including Blunt Trailing Edges Formed with Spanwise Tip Jets
Inlet, Nozzle, Diffuser, and Channel
C07-202 Two Aspects of Use of Full- and Partial-
Flows Transonic Flow Span Gurney Flaps
C07-084 Tradeoffs in Jet Inlet Design: A C07-041 Iterative Response Surface Based C07-212 Investigation of Relative Humidity and
Historical Perspective Optimization Scheme for Transonic Airfoil Induced-Vortex Effects on Aircraft Icing
C07-185 Computational Study of Submerged Air Design C07-218 Effect of Thrust-Vectoring Jets on Delta
Inlet Performance Improvement Using Vortex C07-03v Effect of a Porosity Strength on Drag Wing Aerodynamics
Generators Reduction of a Transonic Projectile C07-009 Dynamics of Corotating Vortex Fila-
C07-047 Transonic Computational Fluid Dynam- ments Part 2: Experimental Results
Jets, Wakes, and Viscid-Inviscid Flow ics Calculations on Preproduction F/A-18E for C07-135 Computational Fluid Dynamics Study
Interactions Stability and Control of Three-Dimensional Dynamic Stall of Various
C07-100 Development of a Trailing Vortex C07-016 Effect of Microvortex Generators On Planform Shapes
Formed with Spanwise Tip Jets Seperated Normal Shock/ Boundary Layer C07-062 Wake of Transport Flying Wings
C07-009 Dynamics of Corotating Vortex Fila- Interactions C07-079 Trailing Vortex Filament: A Novel
ments Part 2: Experimental Results C07-224 Upstream Blowing Jet on Transonic Similarity Analysis
C07-069 Adaptive Compensation Control of Convex-Corner Flow C07-086 Ultrasonic Method for Aircraft Wake
Synthetic Jet Actuator Arrays for Airfoil Virtual C07-092 Extension of Projectile Range Using Vortex Detection
Shaping Oblique-Wing Concept C07-024 Wake Vorticity Measurements for Low
C07-220 Drag Decomposition-Based Adaptive Aspect Ratio Wings at Low Reynolds Number
Plasmadynamics and MHD Mesh Refinement C07-053 Wake Vortex Model for Real-Time
C07-058 Autonomous Sensing and Control of C07-213 Aerodynamic Characteristics of Bodies Flight Simulation Based on Large Eddy
Wing Stall Using a Smart Plasma Slat of Revolution at Near-Sonic Speeds Simulation
C07-161 Influence of Vortex Core on Wake
Separated Flows Unsteady Flows Vortex Sound Emission
C07-035 Flow Control by Spanwise Blowing ona C07-186 Streamwise Vorticity in Simple Me- C07-036 Planform Variations and Aerodynamic
NACA 0012 chanical Flapping Wings Efficiency of Movable Tip Strakes
J. AIRCRAFT, VOL. 44, NO. 6: 2007 INDEX 2097
C07-186 Streamwise Vorticity in Simple Me- Flight Mechanics INTERDISCIPLINARY TOPICS
chanical Flapping Wings
C07-182 Adaptive Stochastic Filtering for Online
C07-214 Effects of Strake Planform Change on Aircraft Flight Path Reconstruction Aerospace Management
Vortex Flow of a Double-Delta Wing
C07-099 Post-Stall Motions Evolving Toward C07-115 Failure Forecasting of Aircraft Air
C07-203 Effect of Leading-Edge Form on Chaos Conditioning/Cooling Pack with Field Data
Performance of Wing-Movable Tip Strake
Configurations Handling Qualities Analytical and Numerical Methods
C07-246 Reduced-Order-Model-Based Flutter C07-221 Forebody Geometry Effects on the Flow C07-184 Application of Probability Methods to
Analysis at High Angle of Attack of a Blunt-Nose Projectile at High Alpha Assess Airframe Crash Modeling Uncertainty
C07-125 Method for Multivariate Analysis with
GUIDANCE, CONTROL, AND Intelligent Control Small Sample in Aircraft Cost Estimation
DYNAMICS TECHNOLOGY C07-057 Piezoelectric Transducer Actuated C07-231 Analysis of Visual Cues During Landing
Leading Edge De-Icing with Simultaneous Shear Phase by Using Neural Network Modeling
Aircraft Dynamics and Impulse Forces C07-064 Analytical Two-Dimensional Model of
a Hybrid (Bolted/Bonded) Single-Lap Joint
C07-123 Dynamic Coupling of the KC-135
Navigation C07-003 Analysis of the Airframe Noise of an
Tanker and Boom for Modeling and Simulation
C07-181 Nonlinear Flight Dynamics of Very 07-205 In-Flight GPS-Signal-Reception A320/A321 with a Parametric Method
C07-178 Compressible Unsteady Vortex Lattice
Flexible Aircraft Anomalies of Helicopters
Method for Arbitrary Two-Dimensional Motion
C07-131 Modeling and Flight Control of Large- C07-160 Magnetometer Autocalibration Lever- of Thin Profiles
Scale Morphing Aircraft aging Measurement Locus Constraints
C07-110 Neuro-Fuzzy Techniques for the Air- C07-194 Autonomous Airborne Refueling of Atmospheric and Space Sciences
Data Sensor Calibration Unmanned Air Vehicles Using the Global C07-093 Local and Total Density Measurements
Positioning System
Aircraft Guidance C07-193 Assessment of Ionosphere Spatial in Ice Shapes
C07-027 Current Experimental Basis for Model-
C07-010 Implementing Time-Based Spacing for Decorrelation for Global Positioning System-
ing Ice Accretions on Swept Wings
Decelerating Approaches Based Aircraft Landing Systems
C07-183 Measured Statistics of Multicomponent
C07-193 Assessment of Ionosphere Spatial
Gust Patterns in Atmospheric Turbulence
Decorrelation for Global Positioning System- Optimization Techniques
Based Aircraft Landing Systems C07-101 Multi-Objective Aerodynamic Explora-
tion of Elements’ Setting for High-Lift Airfoil CAD/CAM
Aircraft Stability and Control
Using Kriging Model C07-136 Automated Aircraft Sheet Metal Com-
07-047 Transonic Computational Fluid Dynam- C07-022 Modelization and Kinematics Optimi- ponent Production Technologies
ics Calculations on Preproduction F/A-18E for zation for a Flapping-Wing Microair Vehicle
Stability and Control Environmental Effects
C07-131 Modeling and Flight Control of Large- Signal Processing C07-140 Methodology for Optimizing Parame-
Scale Morphing Aircraft C07-143 Experimental Training and Validation ters of Noise-Abatement Approach Procedures
C07-033 Method Based on Chebyshev Polyno- of a System for Aircraft Acoustic Signature C07-241 Specific Weight: A Challenge for a Fuel-
mials for Aerservoelastic Interactions on an F/A- Identification Cell-Powered Electric Helicopter
18 Aircraft
C07-199 Overview on Contrail and Cirrus Cloud
C07-099 Post-Stall Motions Evolving Toward State Estimation Avoidance Technology
Chaos
C07-182 Adaptive Stochastic Filtering for Online
C07-207 Experimental Study of a Micro Air Human Factors
Aircraft Flight Path Reconstruction
Vehicle with a Rotatable Tail C07-108 Motion-Visual Phase-Error Detection in
Artificial Intelligence Structural Control a Flight Simulator
C07-085 Cueing System for Near-Term Imple-
C07-110 Neuro-Fuzzy Techniques for the Air- C07-087 Experimental Evaluation of an Ad- mentation of Aircraft Noise Abatement Approach
Data Sensor Calibration vanced Buffet Suppression System on Full Scale Procedures
F/A-18 Fin
Autonomous Vehicles C07-129 Morphing Wing Flight Control Via C07-048 Perception Model Analysis of Flight
Simulator Motion for a Decrab Maneuver
C07-194 Autonomous Airborne Refueling of Postbuckled Precompressed Piezoelectric Actua-
C07-122 Semi-Active Control of Vertical Strok-
Unmanned Air Vehicles Using the Global tors
ing Helicopter Crew Seat for Enhanced
Positioning System
System Identification Crashworthiness
Control System Design C07-231 Analysis of Visual Cues During Landing
C07-014 Volterra Kernel Extrapolation for Mod-
C07-134 Unsteady Thermodynamic Computa- eling Nonlinear Aeroelastic Systems at Novel Phase by Using Neural Network Modeling
tional Fluid Dynamics Simulations of Aircraft Flight Conditions Lasers and Laser Applications
Wing Anti-Icing Operation C07-182 Adaptive Stochastic Filtering for Online C07-198 Flight Test Evaluation of a Helicopter
Control System Sensors Aircraft Flight Path Reconstruction Airborne Lidar
C07-110 Neuro-Fuzzy Techniques for the Air- Trajectory Optimization C07-042 Geometric Properties of Parachutes
Data Sensor Calibration Using 3-D Laser Scanning
C07-044 Study of Near-Optimal Endurance- C07-095 Characterization of Aircraft Wake
Control Theory Maximizing Periodic Cruise Trajectories Vortices by Airborne Coherent Doppler Lidar
C07-020 Robust Multivariable Closed-Loop C07-010 Implementing Time-Based Spacing for
Multidisciplinary Design Optimization
Control of a Turbulent Backward-Facing Step Decelerating Approaches
Flow C07-046 Ranking Based Uncertainty Quantifica-
C07-234 Assessment of Critical Fuel Configura- UAVs tion for a Multifidelity Design Approach
tions Using Robust Flutter Analysis C07-160 Magnetometer Autocalibration Lever- C07-133 Multidisciplinary Design Optimization
aging Measurement Locus Constraints and Data Mining for Transonic Regional-Jet Wing
Dynamics C07-194 Autonomous Airborne Refueling of C07-146 System-of-Systems Inspired Aircraft
C07-123 Dynamic Coupling of the KC-135 Unmanned Air Vehicles Using the Global Sizing and Airline Resource Allocation via
Tanker and Boom for Modeling and Simulation Positioning System Decomposition
2098 J. AIRCRAFT, VOL. 44, NO. 6: 2007 INDEX
C07-176 Coupled Vehicle Design and Network Energy Conservation 07-007 Active Control of Wing Flutter Using
Flow Optimization for Air Transportation C07-044 Study of Near-Optimal Endurance- Piezoactuated Surface
Systems Maximizing Periodic Cruise Trajectories C07-240 Bending-Torsion Divergence of a
C07-209 Design “Feasilization” Using Knowl- Clamped-Clamped Composite Wing
edge-Based Engineering and Optimization Tech- Fuel Cells C07-236 Parametric Studies on Ground Vibration
niques C07-241 Specific Weight: A Challenge for a Fuel- Test Modeling for Highly Flexible Aircraft
C07-235 Optimum Aeroelastic Design of a Cell-Powered Electric Helicopter C07-181 Nonlinear Flight Dynamics of Very
Flapping Wing Flexible Aircraft
Ramjets and Scramjets
C07-126 Interval Analysis-Based Optimum De- C07-i17 Reduced Order Aerodynamic Model for
C07-242 Evaluation of Effectiveness of Periodic
sign of Wing Structures Under Taxiing Loads Aeroelastic Analysis of Complex Configurations
C07-113 Multipoint Aerodynamic Design of Flight by a Hypersonic Vehicle in Incompressible Flow
Wing-Body Configurations for Minimum Drag Reciprocating Machinery C07-246 Reduced-Order-Model-Based Flutter
C07-171 Preliminary Aerostructural Optimiza- Analysis at High Angle of Attack
C07-166 Performance of Articulated Flapping
tion of a Large Business Jet
Wings with Partial Leading-Edge Suction Dynamic Model Analysis
C07-158 Optimization of Aifoil Flow Control
Using a Genetic Algorithm with Diversity Control Wind Power C07-065 Finite Element Modeling of a Bird
Reliability, C07-222. Aerodynamic and Mission Performance Striking an Engine Fan Blade
Maintainability, and Logistics Support of a Winged Balloon Guidance System C07-006 Transient and Limit Cycle Simulation of
C07-115 Failure Forecasting of Aircraft Air a Nonlinear Aeroelastic System
Conditioning/Cooling Pack with Field Data REAL-TIME SYSTEMS Flexible and Active Structures
Research Facilities and Instrumentation Software Engineering C07-087 Experimental Evaluation of an Ad-
C07-206 Sensitivity of Aircraft Performance to C07-053 Wake Vortex Model for Real-Time vanced Buffet Suppression System on Full Scale
Icing Parameter Variations Flight Simulation Based on Large Eddy F/A-18 Fin
C07-029 Calibration and Use of Goodrich Model Simulation C07-130 Investigation of Self-Resetting Active
0871FA Ice Detectors in Icing Wind Tunnels Multistable Laminates
Systems Engineering C07-144 Topology Synthesis of Distributed
Safety
C07-209 Design “Feasilization” Using Knowl- Actuation Systems for Morphing Wing Structures
C07-057 Piezoelectric Transducer Actuated edge-Based Engineering and Optimization Tech- C07-007 Active Control of Wing Flutter Using
Leading Edge De-Icing with Simultaneous Shear niques Piezoactuated Surface
and Impulse Forces C07-042 Geometric Properties of Parachutes
C07-196 Hybrid II Numerical Model for Aircraft SPACE TECHNOLOGY Using 3-D Laser Scanning
Seat Crash Performance Assessment C07-069 Adaptive Compensation Control of
C07-231 Analysis of Visual Cues During Landing Global Positioning System Synthetic Jet Actuator Arrays for Airfoil Virtual
Phase by Using Neural Network Modeling C07-205 In-Flight GPS-Signal-Reception Shaping
C07-097 Reliability-Based Aircraft Structural Anomalies of Helicopters C07-129 Morphing Wing Flight Control Via
Design Pays, Even with Limited Statistical Data C07-193 Assessment of Ionosphere Spatial Postbuckled Precompressed Piezoelectric Actua-
Sensor Systems Decorrelation for Global Positioning System- tors
Based Aircraft Landing Systems
C07-015 Robust Design of an Aerodynamic Materials Structural Properties
Compensation Pitot-Static Tube for Supersonic Spacecraft Structural Configuration, C07-051 Effect of Hydrogen and Hold Time on
Aircraft Design, and Analysis the Lifetime of AF1410 Steel
C07-143 Experimental Training and Validation C07-019 A Tensile Stress Concentration Equa- C07-232 Bending of Bonded Composite Repairs
of a System for Aircraft Acoustic Signature tion for Countersunk Holes for Aluminum Aircraft Structures: A Design
Identification Spacecraft Test and Evaluation Study
C07-029 Calibration and Use of Goodrich Model
0871FA Ice Detectors in Icing Wind Tunnels C07-049 Advancements in Aircraft Model Force Structural Composite Materials
and Attitude Instrumentation by Integrating C07-155 Probabilistic Approach to Damage
LAUNCH VEHICLE AND Statistical Methods Tolerance Design of Aircraft Composite Struc-
tures
MISSILE (LV/M) TECHNOLOGY STRUCTURAL MECHANICS
C07-130 Investigation of Self-Resetting Active
AND MATERIALS Multistable Laminates
Aerodynamics
C07-130 Investigation of Self-Resetting Active
C07-082 Aerodynamic Characterization of Grid Aeroelasticity and Control Multistable Laminates
Fins at Subsonic Speeds C07-087 Experimental Evaluation of an Ad- C07-114 Fuzzy-Logic-Based Health Monitoring
Configuration Design vanced Buffet Suppression System on Full Scale and Residual-Life Prediction for Composite
F/A-18 Fin Helicopter Rotor
C07-046 Ranking Based Uncertainty Quantifica- C07-006 Transient and Limit Cycle Simulation of C07-157 Doubly Curved Anisotropic Sandwich
tion for a Multifidelity Design Approach
a Nonlinear Aeroelastic System Panels: Modeling and Free Vibration
C07-013 Design of Waverider Configuration with C07-094 Two-Dimensional Unsteady Aerody- C07-240 Bending-Torsion Divergence of a
High Lift-Drag Ratio
namic Application to Higher Harmonic Control Clamped-Clamped Composite Wing
Simulation Test Data C07-188 Thermal Buckling and Nonlinear Flutter
C07-046 Ranking Based Uncertainty Quantifica- C07-119 Surface Splines Generalization and Behavior of Functionally Graded Material Panels
Large Deflection Interpolation
tion for a Multifidelity Design Approach 07-137 Supersonic Nonlinear Panel Flutter Structural Design
Suppression Using Shape Memory Alloys C07-209 Design “Feasilization” Using Knowl-
PROPULSION C07-005 Computational Aeroelastic Analysis of edge-Based Engineering and Optimization Tech-
Store-Induced Limit-Cycle Oscillation niques
Airbreathing Propulsion
C07-002 Gust Loads Alleviation Using Special C€07-173 Analysis and Design of Robust Helium
C07-018 Computational Analysis on Flow Control Surfaces Aerostats
Through Transition s-Diffusers: Effect of Inlet C07-067 Case of Explosive Wing-Flaperon C07-032 Riveting Process Induced Residual
Shape Flutter Stresses Around Solid Rivets in Mechanical Joints
J. AIRCRAFT, VOL. 44, NO. 6: 2007 INDEX 2099
C07-040 Analysis of the Effects of Interference C07-157 Doubly Curved Anisotropic Sandwich Structural Optimization
and Sealant on Riveted Lap Joints Panels: Modeling and Free Vibration C07-097 Reliability-Based Aircraft Structural
C07-019 A Tensile Stress Concentration Equa- C07-229 Lateral Response of Nonlinear Nose- Design Pays, Even with Limited Statistical Data
tion for Countersunk Holes Wheel Landing Gear Models with Torsional Free C07-126 Interval Analysis-Based Optimum De-
C07-144 Topology Synthesis of Distributed Play sign of Wing Structures Under Taxiing Loads
Actuation Systems for Morphing Wing Structures C07-230 Lateral Response of Nose-Wheel Land- C07-088 Investigation of Membrane Actuation
C07-097 Reliability-Based Aircraft Structural ing Gear System to Ground-Induced Excitation for Roll Control of a Micro Air Vehicle
Design Pays, Even with Limited Statistical Data C07-057 Piezoelectric Transducer Actuated C07-144 Topology Synthesis of Distributed
C07-155 Probabilistic Approach to Damage Leading Edge De-Icing with Simultaneous Shear Actuation Systems for Morphing Wing Structures
Tolerance Design of Aircraft Composite Struc- and Impulse Forces C07-154 Structural Optimization of a Joined
tures C07-073 Cantilevered Plate Rayleigh—Ritz Trial Wing Using Equivalent Static Loads
C07-153 Residual Strength of Panels with Cracks Function Selection for von Karman’s Plate C07-133 Multidisciplinary Design Optimization
Based on a Plastic Hinge Equations and Data Mining for Transonic Regional-Jet Wing
C07-232 Bending of Bonded Composite Repairs C07-227 Distributed Rate-Dependent Elastoslide
for Aluminum Aircraft Structures: A Design Model for Elastomeric Lag Dampers Structural Stability
Study C07-091 Unstable, Cyclically Symmetric and
Stable, Asymmetric Pumpkin-Balloon Configu-
Structural Durability (Including Fatigue, Structural Finite Elements
rations
Fracture, and Environmental C07-091 Unstable, Cyclically Symmetric and C07-130 Investigation of Self-Resetting Active
Degradation) Stable, Asymmetric Pumpkin-Balloon Configu- Multistable Laminates
C07-232 Bending of Bonded Composite Repairs rations
THERMOPHYSICS AND HEAT
for Aluminum Aircraft Structures: A Design C07-065 Finite Element Modeling of a Bird
Study Striking an Engine Fan Blade TRANSFER
C07-153 Residual Strength of Panels with Cracks C07-196 Hybrid If] Numerical Model for Aircraft Aerothermodynamics/Thermal Protection
Based on a Plastic Hinge Seat Crash Performance Assessment
C07-138 Analysis Method for Inertial Particle
C07-155 Probabilistic Approach to Damage C07-040 Analysis of the Effects of Interference
Separator
Tolerance Design of Aircraft Composite Struc- and Sealant on Riveted Lap Joints
tures C07-032 Riveting Process Induced Residual Computational Heat Transfer
C07-090 Corrosion Pillowing in Aircraft Fuse- Stresses Around Solid Rivets in Mechanical Joints C07-138 Analysis Method for Inertial Particle
lage Lap Joints C07-233 Investigation of the Effect of Metallic Separator
C07-089 Fatigue Testing of a Stiffened Lap Joint Fuselage Dents on Compressive Failure Loads C07-134 Unsteady Thermodynamic Computa-
Curved Fuselage Structure C07-188 Thermal Buckling and Nonlinear Flutter tional Fluid Dynamics Simulations of Aircraft
C07-051 Effect of Hydrogen and Hold Time on Behavior of Functionally Graded Material Panels Wing Anti-Icing Operation
the Lifetime of AF1410 Steel C07-233 Investigation of the Effect of Metallic C07-076 Enhancements of the Cut-Paste Algo-
C07-032 Riveting Process Induced Residual Fuselage Dents on Compressive Failure Loads rithm in Overlapping Grid Generation
Stresses Around Solid Rivets in Mechanical Joints C07-071 Numerical Simulation of Airfoil Ther-
C07-233 Investigation of the Effect of Metallic Structural Modeling mal Anti-Ice Operation, Part 2: Implementation
Fuselage Dents on Compressive Failure Loads and Results
C07-157 Doubly Curved Anisotropic Sandwich
Structural Dynamics and Panels: Modeling and Free Vibration C07-070 Numerical Simulation of Airfoil Ther-
mal Anti-Ice Operation, Part 1: Mathematical
Characterization C07-064 Analytical Two-Dimensional Model of
Modeling
C07-228 Closed-Form Analytical Solution for the a Hybrid (Bolted/Bonded) Single-Lap Joint
Shimmy Instability of Nose-Wheel Landing Gears C07-073 Cantilevered Plate Rayleigh-Ritz Trial Thermal Control
C07-236 Parametric Studies on Ground Vibration Function Selection for von Karman’s Plate C07-054 Effect of Swirl Flows in Aeronautical
Test Modeling for Highly Flexible Aircraft Equations Mix Manifolds
2100 J. AIRCRAFT, VOL. 44, NO. 6: 2007 INDEX
Author Index
Aaron, Kim M., C07-222 Brakke, Kenneth A., C07-091 Durgin, William W., C07-086 Ho, Nhut Tan, C07-085, C07-140
Abdo, Mohammed, C07-171 Brenner, Martin J., C07-014 Elzey, Michael B., C07-012 Hodges, Dewey H., C07-236,
Abdulrahim, Mujahid, C07-088 Bridges, David H., C07-191 Enge, Per, C07-193 C07-240
Abe, Takashi, C07-025 Britcher, Colin, C07-145 Epstein, Boris, C07-113 Holden, Harriet A., C07-016
Aboelkassem, Yasser, C07-079 Broeren, Andy P., C07-206 Eshelby, Martin, C07-043 Holeman, Dennis, C07-197
Acar, Erdem, C07-097 Broughton, Howard, C07-093 Farnsworth, John, C07-072 Holloway, A. Gordon L., C07-100
Agarwal, Guarav, C07-039 Bryant, Robert G., C07-130 Favier, D., C07-135 Hong, YoungSun, C07-186
Aghanajafi, Cyrus, C07-190 Burkholder, Jason O., C07-069 Figueira da Silva, Luis Fernando, Hosder, Serhat, C07-152
Ahmed, Abubaker, C07-089 Bussoletti, John E., C07-213 C07-185 Hosman, Ruud J.A.W., C07-048
Al-Ajmi, Mohammed, C07-188 Campbell, Scot E., C07-206 Filippone, Antonio, C07-030, Howle, Laurens E., C07-169
Alderliesten, René, C07-032 Campos, Luis M. B. C., C07-061 C07-031, C07-200, C07-217 Hu, Hui, C07-245
Al-Garni, Abdullah, C07-115 Canfield, R.A., C07-154 Finley, Tom D., C07-049 Hu, Wei, C07-227
Al-Garni, Ahmad Z., C07-115, Carruthers, Anna C., C07-031 Firooz-Abadi, R. D., C07-117 Hua, Jun, C07-134
C07-138 Castelletti, Luigi-M L., C07-196 Fonov, Vladamir, C07-170 Huang, George, C07-158
Allen, Christian B., C07-163 Cavallo, Peter A., C07-225 Fracasso, Emanuele, C07-196 Huang, Liang, C07-158
Allerton, David J., C07-053 Celis Pérez, César, C07-185 Gaines, Vatanna, C07-093 Huebsch, Wade W., C07-212
Alley, Nicholas R., C07-105, Cesnik, Carlos E.S., C07-181 Gaitonde, Ann L., C07-163 Huet, Jacques, C07-064
C07-106 Chakrabartty, Sunil Kumar, Galbraith, R. A. McD., C07-127, Hureau, Jacques, C07-054
Altman, Aaron, C07-024, C07-083, C07-177 C07-135, C07-216 Ibrahim, Ahmed, C07-030, C07-217
C07-186 Chang, Chong-Seok, C07-236 Gandhi, Farhan, C07-172 Ibrahim, Hesham Hamed, C07-188
Amir, Mohammad, C07-103 Charca, Samuel, C07-051 Ganguli, Ranjan, C07-114 Ifju, Peter, CO7-088
Amitay, Michael, C07-072 Chen, Chang, C07-109 Garcia, Ephrahim, C07-001 Igarashi, Hirofumi, C07-245
Anghileri, Marco, C07-196 Chen, Ping-Chih, C07-092 Garcia-Alegre, Maria del Carmen, Imamura, Taro, C07-017
Apostolyuk, Vladislav, C07-168 Chen, Yong, C07-087 C07-241 Inman, Daniel J., CO7-131, C07-174
Asaka, Kimio, C07-198 Chiba, Kazuhisa, C07-133 Gebbie, David A., C07-170 Inoyama, Daisaku, C07-144
Atre, Amarendra P., C07-040 Choi, Young-Tai, C07-122 Gebre-Egziabher, Demoz, C07-160 In ’t Veld, Alexander C., C07-010
Attar, Peter Joseph, C07-073 Cho, Jeonghyun, C07-215 Gerontakos, P., C07-111 Isikveren, Askin T., C07-171
Awerbuch, Jonathan, C07-089 Cho, Jinsoo, C07-215 Ghaly, Wahid S., C07-098 Isogai, Koji, C07-235
Ayachit, P. V., C07-136 Chung, Hyoung S., C07-214 Ghenaiet, Adel, C07-210 Jamal, Ahmad, C07-115
Azevedo, Joao Luiz F., C07-179 Chung, James J., C07-047 Ghigliazza, Horacio H., C07-062 Jameson, Antony, C07-180
Babinsky, Holger, C07-016 Chung, Kung-Ming, C07-224 Gili, Piero A., C07-110 Jeck, Richard K., C07-029
Badcock, Ken J., C07-141, C07-135 Ciuryla, Marcus, C07-072 Goege, Dennis, C07-045 Jeong, Shinkyu, C07-101
Bae, Jae-Sung, C07-066, C07-131 Clarke, John-Paul, C07-010, Goes, Luiz Carlos Sandoval, Jiang, Ping, C07-218
Baeder, James D., C07-195 C07-085, C07-140 C07-182 Johari, Hamid, C07-086
Baginski, Frank E., C07-091 Clark, Randal J., C07-232 Goto, Yuichiro, C07-077 Johnson, Wayne, C07-056
Baker, J. P., C07-063 Corke, Thomas C., C07-058, Gould, Ronald W., C07-090 Johnson, William S., C07-040
Bakuckas, John, C07-089 C07-150, C07-219 Grant, Peter R., C07-108 Johnston, Christopher O., C07-174
Balakrishnan, N., C07-187 Cotoi, lulian, C07-033 Grant, Richard John, C07-055 Jones, Dorian, C07-163
Barakos, George N., C07-135 Coton, F. N., C07-127, C07-135, Green, Bradford E., C07-047 Jones, John G., C07-183
Barlow, Jewel B., C07-189 C07-216 Groen, Eric L., C07-048 Joo, James, C07-144
Barrett, Ron M., C07-129 Couch, Mark A., C07-094 Guinea, Domingo, C07-241 Joo, Wandon, C07-116
Barros Ferreira, Sandro, C07-185 Crafton, Jim, C07-170 Guinea, Domingo M., C07-241 Katyeke, Fassi, C07-171
Basaran, Emre, C07-112 Crossley, William A., C07-146 Guo, Xinyun, C07-137 Kamman, James W., C07-112
Basha, Wassim, C07-098 Crowther, William J., C07-128 Gursul, Ismet, C07-218 Kanazaki, Masahiro, C07-101
Batista de Jesus, Antonio, C07-185 Cummings, Russell M., C07-208 Haddadpour, Hassan, C07-117 Kanda, Takeshi, C07-242
Battipede, Manuela, C07-110 Dacca, Edmond, C07-026 Haftka, Raphael T., C07-097 Kang, Hantae, C07-083
Behbahani-Nejad, Morteza, Daneshmand, Saeed, C07-190 Hamner, Marvine P., C07-012 Kaplan, Sergey, C07-024
C07-117 Datta-Barua, Seebany, C07-193 Han, Cheolheui, C07-121, C07-174 Karpel, Moti, C07-002
Bellinger, Nicholas C., C07-090, Dayananda, G. N., C07-175 Han, Zhong Hua, C07-165 K., Dhanalakshmi, C07-177
C07-151 Deb, Dipankar, C07-069 Hansman, R. John, C07-156 Kerho, Michael F., C07-159
Beran, Philip S., C07-005 De Breuker, Roeland, C07-129 Hardy, Robin C., C07-184 Khanafseh, Samer M., C07-194
Berton, E., C07-135 De Gaay Fortman, W. F., C07-010 Harino, Yohei, C07-235 Kholodar, Denis B., C07-208
Bhargava, Anil, C07-019 Dehghani, Alireza, C07-190 Hathaway, Eric, C07-172 Kim, Cheolwan, C07-164
Bilyk, Derek, C07-197 DeLaurier, James, C07-192, Hause, Terry, C07-157 Kim, Y.1., C07-154
Biskri, Djallel Eddine, C07-162 C07-166, C07-197 Hauser, Thomas, C07-158 King, Rudibert, C07-020
Blackburn, Ken, C07-207 Del Core, Guiseppe, C07-078 He, Chuan, C07-058, C07-150 Kliment, Linda K., C07-009
Blacodon, Daniel, C07-003 Demasi, Luciano, C07-008 Hein, Eric, C07-153 Kobayashi, Kunihiko, C07-017
Blair, M., C07-154 De Mendonga, Celso Braga, Heinze, Sebastian, C07-234 Kohama, Yasuaki, C07-077
Blasi, Luciano, C07-078 C07-182 Hemerly, Elder Moreira, C07-182 Kolonay, R.M., C07-154
Bleeze, Brian, C07-093 Deng, Xueying, C07-013, C07-021 Henning, Lars, C07-020 Komorowski, Jerzy P., C07-090
Bonnefoy, Philippe A., C07-156 De Ponte, Sergio, C07-099 Hennings, Elsa J., C07-211 Kong, Fanmei, C07-134
Botez, Ruxandra M., C07-033, De Silva, Suraj, C07-060 Hernandes, Fabiano, C07-178 Kontis, Konstantinos, C07-035,
C07-162, C07-238 De Weck, Olivier, C07-176 Heun, Matthew K., C07-222 C07-103, C07-204, C07-244
Botura, Galdemir, C07-057 Dimino, Ignazio, C07-143 Hiemenz, Gregory J., C07-122 Kopp, Friedrich, C07-095
Bourlart, Rémi, C07-054 Dinu, Alin Dorian, C07-033 Hiliuta, Adrian, C07-238 Kornbluh, Roy, C07-197
Bowers, Al H., C07-044 Dowell, Earl H., C07-148 Hilmes, Craig L., C07-213 Krumbein, Andreas M., C07-011,
Bragg, Michael B., C07-206 Duraisamy, Karthikeyan, C07-195 Hiraiwa, Tetsuo, C07-242 C07-107