American Institute of Aeronautics and Astronautics. AIAA Journal 2012: Vol 50 Index

2012·7 MB·English

AIAA JOURNAI
Vol. 50, No. 12, December 2012
2012 AIAA Journal Index
How to Use the Index
In the Subject Index, pages 2944-2952, 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 2953-2955, lists all authors associated with a given technical paper. The locating numbers are identical to
those in the Subject Index. The Chronological Index, pages 2956-2964, 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. The Book Review Index is listed on page 2964. 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 2012, 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, J12-141 Experimental Characterization of Aero- Ji2-122 Comp
CONVENTIONAL, STOL/VTOL dynamic Behavior of Membrane Wings in Low Use of Respor s
Reynolds-Number Flow Load Modeling
J12-150 Effects of Actuation Frequency on Flow Ji2-022 Flow Ar
Aerodynamics
Control Applied to a Wall-Mounted Hump Rey nolds-Number
J12-235 Aerodynamic Investigations of J12-145 Assessment of Wake- fail Interference 312-037 Eddy-Pres
Morphing Membrane Wing Subsonic Flows
Effects on the Dynamics of Flexible Aircraft
Ji2-202 Study of Discrete Modes Branching in J12-040 Low-R
J12-178 Reynolds-Averaged Navier-Stokes
High-Speed Boundary Layers sive Stall Contr
J12-228 Evaluation and Parameterization of Computations of Synthetic Jet Flows Using Edges
Round Vortex Generator Jet Experiments for Deforming Meshes J12-007 Flow Top
Flow Control J12-261 Large-Eddy Simulation of Shock Three-Dimensional Obstac!
J12-213| Oscillation Frequency and Amplitude Boundary-Layer Interaction J12-006 Effects of S
Effects on Plunging Airfoil Propulsion and Flow J127-%26?2 Thrust and Aerodynamic Forces from an of Low-Aspect-R
Periodicity Oscillating Leading Edge Flap Wings
Ji2-212 Numerical Investigation of Energy J12-264 Flapping Flight: High Thrust and J12-005 Mode
Extraction in a Tandem Flapping Wing Confi Propulsive Efficiency due to Forward Gliding Aerothermodynan
guration Oscillations moelasticity
J12-210 Computation of Eigensolution Deriva Ji2-114 Alternative Cokriging Method for
tives for Nonviscously Damped Systems Using Variable-Fidelity Surrogate Modeling Aeroelasticity and Aé
the Algebraic Method Ji2-186 Hovering Hinge-Connected Flapping J12-238 Scaling
Ji2-196 Dynamic Stall Control Using Deploy nomena Using tl
Plate with Passive Deflection
ible Leading-Edge Vortex Generators 512-235 Aerod
J12-091 Gappy Proper Orthogonal Decomposi
Ji2-188 Measurements of Aerodynamic Coeffi Morphing Membr
ion-Based Two-Step Optimization for Airfoil
nts for Flapping Wings at 0-90 Angles of J12-254 X-HALI
Desier
Attack Aerial Vehicle f
Ji2-222 Experimental Studies on a Rudimentary J12-239 Effect of Perforated Plates on the Ji2-141 Experi
Four-Wheel Landing Gear Acoustics of Annular Combustors dynamic Behavi
j12-176 Comparison of Mesh Adaptation Using J12-257 Further Studies of Airfoils Supporting Reyno!ds Number
the Adjoint Methodology and Truncation Error Non-Unique Solutions in Transonic Flow Ji2-145 Assess!
Estimates 12-051 Separation Control Characteristics of Effects on the Dy
Ji2-223 Influence of Large-Scale Freestrean Synthetic Jets Depending on Exit Configuration Ji2-012 Aeroe
Turbulence on the Performance of a Thin Airfoil ji2-077 Surrogate-Based Multi-Objective Aero Material Delta Wi:
Ji2-229 Body Force Model for the Aerodynam thermodynamic Design Optimization of Hyper J12-098 = Efficient
cs of Inclined Perforated Surfaces onic Spiked Bodies Analysis Based
Puching Airfoil with Combined Gurney J12-082 Vortex-Generator Models for Zero- and Reduced-Order M«
Flap and Unsteady Trasiing-Edge Flap Deflection A\dverse-Pressure-Gradient Flows J12-262 Thrusta
J12-054 Effects of Surface Roughness on Oscillating Leadir
J12-048 Effects of Distributed Suction on an
Separated and Transitional Flows over a Wing J12-067 Aeroelasti
Airfoil at Low Reynolds Number
J12-043 Theoretical Modeling of the Chemical Transformation Techr
J12-049 Aerodynamic Shape Optimization of
Non-Equilibrium Flow Behind a Normal Shock J12-089 Aeroelastic Optimi
Wave Wings Using a Parallel Newton-Krylov Approach Wing Venation: A Cellular Di
Ji2-143 Effects of End Plates and Blockage on J12-056 Effect of Jet Nozzle Lip Momentum J12-065 Aeroelastic Simulatior
Low-Reynolds-Number Flows Over Airfoils Loss on Circulation Control Airfoil Performance Flight Vehicles
Ji2-154 Use of Blowing Flow Control to Reduce J12-115 Implicit Computational Fluid Dynamics J12-117 Flutter-Boundary Prraeddiiccttii on
Bluff Body Interaction Noise Methods for Fast Analysis of Rotor Flows Morphing Wing in the Process of Adaptation
Ji2-173 Hierarchical Kriging Model for Varia J12-133 Development of a 17-Hole Omnidirec- J12-047 Aeroelastic Scaling of a Joined Wing for
ble-Fidelity Surrogate Modeling tional Pressure Probe Nonlinear Geometric Stiffness
2944
AIAA JOURNAI
Vol. 50, No. 12, December 2012
2012 AIAA Journal Index
How to Use the Index
In the Subject Index, pages 2944-2952, 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 2953-2955, lists all authors associated with a given technical paper. The locating numbers are identical to
those in the Subject Index. The Chronological Index, pages 2956-2964, 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. The Book Review Index is listed on page 2964. 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 2012, 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, J12-141 Experimental Characterization of Aero- Ji2-122 Comp
CONVENTIONAL, STOL/VTOL dynamic Behavior of Membrane Wings in Low Use of Respor s
Reynolds-Number Flow Load Modeling
J12-150 Effects of Actuation Frequency on Flow Ji2-022 Flow Ar
Aerodynamics
Control Applied to a Wall-Mounted Hump Rey nolds-Number
J12-235 Aerodynamic Investigations of J12-145 Assessment of Wake- fail Interference 312-037 Eddy-Pres
Morphing Membrane Wing Subsonic Flows
Effects on the Dynamics of Flexible Aircraft
Ji2-202 Study of Discrete Modes Branching in J12-040 Low-R
J12-178 Reynolds-Averaged Navier-Stokes
High-Speed Boundary Layers sive Stall Contr
J12-228 Evaluation and Parameterization of Computations of Synthetic Jet Flows Using Edges
Round Vortex Generator Jet Experiments for Deforming Meshes J12-007 Flow Top
Flow Control J12-261 Large-Eddy Simulation of Shock Three-Dimensional Obstac!
J12-213| Oscillation Frequency and Amplitude Boundary-Layer Interaction J12-006 Effects of S
Effects on Plunging Airfoil Propulsion and Flow J127-%26?2 Thrust and Aerodynamic Forces from an of Low-Aspect-R
Periodicity Oscillating Leading Edge Flap Wings
Ji2-212 Numerical Investigation of Energy J12-264 Flapping Flight: High Thrust and J12-005 Mode
Extraction in a Tandem Flapping Wing Confi Propulsive Efficiency due to Forward Gliding Aerothermodynan
guration Oscillations moelasticity
J12-210 Computation of Eigensolution Deriva Ji2-114 Alternative Cokriging Method for
tives for Nonviscously Damped Systems Using Variable-Fidelity Surrogate Modeling Aeroelasticity and Aé
the Algebraic Method Ji2-186 Hovering Hinge-Connected Flapping J12-238 Scaling
Ji2-196 Dynamic Stall Control Using Deploy nomena Using tl
Plate with Passive Deflection
ible Leading-Edge Vortex Generators 512-235 Aerod
J12-091 Gappy Proper Orthogonal Decomposi
Ji2-188 Measurements of Aerodynamic Coeffi Morphing Membr
ion-Based Two-Step Optimization for Airfoil
nts for Flapping Wings at 0-90 Angles of J12-254 X-HALI
Desier
Attack Aerial Vehicle f
Ji2-222 Experimental Studies on a Rudimentary J12-239 Effect of Perforated Plates on the Ji2-141 Experi
Four-Wheel Landing Gear Acoustics of Annular Combustors dynamic Behavi
j12-176 Comparison of Mesh Adaptation Using J12-257 Further Studies of Airfoils Supporting Reyno!ds Number
the Adjoint Methodology and Truncation Error Non-Unique Solutions in Transonic Flow Ji2-145 Assess!
Estimates 12-051 Separation Control Characteristics of Effects on the Dy
Ji2-223 Influence of Large-Scale Freestrean Synthetic Jets Depending on Exit Configuration Ji2-012 Aeroe
Turbulence on the Performance of a Thin Airfoil ji2-077 Surrogate-Based Multi-Objective Aero Material Delta Wi:
Ji2-229 Body Force Model for the Aerodynam thermodynamic Design Optimization of Hyper J12-098 = Efficient
cs of Inclined Perforated Surfaces onic Spiked Bodies Analysis Based
Puching Airfoil with Combined Gurney J12-082 Vortex-Generator Models for Zero- and Reduced-Order M«
Flap and Unsteady Trasiing-Edge Flap Deflection A\dverse-Pressure-Gradient Flows J12-262 Thrusta
J12-054 Effects of Surface Roughness on Oscillating Leadir
J12-048 Effects of Distributed Suction on an
Separated and Transitional Flows over a Wing J12-067 Aeroelasti
Airfoil at Low Reynolds Number
J12-043 Theoretical Modeling of the Chemical Transformation Techr
J12-049 Aerodynamic Shape Optimization of
Non-Equilibrium Flow Behind a Normal Shock J12-089 Aeroelastic Optimi
Wave Wings Using a Parallel Newton-Krylov Approach Wing Venation: A Cellular Di
Ji2-143 Effects of End Plates and Blockage on J12-056 Effect of Jet Nozzle Lip Momentum J12-065 Aeroelastic Simulatior
Low-Reynolds-Number Flows Over Airfoils Loss on Circulation Control Airfoil Performance Flight Vehicles
Ji2-154 Use of Blowing Flow Control to Reduce J12-115 Implicit Computational Fluid Dynamics J12-117 Flutter-Boundary Prraeddiiccttii on
Bluff Body Interaction Noise Methods for Fast Analysis of Rotor Flows Morphing Wing in the Process of Adaptation
Ji2-173 Hierarchical Kriging Model for Varia J12-133 Development of a 17-Hole Omnidirec- J12-047 Aeroelastic Scaling of a Joined Wing for
ble-Fidelity Surrogate Modeling tional Pressure Probe Nonlinear Geometric Stiffness
2944
Noise
J12-233 Active Control of Flow-Induced Acous-
ce Through Surface Perturbation
J12-046 a ai . : :
12-197 Rocket Noise Sources Localization
I Tailored Beam-Forming Technique
J12-005
J12-195 Tailored Nozzles for Jet Plume Control
I Reduction
J12-208 External Mean Flow Effects on Sound
\erospace Plane J: 12-082 Vortex-Generator Mode rr, allssiieons Thrroenueeg h Aco: ustica . Absorp— tive
: \dverse-Pressure-Gradient Flo Structure
J12-065 \ 2.08 lnid ant f rodvt " . 7
: J12-080 Fluidic Control of Ac ) 2-124 Transmission Loss Analysis of a
: ’ on siuff Bodyo f Revolutior . .
n aB luff Body of Revolutio upled Helmholtz Resonator Network
. . 12-25 yw Control for NREL §S : an
Configou ration Desig& n J 1 Fk 7 RI asibility? of Aerodym, namic-Tab Jet
112-173 H = <a , : ££. -iuUrIbOiNn e Airtoil . Suppressors in a Hypersonic NoI zzle at
Z ig yer "< J12-066 Efficiency of Air M ;
Ji2-199 Wall-Pressure Spectral Model Including
Pressure Gradient Effects
Propeller and Rotor Systems
Ji2-234 Turbulence Within the Tip-Leakage
\ \xial Waterjet Pump
12-033 Fluid Rotor« rajt
J12-048 J12-196 Dynamic Stall Control Using Deploy-
LITT I »-Edge Vortex Generators
J12-068 Implicit Computational Fluid Dynamics
Flight Vechanics Stead Fast Analysis of Rotor Flows
ji2-111 Ji2-010 j12-081 Modeling and Testing of a Semiactive
Reynold Damper in Periodic Working Regimes
12-021 mbined Feature-Driven Richardson-
}12-041 Ii aptive Mesh Refinement for Unsteady
l ( J12-064
12-042 RIN i} Eft C Safety
t
J12-232 Effects of Weave Type on Ballistic
Fuels and Fuel Systems
of Fabrics
Flow ( ontrol Ji2-126 Bag Breakup of T
( Simulation
J12-228
112-21 putation of Eigensolution Deriva-
( iscously Damped Systems Using
J12-196 Method
| ro Air Vehicles istic Simulation of Hypersonic
J12-233 192
il Method for Dynamic Anal-
nensional Bimodular Structures
al Investigation of Energy
lem Flapping Wing Confi
! Materials
j12-191
zation of Embedded Sensor
Structural Health Monitoring of
J12-045
nes
J12-054 Flight and Ground
in Experimental Reentry
rom In-Flight Characterization
O Test
"7
thabited and Unmanned Air Vehicles
Around a Comb Wing in Low-
nber Flow
e Control of Flow-Induced Acous-
-()22 Through Surface Perturbation
putation of Eigensolution Deriva-
2-040 iscously Damped Systems Using
St; Method
Endd ctural Condition Assessment from
J12-089 .eroelastic Optt imi Excitation and Covariance of
Wing Ve on lular Di Matrix
2946 AIAAJ, VOL. 50, NO. 12: 2012 INDEX
J12-183 Innovative Digital Self-Powered Auton- J12-164 Effect of Initial Boundary-Layer State Boundary-Layer Stability and Transition
omous System for Multimodal Vibration Sup on Subsonic Jet Noise
Ji2-137 Recepti ind Stability of Supersonic
pression Ji2-181 Nonlinear Bifurcation Structure of Swept Flows
J12-208 External Mean Flow Effects on Sound Panels Subject to Periodic Acoustic Fluid- J12-174 Stabilizatio
Transmission Through Acoustic Absorptive Structure Interaction Layer Using Po
Sandwich Structure Ji2-244 Aeroacoustic Performance of Fractal Thicknesses
J12-165 Solution of Nonlinear Vibration Prob Spoilers J12-206 Transition
lem of a Prestressed Membrane by Adomian J12-248 Characterization of Aeroacoustic, Sili- Blunted Cones
Decomposition con Micromachined Microphones for Aircraft Hypersonic Flight
J12-177. Numerical Method for Dynamic Anal Fuselage Arrays J12-247 Four Dec
ysis of Two-Dimensional Bimodular Structures J12-263 Effect of Door Configuration on Cavity Instability: Problen
312-027 Reduced-Order Modeling for Nonlinea Flow Modulation Process J12-159 Triple-De
Analysis of Cracked Mistuned Multistage Bladed J12-105 Large-Eddy Simulations of Perfectly Boundary Layers
Disk Systems Expanded Supersonic Jets Using an Unstructured J12-164 Effect of
Ji2-011 Resonant Vibration Control of Three Solver on Subsonic Jet Nois
Bladed Wind Turbine Rotors J12-239 Effect of Perforated Plates on the Ji2-116 Roughness
J12-081 Modeling and Testing of a Semiactive Acoustics of Annular Combustors Hypersonic Lamin
Hydraulic Damper in Periodic Working Regimes J12-099 Computational Aeroacousticso f Aft Fan J12-119 Numerica
512-097 Chebyshev-Rit: Approach to Buckling Noises Characterizing a Realistic Coaxial Engine Boundary-Layer St
and Vibration of Curvilinearly Stiffened Plate J12-083 Impedance Eduction Based on Micro- J12-048 Effects
phone Measurements of Liners Under Grazing Airfoil at Low Reyr
COMPUTING, INFORMATION, Flow Conditions J12-020 Time-Resol
AND COMMUNICATION J12-094 Improved Multipole Broadband Time bility Waves in a H
Autonomous Systems Domain Impedance Boundary Condition Ji2-014 Validatio
Ji2-079 Effect of Rotor Wake Structure on Fan Averaged Navie S
Ji2-242 Automated, Real-Time Health Monitor Interaction Tone Noise Dimensional FI]
ing of Structures for Interplanetary Exploration 12-124 Transmission Loss Analysis of a J12-036 Linear
Systems
Parailel-Coupled Helmholtz Resonator Network eling for Aerodynat
J12-073 Single-Sensor Identification of Spinning Near-Wall Reyt
ENERGY
Mode Noise from Aircraft Engine
Wind Power J12-071 Feasibility of Aerodynamic-Tab Jet Computational Fluid Dynamics
Control for NREL S822 Wind Noise Suppressors in a Hypersonic Nozzle at Ji2-236 Beam Riding Perf
Takeoff metrically Propel
J12-003 Semi-Empirical Modeling of Turbulent Ji2-192. Manipu
FLIGHT SIMULATOR SYSTEMS Anisotropy for Airfoil Self-Noise Predictions Regions of Unst
J12-019 Simple Procedure for Multifrequency slow’s I quations
VEMS Analysis J12-228 Evaluat
ji2-113 Thrust Generation of a Heaving Foil in Ji2-026 Airfoil Trailing-Edge Blowing: Broad- Round Vortex
Micro Flow band Noise Prediction from Large-Eddy Simu- Flow Control
J12-220 High-Or
FLUID DYNAMICS Navier-Stokes Al
actions with Solid W
Aeroacoustics Boundary Layers and Heat J12-217 Numeric
Ji2-221 Trailing-Edge Noise Predictions Using Transfer-Laminar Distortions in Supers
Compressible Large-Eddy Simulation and Acous J12-078 Particle Image Velocimetry Measure Ji2-221 Trailing
tic Analog ment of Laminar Boundary Layer in a Streamwise Compressible Lat
Ji2-209 Acoustic Measurements in a Low-Speed Corner tic Analogy
Wind Tunnel Type Gottingen J12-252 Fluid-Thermal Response of Spherical J12-204 Converger
J12-195 Tailored Nozzles for Jet Plume Control Dome Under a Mach 6.59 Laminar Boundary Sensitivity Estimati
nd Noise Reduction Layer J12-190 Study of
Ji2-215 Acoustic Effect of Chevrons on Super action Using Larg
xiting Conical Convergent-Divergent Averaged Navier
Boundary Layers and Heat
J12-224 Unsteady
J12-214 Optimization of Microphone Array Wall Transfer-Turbulent Optimization of FI
Mountings in Closed-Section Wind Tunnels J12-217 Numerical Simulations of Successive J12-167 Numerical Sin
J12-148 Aeroacoustic Effectso f a Cylinder-Plate Distortions in Supersonic Turbulent Flow Tube Flow with Equilibrium Air Model
Configuration J12-199 Wall-Pressure Spectral Model Including J12-225 Scalar-Filtered Mass-Density-Fun
J12-199 Wall-Pressure Spectral Model Including the Adverse Pressure Gradient Effects Simulation of Swirling Reacting Flow
the Adverse Pressure Gradient Effects J12-190 Study of a Compression-Ramp Inter- Unstructured Grids
Ji12-197 Rocket Noise Sources Localization action Using Large-Eddy Simulation/Reynolds- J12-193 Numerical Simulation of Laminar and
Through a Tailored Beam-Forming Technique Averaged Navier-Stokes Models Turbulent Two-Phase Flow in Pressure-Swirl
J12-185 Shock Oscillations in a Supersonic Jet J12-194 Large-Eddy Simulation of Shock/ Atomizers
Exhibiting Antisymmetrical Screech Cooling-Film Interaction J12-136 Experimental and Numerical Investiga
J12-030 Coupled Discontinuous Galerkin/Finite J12-256 Term-by-Term Analysis of Near-Wall tion of a Supersonic Convergent-Divergent
Difference Solver on Hybrid Meshes for Second-Moment Closures Nozzle
Computational Aeroacoustics J12-038 Study of Turbulence-Radiation Interac- J12-176 Comparison of Mesh Adaptation Using
J12-136 Experimental and Numerical Investiga tion in Hypersonic Turbulent Boundary Layers the Adjoint Methodology and Truncation Error
tion of a Supersonic Convergent-Divergent Ji2-064 Towards a General Strategy to Model Estimates
Nozzle Riblet Effects J12-171_ Plasma Jet for Flight Control
J12-154 Use of Blowing Flow Control to Reduce J12-061 Aero-Optical Effects of Supersonic J12-173 Hierarchical Kriging Model for
Bluff Body Interaction Noise Boundary Layers Variable-Fidelity Surrogate Modeling
AIAAJ, VOL. 50, NO. 12: 2012 INDI 2947
J12-166 | teady Flow Analysis of a Multi J12-085 Assessment of Computational J12-252 Fluid-Thermal Response of Spherical
Element Airfoi g Lattice Boltzmann Method Dynamics and Experimental Datz Dome Under a Mach 6.59 Laminar Boundary
J12-030 led Di tinuous Galerkin/Finite Boundary-Layer Interactions
Meshes for J12-079 Effect of Rotor Wake Struct J12-158 Reynolds-Averaged Navier-Stokes Sim-
( ymputati Interaction Tone Noise t > HyShot II Scramjet
J12-241 J12-053 Risk Assessment of Scran J12-063 Rayleigh Scattering Density Measure-
1omal Using Adjoint-Based Sampling Met t Theory, and Nucleation Calcu-
Ji2-250 Lar Ji2-049 Aerodynamic Shape ) h 10
Wings | ygate-Based Multi-Objective Aero-
J12-050 nic Design Optimization of Hyper-
| Bodies
\ir Density Measurementisn aM ach 10
J12-239 lodine Cordes Bands
Kc J12-057 Continuous del Reduction of Computational
12-258 Spalart-Allmaras Model mics for Hypersonic Aerother-
J12-116 Roughness-Induced Instability in a
Outfic H c Laminar Boundary Layer
j12-119 Numerical Investigation of Hypersonic
J12-036 inear-Stability B ry-Layer Stabilization by Porous Surfaces
j12-142 er ¢ \erodynamic J12-007 Flow Topology Around Gas, Liquid and
rt \ NCar- VV ds-Stre I ional Obstacles in Hypersonic Flow
J12-186 J12-037 petitively Pulsed Hypersonic Flow
Sut r Diagnostic Development
ji2-024 Ni Resolved Visualization of Insta-
a Hypersonic Boundary Layer
2-003 Se
Inlet, Nozzle, Diffuser, and Channel
2-039 } Ie ws
‘sient Pressure-Sensitive-Paint In-
i Nozzle
int-Based Design Optimization of
rator in an S-Shaped Subsonic Inlet
Force Model for the Aerodynam-
1 Perforated Surfaces
ibility of Aerodynamic-Tab Jet
sors in a Hypersonic Nozzle at
ive >
ji2-114
rbance Level Characterization of a
is
vdown Facility
J12-132
Eddy Simulation of a Supersonic
zation of Continuous Stream of
ji2-041 | e Past the Langston Turbine
(
Ji2-010 | ed Integral Form of the Com-
R
ield in Thin Channels’ with
Hype rsonic Flow Pressure Unsteadiness and Side
rexpanded Rocket Nozzles
J12-206 |
Jets, Wakes, and Viscid-Inviscid Flow
J12-100 Interactions
K Abr tion Criterion for Axisymmetric
} id fF High Stokes Numbers
J12-240 stic Effect of Chevrons on Super-
iting Conical Convergent-Divergent
J12-189 European Effect of Initial Boundary-Layer State
Testbed Winglet: From In-t Subsonic Jet Noise
SCIROCCO Test J12-160 owfield Characteristics of a Hyper-
Non-U nique lutions in Ji2-241 Carbuncle Phenomena racting with Transverse Injection in
Ji2-084 R olds-Averaged Anomalies in Three Dimensions Sur nic Flow
Study of the Shock-Buffet Instability Mechanism j12-163 PI al ight into S J12-104 Modeling and Simulation of Fuel-
J12-082 Vortex-Generator Models for Zero- and Behavior via Multi-Objective Desig Oxidizer Mixing in Micropower Systems
Adverse-Pressure-Gradient Flows tion J12-134 Formation of Turbulent Vortex Break-
Ji2-243 hp-Adaptive Discontinuous J12-038 Study of Turbulence-Radiatio i termittency, Criticality, and Global
Solver for the Navier-Stokes Equations tion in Hypersonic Turbulent Bounda
J12-069 Periodic Unsteady Flow Analysis Using J12-246 Disturbance Level Charactet 312-180 Turbulent Flows of an Acoustically
a Diagonally Implicit Harmonic Balance Method Hypersonic Blowdown Facility Excited Elevated Transverse Jet
2948 AIAAJ, VOL. 50, NO. 12: 2012 INDEX
J12-244 Aeroacoustic Performance of Fractal J12-259 Tomographic Particle Image Velocim- Ji2-209 Acoustic Meas
Spoilers etry Measurements in a Bluff-Body Wake Flow Wind Tunnel, Type G
Ji2-105 Large-Eddy Simulations of Perfectly J12-031 Separation Control with Nanosecond-
Expanded Supersonic Jets Using an Unstructured Pulse-Driven Dielectric Barrier Discharge Plasma
Supersonic Flow
Solver Actuators
J12-190 Study of Compression-Ramp Inter
J12-151 Source Advection Effects on Unsteady J12-169 Model-Based Feedback Flow Control
action Using Large-Eddy Simulation/Reynolds
Surface-Pressure Asymmetry in Oblique Imping Development and Simulation for a Pitching Turret
Averaged Navier—St es Models
ing Jets J12-223 Influence of Large-Scale Freestream
Ji2-215 Acoustic Effect of Chevrons on Super
Ji2-144 Large Eddy Simulation of Supersonic Turbulence on the Performance of a Thin Airfoil
sonic Jets Exiting Conical Conver:
impinging Jets J12-150 Effects of Actuation Frequency on Flow
Nozzles
Ji2-075 Minimizing the Loss Produced by a Control Applied to a Wall-Mounted Hump
J12-217 Numerical Simulations of Succe
Turbulent Separation Using Vortex Generator Jets J12-143 Effects of End Plates and Blockage on
Distortions in Supersonic Turbulent Flow
J12-080 =Fluidic Control of Aerodynamic Forces Low-Reynolds-Number Flows Over Airfoils
on a Bluff Body of Revolution J12-155 Simulation-Guided, Model-Based Feed- J12-160 Flowfield Characteristics of Hyper
mixer Interacting with Trans\
J12-260 High-Speed Rarefied Round Jet and Jet back Flow Control for a Pitching Turret
Supersonic Flow
Impingement Flows ji2-256 Term-by-Term Analysis of Near-Wall
J12-185 Shock Os
J12-023 Numerical Investigation of a Cylinder Second-Moment Closures
Exhibiting Antisymmetri
Immersed in a Supersonic Boundary Layer J12-247 Four Decadeso f Studying Global Linear
J12-191 Impact
J12-041 Evaluation of Dynamic Derivatives Instability: Problems and Challenges
Shock Boundary |
Using Computational Fluid Dynamics J12-245 Experimental and Numerical Investiga-
J12-144 Larg
J12-050 Effect of Jet Nozzle Lip Momentum tion of a Wing-Body Junction Flow
Impinging Jets
Loss on Circulation Control Airfoil Performance J12-106 Numerical Dissipation Effects on Mas-
Ji2-249 Shockv
sive Separation Around Tandem Cylinders
Multiphase Flows tion Control or
J12-146 Passive Control of High Speed Sepa-
Ji2-193 Numerical Simulation of Laminar and rated Flows Using Splitter Plates Steady Micro Je
Turbulent Two-Phase Flow in Pressure-Swirl J12-244 Aeroacoustic Performance of Fractal J12-250 Large-I
Atomizers Spoilers sonic ( rossflow
Ji2-126 Bag Breakupo f Turbulent Liquid Jets in J12-080 =Fluidic Control of Aerodynamic Forces J12-128 Zones of Inf
Crossflows on a Bluff Body of Revolution a Shock/Boundary
Ji2-031 Separation Control with Nanosecond Ji2-128 Zones of Influence and Shock Motion in J12-103 Provab!
Pulse-Driven Dielectric Barrier Discharge Plasma a Shock/Boundary-Layer Interaction Optumization Al
Actuators 12-112 Novel Time-Resolved Pressure Meas- Fidelity Derivati
J12-167 Numerical Simulation of Air-He Shock urements on an Airfoil at a Low Reynolds Number J12-146 Passive
Tube Flow with Equilibrium Air Model J12-072, Cell Geometry and Material Property rated Flows Usin
J12-053' Risk A
Effects on Membrane and Flow Response
Plasmadynamics and MHD Using Adjoint-B
J12-084 Reynolds-Averaged Navier-Stokes
J12-029 Simulation of Direct-Current Surface J12-110 = Interaction
Study of the Shock-Buffet Instability Mechanism
Plasma Discharges in Air for Supersonic Flow Highly Underexp
Ji2-075 Minimizing the Loss Produced by a
Control J12-108 Extract
Turbulent Separation Using Vortex Generator Jets
J12-009 Plasma Lens for Optical Path Difference Noisy Schlierer
J12-035 | nsteady Transonic Flow over a
Control Vision Techniqu
Transport-Type Swept Wing
J12-058 Simulations of Nanosecond Pulsed J12-023 Numer
J12-033 Fluidic Control of a Wing Tip Vortex
Plasmas in Supersonic Flows for Combustion Immersed in a Super
Ji2-051 Separation Control Characteristics of
Applications J12-021 Control
Synthetic Jets Depending on Exit Configuration
J12-138 Pressure Dependenc e of Dielectric Interaction by |
J12-021 Control of a Shock/Boundary-Layer
Barner Discharge Plasma Flow Actuators J12-061 Aero-Optica
Interaction by Using a Pulsed-Plasma Jet Actuator
Boundary Layer
Rarefied Flows 512-004 Wall Pressure Unsteadiness and Side
Loads in Overexpanded Rocket Nozzles
Ji2-260 High-Speed Rarefied Round Jet and Jet
Impingement Flows J12-008 Comparison of nsteady Pressure Transonic Flow
Sensitive Paint Measurement Techniques J12-098 Efficient Meth
Reacting Flows and Combustion Analysis Based
J12-170 Proper Orthogonal Decomposition for Shock Waves and Detonations Reduced-Order Mox
Experimental Investigation of Flame Instabilities J12-167 Numerical Simulation of Air-He Shock J12-258 Towards
J12-225 Scalar-Filtered Mass-Density-Function Tube Flow with Equilibrium Air Model Dimensional Bumy
Simulation of Swirling Reacting Flows on J12-194 | argc Eddy Simulation of Shock/ and Buffet Alleviat
Unstructured Grids Cooling-Film Interaction J12-238 Scaling Analysis for Aeroelastic Phe
512-093 Simulation of Microgravity Diffusion J12-085 Assessment of Computational Fluid nomena Using the Navier Stokes Fluid Model
Flames Using Sub-Atmospheric Pressures Dynamics and Experimental Data for Shock J12-095 Flow Similarity i Compressible
J12-158 Reynolds-Averaged Navier-Stokes Sim Boundary-Layer Interactions Convex-Corner Flows
ulations of the HyShot I] Scramjet Ji2-256 Term-by-Term Analysis of Near-Wall J12-084 Reynolds-Averaged Navier-Stokes
J12-043 Theoretical Modeling of the Chemical Second-Moment Closures Study of the Shock-Buffet Instability Mechanism
Non-Equilibrium Flow Behind a Normal Shock J12-043 Theoretical Modeling of the Chemical Ji2-257 Further Studies« f Airfoils Supporting
Wave Non-Equilibrium Flow Behind a Normal Shock Non-Unique Solutions in Transonic Flow
Wave J12-052 Improvements and Extensions to a Full
Separated Flows
Potential Formulation Based on Independent
J12-205 Separation and Circulation Control on Subsonic Flow Fields
an Elliptical Airfoil by Steady Blowing J12-042 Improved Integral Form of the Com- J12-035 Unsteady Transonic Flow over a Trans
J12-227 Adjoint-Based Design Optimization of pressible Flowfield in Thin Channels with port-Type Swept Wing
Vortex Generator in an S-Shaped Subsonic Inlet Injection J12-057 Continuous Adjoint Approach for the
J12-222 Experimental Studies on a Rudimentary 512-072 Cell Geometry and Material Property Spalart-Allmaras Model in Aerodynamic Opti-
Four-Wheel Landing Gear Effects on Membrane and Flow Response mization
AIAAJ, VOL. 50, NO 2949
Unsteady Flows Combined Feature-Driven Ri CAD/CAM
J12-213 Oscillation Frequency and Amplitude Adaptive Mesh Refinement fo Ji2-131 Physics- and Engineering Knowledge-
Effects on Plur Airfoil Propulsion and Flow Vortical Flow R Repair of Computer-Aided Design Param-
Periodicity J12-007_ Flow Topology Around G tries
ji2-220 H Phree-Dimensional Obstacles in H
Navier-Stoke Ji2-090 Effe of Flow St Lasers and Laser Applications
Instabiliti
112-00 » Plasma Lens for Optical Path Difference
J12-033 Fl
J12-242 A itomated, Real-Time Health Monitor-
res for Interplanetary Exploration
GUIDANCE, CONTROL, AND
DYNAMICS TECHNOLOGY -Optical Effects of Supersonic
J12-224
oO Aircraft Dynamics 112-063 R eigh Scattering Density Measure-
J12-238 ji2-111 D Theory, and Nucleation Calcu-
M h10o
J12-155 \ th-Speed Fuel/Hydroxyl Radical
Gas Turbine Pilot Burner
Control System Effectors
J12-125 Modelu tf Vultidisciplinary Design Optimization
I
Modeling of Electrodynamic Zero-Net
Control Theory tuators
rgence Error and Higher-Order
ji2-011 R
mations
Db
sing for Robust Design Optimiza-
Dynamics
J12-262 Ji2-011 RK stic Optimization of Flapping
Bladed W \ Cellular Division Approach
j12-098 | J12-107 P bly Convergent Multifidelity
Algorithm Not Requiring High-
I
j12-106 nuous Adjoint Approach for the
de Flight Mechanics s Model in Aerodynamic Opti-
12-259 T J12-145
aa } |
Vi
Reliability, Maintainability, and Logistics
J12-108 Information Processing Supp ort
J12-19 unting for Proof Test Data in a
1 Design Optimization Frame
Optimi
J12-069 P 12-224
O Flapp \irt Research Facilities and Instrumentation
12-008 ( J12-017 Response 17 112-209 stic Measurements in a Low-Speed
pe Gottingen
‘S parison of Unsteady Pressure-
J12-091 Measurement Techniques
ion of Oblique Structures in
n Sequences Using Computer
ji2-010 |
R Optimizationo f Microphone Array Wall
J12-014 Closed-Section Wind Tunnels
System Identification
J12-139 Structural C¢
J12-004 W rical Analysis of the Hydro-
White Notsese Excitation
i ads in VU Phenomenon in Aircraft Fuel Tanks
Covariance Matri
J12-012 Aeroelastic Analy Sensor Systems
Vortices Material Delta Wing in Low 119.9 3) Optimization of Embedded Sensor
J12-245 | Structural Health Monitoring of
tion of a Wi Junction Flow INTERDISCIPLINARY TOPICS Airframes
J12-220 High-Or curate Incompressible Shear-Lag Solution for Guided
Vortex-Rin Analytical and Numerical Methods with Piezoelectric-Wafer Active
J12-099 Computational Aeroacot
Noises Characterizing a Realistic Cc Online Guided Wave-Based Debonding
Subsonic Co sible Flow J12-103 Provably Convergent in Honeycomb Sandwich Structures
Ji2-259 Tomographic Particle Image Velocim Optimization Algorithm Not Requirir le-Sensor Identificofa Stpiinoninng
etry Measuren 1 a Blutf-Body Wake Flow Fidelity Derivatives M from Aircraft Engine
Ji2-134 Formation of Turbulent Vortex Break Ji2-165 Solution of Nonlinear Vibratic J12-248 varacterization of Aeroacoustic, Sili-
agown Interm Criticality, and Global lem of a Prestressed Membrane by Adomiar con Micromachined Microphones for Aircraft
Instability Decomposition Arrays
2950 AIAAJ, VOL. 50, NO. 12: 2012 INDEX
LAUNCH VEHICLE AND Engine Power Cycles Supersonic Combustion
MISSILE (LV/M) TECHNOLOGY J12-197 Rocket Noise Sources Localization J12-028 Supersonic Skin-Friction Drag with
Through a Tailored Beam-Forming Technique Tangential Wali Slot Fuel Injection and
Aerodynamics Combustion
J12-135 Transient Pressure-Sensitive-Paint In- Fuels and Propellants, Properties of
Turbomachinery
vestigation in a Nozzle J12-104. Modeling and Simulation of Fuel-
J12-032 Reduced-Order Modeling Approach for
Propulsion and Propellant Systems Oxidizer Mixing in Micropower Systems Blisks with Large Mass, Stiffness, and Geometric
J12-001 Fuel Options for Next-Generation
J12-260 High-Speed Rarefied Round Jet and Jet Mistuning
Chemical Propulsion
Impingement Flows J12-099 Computational Aeroacoustics of Aft Fan
Noises Characterizing a Realistic Coaxial Engine
Structural Design (Including Loads) Gas Turbine Engines
J12-107 =P iezoelectri sed Vibration Reduc
J12-017. Dynamic Response Topology Optimi J12-090 Effects of Flow Structure Dynamics on tion of Turbomachinery Bladed Disks
zation in the Time Domain Using Equivalent Thermoacoustic Instabilities in Swirl-Stabilized Resonance Frequency Detuning
Static Loads Combustion J12-075 Minimizing the
J12-219 Surrogate-Based Optimum Design for J12-153 Turbine Burners: Performance Improve- Turbulent Separation Using Vortex Gene
Suffened Shells with Adaptive Sampling ment and Challenge of Flameholding
J12-170 Proper Orthogonal Decomposition for SPACE TECHNOLOGY
Testing, Flight and Ground
Experimental Investigation of Flame Instabilities
J12-130 Modeling of Two-Stage Ejector for Spacecraft Structural Configuration,
High- Altitude Testing of Satellite Thrusters Design, and Analysis
Hypersonic Propulsion
Thermal Protection Systems J12-158 Reynolds-Averaged Navier-Stokes Sim- J12-218 Robusines
J12-034 Two-Dimensional Orthotropic Plate ulations of the HyShot II Scramjet Reduction Expans
Structure Model \
Analysis for an Integral Thermal Protection J12-163 Physical Insight into Scramjet Inlet
System Behavior via Multi-Objective Design Optimiza- Spacecrafi Test and Evaluation
Ji2-201 Role of Thermal Contact Conductance ton J12-101 Texture-Ba> sed Photogra
on Sandwich-Type Metallic Thermal Protection J12-055 How Much Compression Should a racy on Curved Surt
System Profile Scramjet Inlet Do? Ji2-211 Exact S
J12-028 Supersonic Skin-Friction Drag with Waves Tuning
PROPULSION CToamngbeunsttiailo n Wall Slot Fuel Injection and JSie2n-s2o1r8s Robustness
Airbreathing Propulsion J12-162 Formation and Structure of Steady Reduction Expans
Oblique and Conical Detonation Waves
J12-153 Turbine Burners: Performance Improve Structure Model V
ment and Challenge of Flameho!ding Laser Integration/Systems Spacecraft Thermal Management
J12-055 How Much Compression Should a
Scramjet Inlet Do? J12-23%6 Beam Riding Performance of Asym- 312-034 Two-Dimensional Orthotropi
metrically Propelled Laser Vehicle Analysis for
J12-161 Disruption of Volatile and Nonvolatile
System
Droplets Under Locally Supersonic Conditions
Ji2-162 Formation and Structure of Steady Micro Propulsion and Power STRUCTURAL MECHANICS
Obl:que and Conical Detonation Waves Ji2-104 Modeling and Simulation of Fuel- AND MATERIALS
Oxidizer Mixing in Micropower Systems
Combustion and Combustor Designs
Aeroelasticity and Control
J12-126 Bag Breakupo f Turbulent Liquid Jets in Microwaves J12-067 Aeroelastic Analy
Crossflows
Ji2-179 Design for Broadband High-Temper- Transformation Techniqu
512-093 Simulation of Microgravity Diffusion
ature Radome Wall with Graded Porous Structure
Flames Using Sub-Atmospheric Pressures Dynamic Model Analysis
Ji2-153 Turbine Burners: Performance Improve Ramjets and Scra:njets J12-181 Nonlinear Bifi
ment and Challenge of Flameholding Panels Subject
J12-163 Physical Insight into Scramjet Inlet
Combustion Instability Behavior via Multi-Objective Design Optimiza- Structure Interaction
J12-187 On Strain-Rate Dependence of Kinetic
Ji2-170 Proper Orthogonal Decomposition for von
Energy in Homogenization Approach: Theory and
Experimental Investigation of Flame Instabilities J12-147_ Large-Eddy Simulation of a Supersonic
Experiment
312-090 Effects of Flow Structure Dynamics on Inlet-Isolator
Ji12-074 Dynamic Strain Mapping and Real
Thermoacoustic Instabilities in Swirl-Stabilized J12-250 Large-Eddy Simulation of Jet in Super-
Time Damage-State Estimation Under Random
Combustion sonic Crossflow with Different Injectant Species
Fatigue Loading
J12-124 Transmission Loss Analysis of a Ji2-160 Flowfield Characteristics of a Hyper-
J12-081 Modeling and Testing of a semiactive
Parallel-Coupled Helmholtz Resonator Network mixer Interacting with Transverse Injection in
Hydraulic Damper in Periodic Working Regimes
J12-162 Formation and Structure of Steady Supersonic Flow
Oblique and Conical Detonation Waves J12-055 How Much Compression Should a Flexible and Active Structures
Droplet and Spray Characterization Scramjet Inlet Do? J12-232 Effects of Weave Type on Ballistic
J12-053 Risk Assessment of Scramjet Unstart Performance of Fabrics
Ji2-161 Disruption of Volatile and Nonvolatile Using Adjoint-Based Sampling Methods J12-211 Exact Shear-Lag Solution for Guided
Droplets Under Locally Supersonic Conditions J12-161 Disruption of Volatile and Nonvolatile Waves Tuning with Piezoelectric-Wafer Active
Emissions and Noises Droplets Under Locally Supersonic Conditions Sensors
J12-195 Tailored Nozzles for Jet Plume Control Ji2-123 Design and Testing of Pressurized
and Noise Reduction Solid Rocket Motors Cellular Planar Morphing Structures
J12-096 Modeling of Heterogeneous Propellant Ji2-101 Texture-Based Photogrammetry Accu
Engine Cooling and Heat Transfer Combustion: A Survey racy on Curved Surfaces
J12-616 =Visualization of Continuous Stream of J12-200 Low-Velocity Impact and Residual J12-203 Optimization of Stiffness Character-
Grid Turbulence Past the Langston Turbine Burst-Pressure Analysis of Cylindrical Composite istics for the Design of Bistable Composite
Cascade Pressure Vessels Laminates
AIAAJ, VOL. 50, NO. 12: 2012 INDEX 2951
J12-047_ Aeroelastic Scaling of a Joined Wing for J12-088 Fundamental Frequencies of Ellipti i] Ji2-019 Simple Procedure for Multifrequency
Nonlinear Geometri c Suftness Composite Cylinders with Circumfer Analvsis
512-072 Cx ometry and Material Property Varying Fiber Orientation J12-018 Finite Element Free Vibration Analysis
Effects on Me ne and Flow Response Ji2-123 Design and Testing t-Core Sandwich Beams
Ji2-107' P Vibration Reduc Cellular Planar Morphing Structures
led Disks via J12-013 Refined One-Dimensional Fi
Structural Modeling
for Laminat -d Structure Analysis
J12-121) Ad inces in Boundii ji2-187 On Strain-Rate Dependence of Kinetic
Aircraft Structures I Homogenization Approach: Theory and
;
Ji2-232 Eff J12-047 Aeroelastic Scaling of
Perforn Nonlinear Geometric Stiffness J12-168 Multimaterial Arbitrary-Lagrangian-
j12-056 \ Formulation for Blast-Induced Fluid-
D Structural Durability (Including Fatigue, Interaction in Fiber-Metal Laminates
Quadrature M Fracture, and Environmental Macroscale Independently Homogen-
J12-168 M Degradation) ls for Modeling Braided Composites
ternal Mean Flow Effects on Sound
J12-200 |
Through Acoustic Absorptive
Burst-Pre
Structure
Pre re Vess
Numerical Method for Dynamic Anal-
Structural Composite Materials J12-118 An
Dimensional Bimodular Structures
112-230 ©O Crack « R<eedduu ced-Order Modeling for Nonlinear
M "J 12-060 ‘f Cracked Mistuned Multistage Bladed-
Ji2-231 (
ced-Order Modeling Approach for
rge Mass, Stiffness, and Geometric
12-200 |
RBurst-Py
byshev-Ritz Approach to Buckling
Structural Dynamics and
of Curvilinearly Stiffened Plate
J12-140 Characterization
nerical Analysis of the Hydro-
J12-187 Or Phenomenon in Aircraft Fuel Tanks
bal Buckling of Sandwich Beams
}12-168 I
Extended High-Order Theory
t J12-032 1-Shell Deployable Reflectors with
Stiffeners: Experiments and Simu-
Ji2-172
is
lamental Frequencies of Elliptical
12-012
Cylinders with Circumferentially
M
r Orientation
J12-156 J12-218 K nlinear Model Reduction of von
Sand W Ic Re
tes Under Linearized Compressible
12-034 Cty
12-165
Procedure for Multifrequency
Syste
12-025
inces in Bounding Techniques for
Wetecuol
tures
J12-088
nsideration of Wear at High Veloc-
t
Hydrocode
Varying Ji?-027 KR
fined One-Dimensional Formulations
J12-013 \
1 Structure Analysis
© Lan UVisk S
Finite Element Free Vibration Analysis
J12-109 Ji2-070 ¢
ery in ( | Sandwich Beams
112-056 J12-097 J12-109 ietrically Nonlinear Stress Recov-
site Laminates
Me Ji2-102 tructural Damage
Generalized Flexibility Mat Structural Optimization
Structural Design Natural F requenc Surrogate-Based Optimum Design for
J12-203 J12-018 Finite Element Shells with Adaptive Sampling
i Soft re Sandwich Bea Optimization and Antioptimization of
Laminates J12-056 Vibration An Load for Composite Cylindrical Shells
J12-179 Desig for Broadband High wich Plates by the General ertainties
femperature Radome Wall with Graded Porous Quadrature Method Maximal Stiffness Design of Two-
Structure J12-025 Online Guided Wave Structures by Topology Optimization
J12-198 Accounting for Proof Test Detection in Honeycomb Sandwi babilistic Reliability
Reliability-Ba sed Design Optimization Frame Optimization of Stiffness Character-
work Structural Finite Elements the Design of Bistable Composite
J12-183 Inno itive Digital Self-Powered Auton J12-201 Role of Thermal Contact Cor
omous Syst *m for Multimodal Vibration Su; on Sandwich-Type Metallic Therma J12-086 Buckling Analysis and Optimization of
pression System Profile Stiffened Composite Flat and Curved Panels
J12-070 Consideration of Wear at High Veloc J12-231 Compression Response of Fl Ji2-123, Design and Testing of Pressurized
ities | sing a Hydrocode Composite Panels Cf ellular Planar Morphing Structures
2952 AIAAJ, VOL. 50, NO. 12: 2012 INDEX
512-198 Accounting for Proof Test Data in a J12-201 Kole of Thermal Contact Conductance Computational Heat Transfer
Reliability-Based Design Optimization Frame- on Sandwich-Type Metallic Thermal Protection
J12-226 Simulation and Cryogenic Experiments
work System Profile
of Natural Convection for the Titan Montgolfiere
Structural Stability
Cryogenics
J12-044 Thermal Buckling of Functionally THERMOPHYSICS AND HEAT
Graded Material Cylindrical Shells on Elastic TRANSFER J12-226 Simulation and Cryogenic Experiments
Foundation of Natural Convection for the Titan Montgolfiere
J12-140 Optmization and Antioptimization of
Aerothermodynamics/Thermal Protection Natural Convection
Buckling Load for Composite Cylindrical Shells
Under Uncertainties J12-189 European Experimental Reentry J12-226 Simulation and Cryogenic Experiments
J12-219 Surrogate-Based Optimum Design for Testbed Winglet: From In-Flight Characterization of Natural Convection for the Titan Montgolfiere
Stiffened Shells with Adaptive Sampling to SCIROCCO Test
J12-059 Thin-Shell Deployable Reflectors with J12-194 Large-Eddy Simulation of Shock/ Nonintrusive Diagnostics
Collapsible Stiffeners: Experiments and Simu- Cooling-Film Interaction Ji2-129 Air Density Measurements in a Mach 10
lations J12-207 Development of a Mach Wake Using lodine Cordes Bands
J12-086 Buckling Analysis and Optimization of Nonequilibrium-Flow Wind Tunnel J§12-127 Nitrogen Vibrational Population Meas
Stiffened Composite Flat and Curved Panels J12-063 Rayleigh Scattering Density Measure- urements in the Plenum of a Hypersonic Wind
J12-157 Global Buckling of Sandwich Beams ments, Cluster Theory, and Nucleation Calcu- Tunnel
Based on the Extended High-Order Theory lations at Mach 10 J12-207 Development of a Mach
J12-129 Air Density Measurements in a Mach 10 Nonequilibrium-Flow Wind Tunnel
Thermal Effects Wake Using lodine Cordes Bands
J12-044 Thermal Buckling of Functionally J12-179 Design for Broadband High- Radiation in Participating Media
Graded Material Cylindrical Shells on Elastic Temperature Radome Wall with Graded Porous J12-038 Study of Turbulence-Radiation Interac
Foundation Structure tion in Hypersonic Turbulent Boundary Layers