Computational Optimization of Flexible Wing Aerodynamic Performance in Hover (Englisch)
- Neue Suche nach: Ren, Y.
- Neue Suche nach: Dong, H.
- Neue Suche nach: American Institute of Aeronautics and Astronautics
- Neue Suche nach: Ren, Y.
- Neue Suche nach: Dong, H.
- Neue Suche nach: American Institute of Aeronautics and Astronautics
In:
Applied aerodynamics; 30th AIAA applied aerodynamics conference 2012; New Orleans, Louisiana, USA, 25-28 June, 2012
;
1659-1668
;
2012
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ISBN:
- Aufsatz (Konferenz) / Print
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Titel:Computational Optimization of Flexible Wing Aerodynamic Performance in Hover
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Beteiligte:
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Kongress:Conference; 30th, Applied aerodynamics; 30th AIAA applied aerodynamics conference 2012; New Orleans, Louisiana, USA, 25-28 June, 2012 ; 2012 ; New Orleans, LA
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Erschienen in:PAPERS - AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS ; 2 ; 1659-1668
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Verlag:
- Neue Suche nach: Curran
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Erscheinungsort:Red Hook, NY
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Erscheinungsdatum:01.01.2012
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Format / Umfang:10 pages
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Anmerkungen:Includes bibliographical references and author index
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ISBN:
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Medientyp:Aufsatz (Konferenz)
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Format:Print
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Sprache:Englisch
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Schlagwörter:
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Datenquelle:
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Inhaltsverzeichnis Konferenzband
Die Inhaltsverzeichnisse werden automatisch erzeugt und basieren auf den im Index des TIB-Portals verfügbaren Einzelnachweisen der enthaltenen Beiträge. Die Anzeige der Inhaltsverzeichnisse kann daher unvollständig oder lückenhaft sein.
- 1
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Boomerang Flight DynamicsVassberg, J. / American Institute of Aeronautics and Astronautics et al. | 2012
- 44
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Airfoil Boundary-Layer Flow Control Using Fluidic OscillatorsChoephel, T. / Coder, J. / Maughmer, M. / American Institute of Aeronautics and Astronautics et al. | 2012
- 55
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Numerical and Experimental Investigation of the Effect of Multiple Rotating Cylinders on Base Pressure of a Three Dimensional Bluff Body in Ground ProximityBell, J. / Burton, D. / McArthur, D. / Sheridan, J. / American Institute of Aeronautics and Astronautics et al. | 2012
- 66
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Application of Breathing Blunt Nose Concept to Lifting Body ConfigurationKhurana, S. / Suzuki, K. / Rathakrishnan, E. / American Institute of Aeronautics and Astronautics et al. | 2012
- 78
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Fluid-Structure Interaction and Design Optimization of HAR Wing for Endurance Efficiency of S-HALE AircraftLee, S. / Park, K.-H. / Kim, J.-H. / Jun, S.-O. / Lee, D. / American Institute of Aeronautics and Astronautics et al. | 2012
- 87
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Flexible Wing Twist Optimisation using Rapid Computational MethodsAgostinelli, C. / Allen, C. / American Institute of Aeronautics and Astronautics et al. | 2012
- 101
-
Design of a Flapped Laminar Airfoil for High Performance SailplaneKubrynski, K. / American Institute of Aeronautics and Astronautics et al. | 2012
- 121
-
On the Simulation of Complex Gusts at Low Reynolds NumbersWong, J. / Rival, D. / Mohebbian, A. / Kriegseis, J. / American Institute of Aeronautics and Astronautics et al. | 2012
- 132
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Flow Visualization in the Wake of the Flapping-Wing MAV `DelFly II' in Forward FlightPercin, M. / Eisma, J. / Van Oudheusden, B. / Remes, B. / Ruijsink, R. / De Wagter, C. / American Institute of Aeronautics and Astronautics et al. | 2012
- 144
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Experimental and Computational Analysis of High Angle of Attack Perching ManeuversLego, Z. / Altman, A. / Gunasekaran, S. / American Institute of Aeronautics and Astronautics et al. | 2012
- 161
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A Transonic Laminar-Flow Wing Glove Flight Experiment: Overview and Design OptimizationBelisle, M. / Roberts, M. / Williams, T. / Tufts, M. / Tucker, A. / Saric, W. / Reed, H. / American Institute of Aeronautics and Astronautics et al. | 2012
- 176
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A Transonic Laminar-Flow Wing Glove Flight Experiment: Computational Evaluation and Linear StabilityRoberts, M. / Reed, H. / Saric, W. / American Institute of Aeronautics and Astronautics et al. | 2012
- 195
-
Experimental Investigation of the Low-Speed Aerodynamic Characteristics of a 5.8-Percent Scale Hybrid Wing Body ConfigurationGatlin, G. / Vicroy, D. / Carter, M. / American Institute of Aeronautics and Astronautics et al. | 2012
- 219
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Passitve Wing Rotation in Flexible Flapping Wing AerodynamicsKang, C.-K. / Shyy, W. / American Institute of Aeronautics and Astronautics et al. | 2012
- 231
-
Fluid-Structure Interaction Simulation for the Design of Bio-Inspired Micro Air Vehicle WingsCombes, T. / Malik, A. / Bramesfeld, G. / American Institute of Aeronautics and Astronautics et al. | 2012
- 245
-
Static Aeroelastic Calculations for a Wing Under Large DeformationsAtik, H. / Baran, O. / Tuzun, A. / American Institute of Aeronautics and Astronautics et al. | 2012
- 254
-
The Effects of Nonlinear Bending Stiffness on the Flutter Speed and Pitch Motion of UAV with High Aspect RatioTsai, M. / American Institute of Aeronautics and Astronautics et al. | 2012
- 273
-
Glide and Powered Flight Characteristics of Micro Air Vehicles from Experimental MeasurementsRao, A. / Uhlig, D. / Selig, M. / American Institute of Aeronautics and Astronautics et al. | 2012
- 290
-
Representation of Morphing Airfoil Thickness in Dynamic Stall SimulationsAhaus, L. / Roe, R. / Peters, D. / Rong, X. / American Institute of Aeronautics and Astronautics et al. | 2012
- 302
-
Vortex Creation and Wing-Tip Geometry DependenciesBuffo, R. / Wolf, C. / Dufhaus, S. / Hornschemeyer, R. / Stumpf, E. / American Institute of Aeronautics and Astronautics et al. | 2012
- 320
-
Compact Formulation of Nonlinear Inviscid Aerodynamics for Fixed-Wing AircraftBunge, R. / Kroo, I. / American Institute of Aeronautics and Astronautics et al. | 2012
- 340
-
An Attempt to Correlate Collision Theory with Aerodynamic LiftVidhyasagar, L.S. / Kumar, V.R.S. / American Institute of Aeronautics and Astronautics et al. | 2012
- 351
-
A Computational Study on the Aerodynamic Characteristics of a Flying-Wing MAV DesignAhn, J. / Lee, D. / American Institute of Aeronautics and Astronautics et al. | 2012
- 359
-
Airfoil Designs and Free-Flight Tests of a Fixed Wing MAV DesignAhn, J. / Lee, D. / American Institute of Aeronautics and Astronautics et al. | 2012
- 367
-
CFD Based Study of Unconventional Aeroengine Exhaust SystemsCoates, T. / Page, G. / American Institute of Aeronautics and Astronautics et al. | 2012
- 394
-
The Effects of Wall Boundaries on the Flow Field of a Rotating WingSchlueter, K. / Jones, A. / American Institute of Aeronautics and Astronautics et al. | 2012
- 409
-
HPC Capabilities of the ElsA CFD Software Applied to a Counter Rotating Open Rotor Test RigBoisard, R. / Delattre, G. / Falissard, F. / American Institute of Aeronautics and Astronautics et al. | 2012
- 428
-
In-plane Airloads of a Propeller with Inflow Angle: Prediction vs. ExperimentOrtun, B. / Boisard, R. / Gonzalez-Martino, I. / American Institute of Aeronautics and Astronautics et al. | 2012
- 443
-
Efficient Solution Methods for Strand Grid ApplicationsKatz, A. / Wissink, A. / American Institute of Aeronautics and Astronautics et al. | 2012
- 465
-
Parametric Investigation of Vertical Axis Wind Turbine Aerodynamic CharacteristicsLohry, M. / Martinelli, L. / American Institute of Aeronautics and Astronautics et al. | 2012
- 474
-
CFD Analysis of Multielement Airfoils for Wind TurbinesNarsipur, S. / Pomeroy, B. / Selig, M. / American Institute of Aeronautics and Astronautics et al. | 2012
- 492
-
Evaluation of a Potential Flow Model for Wind Turbine DesignKatz, J. / Patel, B. / American Institute of Aeronautics and Astronautics et al. | 2012
- 506
-
Computational Investigation of the Sensitivity of Spoiler Attachment on Wind Turbine BladesBaker, J. / Sitaraman, J. / Masarati, P. / Quaranta, G. / American Institute of Aeronautics and Astronautics et al. | 2012
- 525
-
An Experimental Investigation on the Wake Interference of Multiple Wind Turbines in Atmospheric Boundary Layer WindsOzbay, A. / Tian, W. / Yang, Z. / Sarkar, P. / Hu, H. / American Institute of Aeronautics and Astronautics et al. | 2012
- 538
-
The Case for Counter-Rotation of Installed Contra-Rotating Open Rotor Propulsion SystemsStuermer, A. / Yin, J. / American Institute of Aeronautics and Astronautics et al. | 2012
- 558
-
Aerodynamics of Counter-Rotating Open Rotors at High SpeedBarth, M. / Calmels, B. / Aupoix, B. / American Institute of Aeronautics and Astronautics et al. | 2012
- 573
-
Validation of Actuator Disk Simulations of CROR Propulsion Systems at Low-Speed Flight ConditionsMarquez, C. / Stuermer, A. / Clemen, C. / Grimminger, A. / American Institute of Aeronautics and Astronautics et al. | 2012
- 591
-
Aerodynamics of a Swept Wing with Ice Accretion at Low Reynolds NumberDiebold, J. / Bragg, M. / Monastero, M.C. / American Institute of Aeronautics and Astronautics et al. | 2012
- 611
-
Measurement of Unsteady Flow Reattachment on an Airfoil with a Leading-Edge Horn-Ice ShapeAnsell, P. / Bragg, M. / American Institute of Aeronautics and Astronautics et al. | 2012
- 625
-
Icing Wind Tunnel Tests of a Contaminated Supercritical Anti-iced Wing Section during Simulated Take-off - Phase 2Clark, C. / Macmaster, M. / American Institute of Aeronautics and Astronautics et al. | 2012
- 640
-
NASA Trapezoidal Wing Computations Including Transition and Advanced Turbulence ModelingRumsey, C. / Lee-Rausch, E. / American Institute of Aeronautics and Astronautics et al. | 2012
- 662
-
Computational Studies of the NASA High-Lift Trap Wing Using Structured and Unstructured Grid SolversMurayama, M. / Yamamoto, K. / Ito, Y. / Tanaka, K. / American Institute of Aeronautics and Astronautics et al. | 2012
- 697
-
Transitional Flow Computations of the NASA Trapezoidal Wing with the DLR TAU CodeCrippa, S. / Krimmelbein, N. / American Institute of Aeronautics and Astronautics et al. | 2012
- 706
-
Influence of High-Lift Supporting Systems on the Trapezoidal Wing Aerodynamic CoefficientsAntunes, A. / Da Silva, R. / Azevedo, J.L. / American Institute of Aeronautics and Astronautics et al. | 2012
- 730
-
Quantification of Grid Refinement Effects for NASA High Lift Trap Wing Using Error Transport ModelCavallo, P. / Feldman, G. / American Institute of Aeronautics and Astronautics et al. | 2012
- 744
-
Investigation of Solution Methodology for Addressing Side of Body Flow SeparationMoitra, A. / Gujar, P. / Gupta, P. / American Institute of Aeronautics and Astronautics et al. | 2012
- 754
-
Unstructured Adaptive Mesh Calculations for NASA Trap Wing Using the Code HiFUNKrishnamurthy, R. / Shende, N. / Patel, S. / Narayanarao, B. / American Institute of Aeronautics and Astronautics et al. | 2012
- 769
-
CFD Analysis of a Slatted UH-60 Rotor in HoverGanti, Y. / Baeder, J. / American Institute of Aeronautics and Astronautics et al. | 2012
- 787
-
Extension of a Modern Lifting-Line Method to Transonic Speeds and Application to Multiple-Lifting-Surface ConfigurationsJacobs, R. / Ran, H. / Kirby, M. / Mavris, D. / American Institute of Aeronautics and Astronautics et al. | 2012
- 800
-
The Influence of Hole Orientation on the Aerodynamics of Battle Damaged WingsRender, P. / Pickhaver, T. / American Institute of Aeronautics and Astronautics et al. | 2012
- 814
-
Assessment of Methods for the Prediction of Parasitic Drag Due to Wing RepairsHahn, M. / Lawson, S. / Peace, A. / Miller, A. / Chant, T. / American Institute of Aeronautics and Astronautics et al. | 2012
- 835
-
Experimental Study of a Multielement Airfoil for Large Wind TurbinesPomeroy, B. / Williamson, G. / Selig, M. / American Institute of Aeronautics and Astronautics et al. | 2012
- 853
-
Mid-span PIV Measurements of a Low Aspect Ratio Circulation Control WingMiklosovic, D. / Imber, R. / Britt-Crane, M. / Colantonio, K. / American Institute of Aeronautics and Astronautics et al. | 2012
- 873
-
Investigation of Rocket Based Combined Cycle Design Modifications to Improve Cm~0 and Cm~ ~a~l~p~h~a~ at Subsonic SpeedsGuarnaccio, C. / Thompson, M. / Post, M. / Brandt, S. / American Institute of Aeronautics and Astronautics et al. | 2012
- 885
-
Effect of a Nonlinear Constitutive Relation for Turbulence Modeling on Predicting Flow Separation at Wing-Body Juncture of Transonic Commercial AircraftYamamoto, K. / Murayama, M. / Tanaka, K. / American Institute of Aeronautics and Astronautics et al. | 2012
- 899
-
Random Turbulent Flow Generation Coupled with ZDES for Civil Aircraft Jet ConfigurationsBrunet, V. / American Institute of Aeronautics and Astronautics et al. | 2012
- 919
-
Comparison of Experimental and Computational Ship Air Wakes for a Naval Research VesselSnyder, M. / Kang, H.S. / Burks, J. / American Institute of Aeronautics and Astronautics et al. | 2012
- 938
-
A Computational and Experimental Investigation of Flow over an Inflatable WingGhobadi, K. / Pifer, E. / Lebeau, R. / Bramesfeld, G. / McQuilling, M. / American Institute of Aeronautics and Astronautics et al. | 2012
- 950
-
Hybrid LES/RANS Simulations of Transonic Flowfield around a Rocket FairingTsutsumi, S. / Takaki, R. / Takama, Y. / Imagawa, K. / Nakakita, K. / Kato, H. / American Institute of Aeronautics and Astronautics et al. | 2012
- 967
-
Evaluation of Higher Order Improvement of Unstructured Schemes for Helicopter Rotor SimulationsZhao, Q. / Sheng, C. / American Institute of Aeronautics and Astronautics et al. | 2012
- 983
-
Computational Study of a Battle Damaged Finite Aspect Ratio WingYang, Z. / Samad-Suhaeb, M. / Render, P. / American Institute of Aeronautics and Astronautics et al. | 2012
- 992
-
Computational Investigation of Pitch Damping on Missile Geometries at High Angles of AttackMcGowan, G. / Kurzen, M. / Nance, R. / Carpenter, J. / Moore, F. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1009
-
Computational Investigation of Roll Damping for Missile ConfigurationsEidell, M. / McGowan, G. / Nance, R. / Carpenter, J. / Moore, F. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1022
-
Numerical Prediction of Roll Damping and Magnus Dynamic Derivatives for Finned Projectiles at Angle of AttackBhagwandin, V. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1039
-
Computational Analysis of a Spinning Fin-Stabilized ProjectileSilton, S. / Bhagwandin, V.A. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1060
-
Transient Lateral Jet Interaction Effects on a Generic Fin-Stabilized ProjectileDespirito, J. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1079
-
Measurements of the Forces and Moments Generated by Swept-back Grid FinsDebiasi, M. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1090
-
Eigenvalues and Mode Shapes for the Complete Rotor Dynamic-Wake ModelFei, Z. / Peters, D. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1101
-
A Hybrid CFD Methodology to Model the Two-phase Flowfield beneath a Hovering Laboratory Scale RotorThomas, S. / Baeder, J. / Kalra, T.S. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1121
-
A Hybrid Vortex-Particle Method for Rotorcraft ApplicationsDuque, E. / Stone, C. / Hennes, C. / Gharakhani, A. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1137
-
Numerical Investigation of Helicopter Rotors in Ground EffectKutz, B. / Kowarsch, U. / Kessler, M. / Kraemer, E. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1151
-
Aerodynamic Impacts of Helicopter Blade Erosion CoatingsCalvert, M. / Wong, T.-C. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1164
-
Effects of Model Scaling on Sediment Transport in BrownoutGlucksman-Glaser, M. / Jones, A. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1184
-
PICASSO: A Meshing Infrastructure for Strand-Cartesian CFD SolversWissink, A. / Katz, A. / Sitaraman, J. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1210
-
Application of an Unsteady Curved Lifting-Line Theory to Propeller SimulationsGonzalez-Martino, I. / Costes, M. / Rodriguez, B. / Devinant, P. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1233
-
Numerical Simulation of the NASA High-Lift Trap Wing with the elsA CFD SoftwareWiart, L. / Moens, F. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1246
-
Extended OVERFLOW Analysis of the NASA Trap Wing Wind Tunnel ModelSclafani, A. / Slotnick, J. / Vassberg, J. / Pulliam, T. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1276
-
Numerical Simulation of High Lift Trap Wing Using STAR-CCM+Shankara, P. / Snyder, D. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1290
-
Numerical Simulation of NASA Trap-Wing Model as a Colombian Contribution to the High-Lift Prediction WorkshopLopez, O. / Escobar, J. / Ochoa, N. / Mahecha, J. / Leguizamon, S. / Ramirez, S. / Jimenez, R. / Giraldo, A.M. / Silva, C. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1316
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Unsteady Flow Simulation of High-Lift Stall Hysteresis Using a Lattice Boltzmann ApproachFares, E. / Fabiano, E. / Nolting, S. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1341
-
Advanced Aerodynamic Analysis of the NASA High-Lift Trap Wing with a Moving Flap ConfigurationHolman, D.M. / Brionnaud, R. / Martinez, F.J. / Mier-Torrecilla, M. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1360
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EUROLIFT Test Case Description for the 2nd High Lift Prediction WorkshopRudnik, R. / Huber, K. / Melber-Wilkending, S. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1390
-
Knowledge-Based Airfoil Shape Optimization Using Space MappingKoziel, S. / Leifsson, L. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1400
-
Multidisciplinary Optimization of a Generic 2D High-Lift Configuration Regarding Kinematics, Aerodynamics and Flight MechanicsFranke, D. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1414
-
Optimal Shape Design for Open Rotor BladesEconomon, T. / Palacios, F. / Alonso, J. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1437
-
Investigation on Aerodynamics Behaviors at the Extreme Angle of Attack of Two-Dimensional WingLee, E.H. / Park, B.H. / Han, Y.O. / Kim, J.-H. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1448
-
A Numerical Assessment of Side Plate Effects for a Low Aspect Ratio Wind Tunnel Model with a Smart Droop Nose DeviceKuhn, T. / Lenfers, C. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1465
-
Wall-modeled Large Eddy Simulation of the McDonnell-Douglas 30P/30N High-lift Airfoil in Nearstall ConditionsBodart, J. / Larsson, J. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1476
-
A Fully Coupled Zonal RANS-LES Method for High Angle of Attack FlowGeurts, K. / Meinke, M. / Schroeder, W. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1487
-
Vortex Generation in a Low Speed Wind Tunnel and Vortex Interactions with a High-lift AirfoilHahn, D. / Scholz, P. / Radespiel, R. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1505
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Effect of Airfoil Shape and Reynolds Number on Leading Edge Vortex Shedding in Unsteady FlowsRamesh, K.K. / Ke, J. / Gopalarathnam, A. / Edwards, J. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1516
-
Low-to-Moderate Aspect Ratio Wings Tested at Low Reynolds NumbersSelig, M. / Sukumar, P. / Ananda, G.K. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1535
-
Theoretical Modeling of Leading Edge Vortices Using the Leading Edge Suction ParameterRamesh, K.K. / Gopalarathnam, A. / Granlund, K. / Ol, M. / Edwards, J. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1551
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Analysis of Steady and Unsteady Flows Past Airfoils in the Proximity of the Ground at Low Reynolds NumbersMateescu, D. / Panahi, A. / Wang, C. / Scholoz, O. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1571
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Compressibility Effects on Airfoil Aerodynamics at Low Reynolds NumbersSuwa, T. / Nose, K. / Numata, D. / Nagai, H. / Asai, K. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1584
-
An Experimental Study on Laminar Separation Bubble and Transition over an Aerofoil at Low Reynolds NumberGenc, M.S. / Akpolat, M.T. / Karasu, I. / Acikel, H.H. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1593
-
Reduction of Helicopter BVI Noise Using Active Flow Control; The Case of Vortex Street InteractionsIlie, M. / Velez, C. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1607
-
Evaluation of a Space-time Formulation of the Euler EquationsPower, E. / Rendall, T. / Allen, C. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1623
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Turbulence Modelling Effects on Tandem Cylinder Interaction Flow and Analysis of Installation Effects on Broadband Noise Using Chimera TechniqueGreschner, B. / Eschricht, D. / Mockett, C. / Thiele, F. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1644
-
A Computational Tool for Unsteady Aerodynamic Flow Simulations Coupled with Rigid Body Dynamics and ControlCamargo, J. / Lopez, O. / Ochoa-Lleras, N. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1659
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Computational Optimization of Flexible Wing Aerodynamic Performance in HoverRen, Y. / Dong, H. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1669
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Static and Dynamic Lateral Loads for a Low Aspect Ratio Wing at Low Reynolds NumbersShields, M. / Mohseni, K. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1680
-
Transition at Low-Re Numbers for UAV Type Airfoils at High Subsonic Mach NumbersCakmakcioglu, S. / Kaynak, U. / Genc, M.S. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1698
-
An Experimental Investigations into the Feasibility of Measuring Static and Dynamic Aerodynamic Derivatives in a Water TunnelErm, L. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1720
-
Optimization of Hydrofoils Using a Genetic AlgorithmCocke, T. / Moscicki, Z. / Agarwal, R. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1745
-
Adaptive Response Correction for Surrogate-Based Airfoil Shape OptimizationKoziel, S. / Leifsson, L. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1758
-
Aerodynamic Shape Optimization of a Blended Wing Body Configuration for Several Wing PlanformsMeheut, M. / Arntz, A. / Carrier, G. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1771
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Numerical Simulations of Global Instability in Separated Flows at High Mach NumberZhang, K. / Sandham, N. / Hu, Z. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1787
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A Rigorous Solution for Finite-State Inflow throughout the FlowfieldFei, Z. / Peters, D. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1799
-
Effects of Transient Aerodynamics on Vehicle Stability: A Large Eddy Simulation AnalysisYuan, C.S. / Tsubokura, M. / Nakashima, T. / Okada, Y. / Nouzawa, T. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1807
-
An Assessment of Frequency-Domain and Time-Domain Techniques for Turbomachinery AeromechanicsEkici, K. / Huang, H. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1824
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Transonic Aerodynamic Loads Modeling of X-31 AircraftGhoreyshi, M. / Da Ronch, A. / Jirasek, A. / Cummings, R. / Badcock, K. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1853
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Unsteady Aerodynamics of Road Vehicle in Dynamic ManeuveringTsubokura, M. / Kobayashi, R. / Ikawa, Y. / Nakashima, T. / Okada, Y. / Kamioka, T. / Nouzawa, T. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1871
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Novel Approach to High-Altitude, Long-Endurance StationkeepingEngblom, W. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1885
-
Modeling Turbulence Control Effect of the SINHA Flexible Composite Surface DeturbulatorWang, X. / Walters, K. / Coley, L. / Barton, M. / Sinha, S. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1898
-
Drag Components, Efficiency Parameters and Wake Structures behind a Three Dimensional Air OutletScholz, P. / Gericke, T. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1911
-
Deformation of the Upper Surface of an Airfoil by Macro Fiber Composite ActuatorsDebiasi, M. / Bouremel, Y. / Khoo, H.H. / Luo, S.C. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1923
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Adapting Some Aspects of Soaring Flight to Powered AircraftKentfield, J. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1933
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A Conceptual Study of a Transonic NLF Transport Aircraft with Forward Swept WingsKruse, M. / Wunderlich, T. / Heinrich, L. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1960
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Further Investigation of the Support System Effects and Wing Twist on the NASA Common Research ModelRivers, M. / Hunter, C. / Campbell, R.L. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1994
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Underbody Drag for Pickup TrucksMokhtar, W. / Pervez, N. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2004
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Advances in Aerodynamic Drag Extraction by Far Field MethodsLanzetta, M. / Mele, B. / Tognaccini, R. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2022
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Dominant Flow Structures in the Wake of a CyclistCrouch, T. / Sheridan, J. / Burton, D. / Thompson, M. / Brown, N. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2032
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Experimental Study on Aerodynamic Drag Characteristics by Train Underbody Shape VariationKwak, M.H. / Lee, Y. / Lee, J. / Cho, J. / Kim, K.H. / Lee, D. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2040
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3-D Inlet Shock-Boundary Layer Interactions - PIV Database for the Second SBLI WorkshopEagle, W. / Driscoll, J. / Benek, J. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2067
-
How to Accurately Measure Low Sonic Boom or Model Surface Pressure in Supersonic Wind TunnelsMorgenstern, J. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2083
-
Distortion Correction of Low Sonic Boom Measurements in Wind TunnelsMorgenstern, J. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2103
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N+2 Low Boom Wind Tunnel Model Design and ValidationMorgenstern, J. / Buonanno, M. / Norstrud, N. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2135
-
Optimum Signature Shaping for Low Sonic BoomMorgenstern, J. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2141
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Alleviation of Tail Boom with Staged Aft-bodySuzuki, K. / Imaizumi, T. / Toyoda, A. / Sasoh, A. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2152
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Sonic Boom Mitigation through Aircraft Design and Adjoint MethodologyRallabhandi, S. / Nielseny, E.J. / Diskin, B. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2170
-
High Lift-to-Drag Ratio Waveriders for Missions in the Martian AtmosphereRodi, P. / Bennett, G. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2183
-
Non-Symmetric Waverider Star Bodies for Aerodynamic Moment GenerationRodi, P. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2193
-
Preliminary Ramjet/Scramjet Integration with Vehicles Using Osculating Flowfield Waverider ForebodiesRodi, P. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2206
-
Studies of Inlet Distortion in a Direct-Connect Axisymmetric Scramjet IsolatorHsu, K.-Y. / Tam, C.-J. / Hagenmaier, M. / Raffoul, C. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2217
-
Estimation of Dynamic Stability Coefficients for Aerodynamic Decelerators Using CFDStern, E. / Gidzak, V. / Candler, G.V. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2231
-
Effects of Geometrical Parameters of Heat Shield on Flow Characteristics at Transonic Mach NumberMehta, R. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2246
-
Evaluation of Drogue Parachute Damping Effects Utilizing the Apollo Legacy Parachute ModelCurrin, K. / Gamble, J. / Matz, D. / Bretz, D. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2268
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Methods to Scale Subsonic Wind Tunnel Data to Full-ScaleKaushik, B. / Anemaat, W. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2280
-
Numerical Analysis of Wind Tunnel Wall Interference on Two-dimensional Airfoil by New Porous Wall ModelNambu, T. / Hashimoto, A. / Murakami, K. / Sato, T. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2292
-
Numerical and Experimental Investigation of the Magnus Effect in Supersonic FlowsKlatt, D. / Leopold, F. / Hruschka, R. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2302
-
An Evaluation of the Overall T-38 Wind Tunnel Data Quality in Testing of a Calibration ModelDamljanovic, D. / Rasuo, B. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2316
-
Study of the Influence of a Highly Integrated Flow-through Intake on Compressible Flows About the Lambda Wing Configuration SACCONRein, M. / Gardner, A. / Ruetten, M. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2326
-
Numerical Investigation of the Aerodynamic Properties of a Flying Wing ConfigurationHuber, K. / Schutte, A. / Rein, M. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2341
-
Numerical Flow Investigation of Morphing Leading Edges for the Enhancement of Maneuverability of Unmanned Combat Air VehiclesRutten, M. / Saalfeld, B. / Kinemund, J. / Saalfeld, S. / Rein, M. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2358
-
Unsteady Aerodynamics Modeling for Aircraft Maneuvers: A New Approach Using Time-Dependent Surrogate ModelingGhoreyshi, M. / Cummings, R. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2383
-
Numerical Simulation of Wingtip VorticesGoparaju, K. / Zhuang, M. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2392
-
Detached Eddy Simulation Compared with Wind Tunnel Results of a Delta Wing with Sharp Leading Edge and Vortex BreakdownTangermann, E. / Furman, A. / Breitsamter, C. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2403
-
LES of Helicopter Blade-vortex Interaction; The Case of Vortex Street-blade InteractionIlie, M. / Velez, C. / Coronado, P. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2415
-
Experimental/Numerical Investigation of a Wingtip Vortex in the Near-FieldO Regan, M. / Young, T. / Griffin, P. / McNicholas, G. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2423
-
Propeller Design for a Future QESTOL Aircraft in the BNF ProjectLenfers, C. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2441
-
Installation Effects of a Propeller Over a Wing with Internally Blown FlapMuller, L. / Kozulovic, D. / Radespiel, R. / Hepperle, M. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2455
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Development of Vertical Takeoff and Landing Vehicle with Flapping WingsSumita, T. / Takahashi, S. / Arai, N. / Shimoyama, K. / Jeong, S. / Obayashi, S. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2468
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Application of Statistical Techniques to Analyze and Model Trajectory Envelopes for Subscale Store Separation TestingBinkley, B. / Vanderwyst, A. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2479
-
The Aero-acoustic Environment Within the Weapons Bay of a Generic UCAVChaplin, R. / Birch, T. / American Institute of Aeronautics and Astronautics et al. | 2012
- 2505
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Different Approaches for Simulating the Flow Inside and Near a Weapons BayRokita, T. / Arieli, R. / Levy, Y. / American Institute of Aeronautics and Astronautics et al. | 2012