2012-2658 Blowing Strategies of Pylon-Propeller Configuration for Noise Reduction Using Numerical Approach (English)
- New search for: Chelius, A.
- New search for: Nasr, N.B.
- New search for: Rodriguez, B.
- New search for: American Institute of Aeronautics and Astronautics
- New search for: Chelius, A.
- New search for: Nasr, N.B.
- New search for: Rodriguez, B.
- New search for: American Institute of Aeronautics and Astronautics
In:
AIAA flow control conference
;
15-32
;
2012
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ISBN:
- Conference paper / Print
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Title:2012-2658 Blowing Strategies of Pylon-Propeller Configuration for Noise Reduction Using Numerical Approach
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Contributors:Chelius, A. ( author ) / Nasr, N.B. ( author ) / Rodriguez, B. ( author ) / American Institute of Aeronautics and Astronautics
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Conference:6th, AIAA flow control conference ; 2012 ; New Orleans, Louisiana
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Published in:AIAA flow control conference ; 15-32
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Publisher:
- New search for: Curran
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Place of publication:New York
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Publication date:2012-01-01
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Size:18 pages
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Remarks:Includes bibliographic references and index
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ISBN:
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Type of media:Conference paper
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Type of material:Print
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Language:English
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Keywords:
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Source:
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Table of contents conference proceedings
The tables of contents are generated automatically and are based on the data records of the individual contributions available in the index of the TIB portal. The display of the Tables of Contents may therefore be incomplete.
- 1
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2012-2657 Performance Enhancement of a Vertical Stabilizer Using Synthetic Jet Actuators: Non-Zero SideslipRathay, N. / Boucher, M. / Amitay, M. / Whalen, E. / American Institute of Aeronautics and Astronautics et al. | 2012
- 15
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2012-2658 Blowing Strategies of Pylon-Propeller Configuration for Noise Reduction Using Numerical ApproachChelius, A. / Nasr, N.B. / Rodriguez, B. / American Institute of Aeronautics and Astronautics et al. | 2012
- 33
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2012-2679 On the Role of Global Flow Instability Analysis in Closed Loop Flow ControlLiu, Q. / He, W. / Gomez, F. / American Institute of Aeronautics and Astronautics et al. | 2012
- 46
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2012-2680 Laminar Separation Bubble Manipulation with Dynamic RoughnessWallace, R. / McKeon, B. / American Institute of Aeronautics and Astronautics et al. | 2012
- 59
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2012-2681 Low Reynolds Number Airfoil Stall Suppression with Dynamic RoughnessHuebsch, W. / Rothmayer, A. / Hu, H. / Grager, T. / American Institute of Aeronautics and Astronautics et al. | 2012
- 70
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2012-2682 Control of Laminar Separation Bubble Using Electro-Active PolymersZaremski, S. / Weddle, A. / Zhang, L. / Amitay, M. / American Institute of Aeronautics and Astronautics et al. | 2012
- 81
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2012-2683 Airfoil Stall Suppression Using Rectangular Bubble Burst Control Plate and Sensor ActuatorsRinoie, K. / Komuro, T. / Nakamkura, Y. / Sunada, Y. / American Institute of Aeronautics and Astronautics et al. | 2012
- 97
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2012-2684 An Experimental Study of Acoustic Disturbances Effect on Laminar Separation Bubble and Transition over an Aerofoil at Low Reynolds NumberGenc, M.S. / Karasu, I. / American Institute of Aeronautics and Astronautics et al. | 2012
- 107
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2012-2737 On Gasdynamic Instabilities Supported by Non-Equilibrium Plasma in a Supersonic FlowDenison, M. / Massa, L. / American Institute of Aeronautics and Astronautics et al. | 2012
- 122
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2012-2801 Flight and Wind Tunnel Tests of Closed-Loop Active Flow ControlKing, R. / Heinz, N. / Bauer, M. / Grund, T. / Nitsche, W. / American Institute of Aeronautics and Astronautics et al. | 2012
- 137
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2012-2802 Multivariable Closed-Loop Flow Control of Drag and Yaw Moment for a 3D Bluff BodyPfeiffer, J. / King, R. / American Institute of Aeronautics and Astronautics et al. | 2012
- 151
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2012-2803 Closed-Loop Performance Control of DBD Plasma ActuatorsKriegseis, J. / Schroter, D. / Grundmann, S. / Tropea, C. / American Institute of Aeronautics and Astronautics et al. | 2012
- 161
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2012-2804 Active Flow Control of a Pitching Turret Flow Field Using Closed-Loop Feedback ControlShea, P. / Glauser, M. / Carlson, H. / Verberg, R. / Schmit, R. / American Institute of Aeronautics and Astronautics et al. | 2012
- 177
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2012-2805 Transient Aerodynamic Response to Leading Edge Flow ControlPackard, N. / Bons, J. / American Institute of Aeronautics and Astronautics et al. | 2012
- 191
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2012-2806 Slat Noise Feedback Control with a Dielectric Barrier Discharge Plasma ActuatorChappell, S. / Cai, Z. / Zhang, X. / Angland, D. / American Institute of Aeronautics and Astronautics et al. | 2012
- 206
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2012-2807 Simultaneous Drag Reduction and Kinetic Energy Density of the Plane Poiseuille FlowDao, X.-Q. / Collewet, C. / American Institute of Aeronautics and Astronautics et al. | 2012
- 217
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2012-2808 Detection and Transient Dynamics Modeling of Experimental Hypersonic Inlet UnstartHutchins, K. / Akella, M. / Clemens, N. / Donbar, J. / American Institute of Aeronautics and Astronautics et al. | 2012
- 235
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2012-2809 Experimental Study and Plasma Control of an Unstarting Supersonic FlowIm, S.-k. / Do, H. / Mungal, G. / Cappelli, M. / American Institute of Aeronautics and Astronautics et al. | 2012
- 245
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2012-2810 Control of Oblique Shock Wave-Boundary Layer Interactions Using Plasma ActuatorsWebb, N. / Clifford, C. / Porter, A. / Samimy, M. / American Institute of Aeronautics and Astronautics et al. | 2012
- 263
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2012-2811 Adjoint Optimization of Mass, Momentum and Energy Addition in Steady Supersonic FlowLimbach, C. / Martinelli, L. / Miles, R. / American Institute of Aeronautics and Astronautics et al. | 2012
- 280
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2012-2812 Comparison of Micro-Vortex Generators in Supersonic FlowsNolan, W. / Babinsky, H. / American Institute of Aeronautics and Astronautics et al. | 2012
- 293
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2012-2813 Experiments on Resonance Enhanced Pulsed Microjet Actuators in Supersonic CrossflowTopolski, M. / Solomon, J. / Alvi, F. / American Institute of Aeronautics and Astronautics et al. | 2012
- 305
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2012-2814 SparkJet Actuator Characterization in Supersonic Cross FlowEmerick, T. / Ali, M. / Foster, C. / Alvi, F. / Cybyk, B. / American Institute of Aeronautics and Astronautics et al. | 2012
- 325
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2012-2815 Wave Drag Reduction of Blunt Bodies Using Laser Sustained Energy Deposition in Argon AtmosphereSperber, D. / Eckel, H.-a. / Fasoulas, S. / American Institute of Aeronautics and Astronautics et al. | 2012
- 335
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2012-2944 Effect of DBD Plasma Actuator Geometry and Excitation for Producing Transient Growth Modes in a Laminar Boundary LayerOsmokrovic, L. / Hanson, R. / Lavoie, P. / American Institute of Aeronautics and Astronautics et al. | 2012
- 346
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2012-2945 Transition Delay Using DBD Plasma Actuators in Direct Frequency ModeKurz, A. / Grundmann, S. / Tropea, C. / Forte, M. / Seraudie, A. / Arnal, D. / Goldin, N. / King, R. / American Institute of Aeronautics and Astronautics et al. | 2012
- 355
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2012-2946 Development of Active Wave Cancellation using DBD Plasma Actuators for In-flight Transition ControlKurz, A. / Grundmann, S. / Tropea, C. / Goldin, N. / King, R. / American Institute of Aeronautics and Astronautics et al. | 2012
- 361
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2012-2947 Separation Control Using Dielectric Barrier Discharge-Induced Suction and Vortex GenerationIm, S.-k. / Bak, M.S. / Mungal, G. / Cappelli, M. / American Institute of Aeronautics and Astronautics et al. | 2012
- 369
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2012-2948 Interaction of a Finite-Span Synthetic-Jet and a Cross-Flow over a Sweptback Finite WingVasile, J. / Amitay, M. / American Institute of Aeronautics and Astronautics et al. | 2012
- 391
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2012-2949 Efficiency of Slotted Jet Actuators at High Subsonic Mach NumbersSonnemann, D. / Pickel, C. / Muller, J. / Kahler, C. / American Institute of Aeronautics and Astronautics et al. | 2012
- 405
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2012-2951 Experimental Studies of DBD Actuator Effects on Wing Tip Vortex TopologyLeroy, A. / Pons, J. / Molton, P. / Carpels, Y. / American Institute of Aeronautics and Astronautics et al. | 2012
- 419
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2012-2952 Active Control of a Wing Tip Vortex with a Dielectric Barrier Discharge Plasma ActuatorChappell, S. / Angland, D. / American Institute of Aeronautics and Astronautics et al. | 2012
- 434
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2012-2953 Vortex Dynamics of a Tangent Ogive at High Angle of AttackSeidel, J. / Porter, C. / Fagley, C. / Farnsworth, J. / McLaughlin, T. / American Institute of Aeronautics and Astronautics et al. | 2012
- 447
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2012-2954 Effects of the Plasma Actuation on the Asymmetric Vortex around an Ogive Body at High IncidenceLee, E. / Lee, J.-I. / Lee, K.-S. / Seidel, J. / Fagley, C. / Porter, C. / McLaughlin, T. / American Institute of Aeronautics and Astronautics et al. | 2012
- 459
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2012-2955 The Transient Response of a von Karman Ogive to Open Loop Plasma ActuationFarnsworth, J. / Fagley, C. / Porter, C. / Seidel, J. / McLaughlin, T. / American Institute of Aeronautics and Astronautics et al. | 2012
- 475
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2012-2956 Plasma Control for a Maneuvering Low-Aspect-Ratio Wing at Low Reynolds NumberRizzetta, D. / Visbal, M. / American Institute of Aeronautics and Astronautics et al. | 2012
- 500
-
2012-2957 Study of the Wake of a Circular Cylinder under Spatially and Temporally Modulated Plasma ActuationBhattacharya, S. / Gregory, J. / American Institute of Aeronautics and Astronautics et al. | 2012
- 519
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2012-2958 Investigation and Active Control of Bluff Body Vortex Shedding Using Plasma ActuatorsKoc, I. / Britcher, C. / Wilkinson, S. / American Institute of Aeronautics and Astronautics et al. | 2012
- 530
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2012-3041 A Generic Automotive Aftbody Separation Control Using MicrojetsMcNally, J. / Fernandez, E. / Kumar, R. / Alvi, F. / American Institute of Aeronautics and Astronautics et al. | 2012
- 541
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2012-3042 Numerical Simulation of Flow over a Submerged Hemispherical Flat-Window TurretMorgan, P. / Visbal, M. / American Institute of Aeronautics and Astronautics et al. | 2012
- 561
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2012-3043 Interaction of a Single Synthetic Jet with a Finite Aspect Ratio Circular CylinderDemauro, E. / Leong, C. / Amitay, M. / American Institute of Aeronautics and Astronautics et al. | 2012
- 580
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2012-3044 Circulation Control of a Circular Cylinder by Tangential BlowingCaraway, D. / Hayashibara, S. / Duque, E. / American Institute of Aeronautics and Astronautics et al. | 2012
- 599
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2012-3045 CFD Investigation of the Drag Effects of Heating and Cooling Cylinders in CrossflowMarquart, J. / Endicott, D. / Dear, C. / American Institute of Aeronautics and Astronautics et al. | 2012
- 610
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2012-3046 Optimal Sensor Arrangement for Asymmetric Vortex State Estimation on a Slender Body at High IncidenceFagley, C. / Seidel, J. / Farnsworth, J. / Porter, C. / McLaughlin, T. / American Institute of Aeronautics and Astronautics et al. | 2012
- 620
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2012-3047 Response of Passive Surface Hairs in Steady Falkner-Skan Boundary LayersMcClain, S. / Case, L. / Dickinson, B. / American Institute of Aeronautics and Astronautics et al. | 2012
- 632
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2012-3048 The Dynamic Response of Quasi-Steady Hair-Like Structures in Oscillatory Boundary Layer FlowsDickinson, B. / McClain, S. / Case, L. / American Institute of Aeronautics and Astronautics et al. | 2012
- 644
-
2012-3049 Numerical Study on Flow Characteristics of Synthetic Jets with Rectangular and Circular ExitsKim, M. / Lee, B. / Kim, C. / Jung, K.J. / American Institute of Aeronautics and Astronautics et al. | 2012
- 663
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2012-3050 Separation Control Characteristics of Synthetic Jets with Circular Exit ArrayLee, B. / Kim, M. / Lee, J. / Kim, C. / Jung, K.J. / American Institute of Aeronautics and Astronautics et al. | 2012
- 688
-
2012-3051 Utilizing Vortex Acceleration to Improve the Efficiency of Air Jet Vortex GeneratorsShun, S. / Ahmed, N. / American Institute of Aeronautics and Astronautics et al. | 2012
- 702
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2012-3052 Unsteady Forcing of a Post-Stall Flow Over a NACA0012 Airfoil by a Surface DBD ActuatorPierre, A. / Hong, D. / Leroy, A. / American Institute of Aeronautics and Astronautics et al. | 2012
- 711
-
2012-3053 Numerical Investigation of Plasma Actuator Configurations for Flow Separation Control at Multiple Angles of AttackWest, T. / Hosder, S. / American Institute of Aeronautics and Astronautics et al. | 2012
- 731
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2012-3054 Burst Frequency Effect of DBD Plasma Actuator on the Control of Separated Flow over an AirfoilAsada, K. / Fujii, K. / American Institute of Aeronautics and Astronautics et al. | 2012
- 743
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2012-3094 Influence of the N~2/O~2 Volumetric Ratio on the Behavior of a SDBD Plasma ActuatorPierre, A. / Rabat, H. / Hong, D. / Leroy, A. / American Institute of Aeronautics and Astronautics et al. | 2012
- 753
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2012-3135 Combustion Powered Actuators for Separation Control (Invited)Crittenden, T. / Woo, G.T. / Glezer, A. / American Institute of Aeronautics and Astronautics et al. | 2012
- 771
-
2012-3136 EHD Force and Electric Wind Produced by Plasma Actuators Used for Airflow Control (Invited)Benard, N. / Moreau, E. / American Institute of Aeronautics and Astronautics et al. | 2012
- 818
-
2012-3137 Nanosecond Pulse Surface Discharges for High-Speed Flow Control (Invited)Adamovich, I. / Little, J. / Nishihara, M. / Takashima, K. / Samimy, M. / American Institute of Aeronautics and Astronautics et al. | 2012
- 852
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2012-3138 Shear Layer Characteristics of the Supersonic Free and Impinging JetsDavis, T. / Kumar, R. / Alvi, F. / American Institute of Aeronautics and Astronautics et al. | 2012
- 863
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2012-3139 Examining Passive Flow Control Devices with High Speed Shadowgraph Images around a Mach1.5 Cavity Flow FieldSchmit, R. / Semmelmayer, F. / Haverkamp, M. / Grove, J. / Ahmed, A. / American Institute of Aeronautics and Astronautics et al. | 2012
- 882
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2012-3140 Active Flow Control Upon Cavities at Low Reynolds NumbersDelnero, J. / Maranon, J. / Martinez, M. / Colman, J. / Sainz, M.G. / Camocardi, M.E. / American Institute of Aeronautics and Astronautics et al. | 2012
- 900
-
2012-3141 Large-eddy Simulation of Small-scale Actuation over Backward-facing StepJavadi, A. / Khalili, A. / American Institute of Aeronautics and Astronautics et al. | 2012
- 911
-
2012-3236 Characterization of Nanosecond Pulse Driven Dielectric Barrier Discharge Plasma Actuators for Aerodynamic Flow ControlDawson, R. / Little, J. / American Institute of Aeronautics and Astronautics et al. | 2012
- 924
-
2012-3237 Characterization of Corner Plasma Actuators for Pulsed Jet ProductionMellinger, S. / Weissinger, T. / McLaughlin, T. / Stephen, E. / American Institute of Aeronautics and Astronautics et al. | 2012
- 942
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2012-3238 Jet Vectoring and Enhancement of Flow Control Performance of Trielectrode Plasma Actuator Utilizing Sliding DischargeMatsuno, T. / Kawaguchi, M. / Fujita, N. / Yamada, G. / Kawazoe, H. / American Institute of Aeronautics and Astronautics et al. | 2012
- 953
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2012-3239 Numerical Simulation of Fluidic Actuators for Flow Control ApplicationsVatsa, V. / Koklu, M. / Wygnanski, I. / American Institute of Aeronautics and Astronautics et al. | 2012
- 970
-
2012-3240 Studies on the Resonance-Enhanced Micro-Actuator with Active StructuresKreth, P. / Gustavsson, J. / Alvi, F. / Oates, W. / American Institute of Aeronautics and Astronautics et al. | 2012
- 989
-
2012-3241 A Comparative Study of Two Methods for Driving Electrodynamic Zero Net Mass Flux ActuatorsSawant, S. / Eskinazi, I. / Sheplak, M. / Cattafesta, L. / Arnold, D. / American Institute of Aeronautics and Astronautics et al. | 2012
- 998
-
2012-3242 Development of Design Methodology for Synthetic Jet Actuator Array for Flow Separation Control ApplicationsJabbal, M. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1016
-
2012-3243 Vortex Interaction of In-Line Synthetic Jets Injected at Difference Phase in Low Reynolds Number Cross FlowHonami, S. / Motosuke, M. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1024
-
2012-3244 Improving Rudder Effectiveness with Sweeping Jet ActuatorsSeele, R. / Graff, E. / Gharib, M. / Taubert, L. / Wygnanski, I. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1036
-
2012-3245 High-Lift Enhancement Using Active Flow ControlDesalvo, M. / Whalen, E. / Glezer, A. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1054
-
2012-3246 Aerodynamic Control Using Distributed BleedKearney, J. / Glezer, A. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1071
-
2012-3247 Numerical Investigation of Separation Control for Wing SectionsGross, A. / Fasel, H. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1090
-
2012-3248 Effect of Microjet-Spacing on the Control of a Highly Separated FlowfieldFernandez, E. / Kumar, R. / Alvi, F. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1107
-
2012-3249 Experimental Detection and Pulsed Jets Control of Turbulent Boundary Layer SeparationChabert, T. / Dandois, J. / Garnier, E. / Jacquin, L. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1127
-
2012-3250 Flow Control by Pulsed Jet in a Highly Bended S-ductGarnier, E. / Leplat, M. / Monnier, J.C. / Delva, J. / American Institute of Aeronautics and Astronautics et al. | 2012
- 1144
-
2012-3251 A New Linear High Speed Compressor Stator Cascade for Active Flow Control InvestigationsTiedemann, C. / Heinrich, A. / Peitsch, D. / American Institute of Aeronautics and Astronautics et al. | 2012