AIAA-2006-2603 Integrated Aero-Acoustic Rotor Simulation and Design Optimization (Englisch)
- Neue Suche nach: Xue, S.
- Neue Suche nach: Docker, B.
- Neue Suche nach: Narramore, J.
- Neue Suche nach: Han, Z.
- Neue Suche nach: American Institute of Aeronautics and Astronautics
- Neue Suche nach: CEAS
- Neue Suche nach: Xue, S.
- Neue Suche nach: Docker, B.
- Neue Suche nach: Narramore, J.
- Neue Suche nach: Han, Z.
- Neue Suche nach: American Institute of Aeronautics and Astronautics
- Neue Suche nach: CEAS
In:
Aeroacoustics
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2613-2624
;
2006
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ISBN:
- Aufsatz (Konferenz) / Print
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Titel:AIAA-2006-2603 Integrated Aero-Acoustic Rotor Simulation and Design Optimization
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Beteiligte:Xue, S. ( Autor:in ) / Docker, B. ( Autor:in ) / Narramore, J. ( Autor:in ) / Han, Z. ( Autor:in ) / American Institute of Aeronautics and Astronautics / CEAS
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Kongress:12th:; Conference, Aeroacoustics ; 2006 ; Cambridge, MA
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Erschienen in:Aeroacoustics ; 2613-2624AIAA CEAS AEROACOUSTICS CONFERENCE ; 4 ; 2613-2624
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Verlag:
- Neue Suche nach: AIAA,
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Erscheinungsdatum:01.01.2006
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Format / Umfang:12 pages
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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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AIAA-2006-2400 A Self-Powered Wireless Active Acoustic LinerKadirvel, S. / Liu, F. / Horowitz, S. / Nishida, T. / Ngo, K. / Cattafesta, L. / Sheplak, M. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 11
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AIAA-2006-2401 Experimental Study of Acoustic Impedance of MEMS-Based Micro-Perforated LinersChandrasekharan, V. / Sheplak, M. / Cattafesta, L. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 26
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AIAA-2006-2402 Cascaded Perforates as One-Dimensional, Bulk AbsorbersParrott, T. / Jones, M. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 46
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AIAA-2006-2403 Assessment of Bulk Absorber Properties for Multi-Layer Perforates in Porous Honeycomb LinersJones, M. / Parrott, T. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 67
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AIAA-2006-2404 Experimental Investigation of Nonlinear Acoustic Properties for PerforatesBoden, H. / Guo, Y. / Tozun, H. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 75
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AIAA-2006-2405 The Sound Absorbing Potential of Carbon-Graphite FoamGaeta, R. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 89
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AIAA-2006-2406 Self-Sustained Oscillations in Shock Wave/Turbulent Boundary Layer InteractionPirozzoli, S. / Grasso, F. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 103
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AIAA-2006-2407 Correlation Characteristics of the Pressure-Fluctuations at Shock-Boundary Layer InteractionEfimtsov, B. / Kozlov, N. / Andersson, A. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 113
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AIAA-2006-2408 Sound and Vibration Produced by an Airfoil Tip in a Turbulent Boundary Layer Flow with an Elastic End WallSlaboch, P. / Morris, S. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 121
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AIAA-2006-2409 Rough Wall Boundary Layer NoiseGrissom, D. / Smith, B. / Devenport, W. / Glegg, S. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 137
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AIAA-2006-2410 Characteristic Lifelength of Coherent Structure in the Turbulent Boundary LayerPalumbo, D. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 153
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AIAA-2006-2411 Sound Level Effect on Perforated Panel Boundary Layer GrowthGallman, J. / Drouin, M. / Olsen, R. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 166
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AIAA-2006-2412 Prediction of Boundary Layer Sound Radiation from Wall Shear Stresses Using DNS DataHu, Z. / Morfey, C. / Sandham, N. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 176
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AIAA-2006-2413 Shock-Capturing Dissipation Schemes for High-Accuracy Computational Aeroacoustics (CAA) CodesHixon, R. / Bhate, D. / Nallasamy, M. / Sawyer, S. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 187
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AIAA-2006-2414 Aeroacoustic Computations Using a High Order Shock Capturing SchemeDaru, V. / Gloerfelt, X. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 190
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AIAA-2006-2415 A New High-Resolution Balance-Characteristic Method for AeroacousticsKarabasov, S. / Goloviznin, V. / Kozubskaya, T. / Abalakin, I. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 205
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AIAA-2006-2416 Non-Reflecting Boundary Conditions for One-Step LBM Simulation of AeroacousticsKam, E. / So, R. / Leung, R. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 214
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AIAA-2006-2417 CAA Using 3D CESE Method with a Simplified Courant Number Insensitive SchemeYen, J. / Duell, E. / Martindale, W. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 231
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AIAA-2006-2418 Aeroacoustic Simulations for Complex Geometries Based on Hybrid MeshesLorcher, F. / Utzmann, J. / Dumbser, M. / Munz, C. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 251
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AIAA-2006-2419 The Influence of Flow Domain Modeling on the Accuracy of Direct and Hybrid Aeroacoustic Noise CalculationsDe Roeck, W. / Rubio, G. / Baelmans, M. / Sas, P. / Desmet, W. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 272
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AIAA-2006-2420 The Prediction of Fan Exhaust Noise PropagationZhao, Y. / Morris, P. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 288
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AIAA-2006-2421 Numerical Prediction of Propagation and Radiation of Aft Fan and Core Nozzle NoiseArina, R. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 296
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AIAA-2006-2423 A 3D Parabolic Equation Method for Wind Turbine Noise Propagation in Moving Inhomogeneous AtmosphereCheng, R. / Morris, P. / Brentner, K. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 310
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AIAA-2006-2424 Leading Edge NoiseGlegg, S. / Staubs, J. / Devenport, W. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 341
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AIAA-2006-2426 A Parametric Study of Nonlinear Gust-Airfoil InteractionGolubev, V. / Mankbadi, R. / Visbal, M. / Scott, J. / Hixon, R. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 354
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AIAA-2006-2427 Analysis of Control Concepts for Cavity FlowsArunajatesan, S. / Kannepalli, C. / Sinha, N. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 364
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AIAA-2006-2428 Flow Field Dynamics in Open Cavity FlowsMurray, N. / Ukeiley, L. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 380
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AIAA-2006-2429 An Investigation into Supersonic Swept Cavity FlowsGai, S. / Samanes, E. / Milthorpe, J. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 390
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AIAA-2006-2430 Coupling of a Jet-Slot Oscillator With the Flow-Supply Duct: Flow-Acoustic Interaction ModelingGlesser, M. / Billon, A. / Valeau, V. / Sakout, A. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 399
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AIAA-2006-2431 Two and Three Dimensional Simulations of Supersonic Cavity FlowKim, H. / Aradag, S. / Knight, D. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 417
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AIAA-2006-2432 Compressible POD/Galerkin Reduced-Order Model of Self-Sustained Oscillations in a CavityGloerfelt, X. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 445
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AIAA-2006-2433 Aeroacoustic Computations of High-Reynolds Number Cavity Flows on Staggered GridsGloerfelt, X. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 466
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AIAA-2006-2434 Reducing Propulsion Airframe Aeroacoustic Interactions with Uniquely Tailored Chevrons: 2. Installed NozzlesMengle, V. / Elkoby, R. / Brusniak, L. / Thomas, R. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 480
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AIAA-2006-2435 Reducing Propulsion Airframe Aeroacoustic Interactions with Uniquely Tailored Chevrons: 3. Jet-Flap InteractionMengle, V. / Brusniak, L. / Elkoby, R. / Thomas, R. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 495
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AIAA-2006-2436 Computational Analysis of a Chevron Nozzle Uniquely Tailored for Propulsion Airframe AeroacousticsMassey, S. / Elmiligui, A. / Hunter, C. / Thomas, R. / Pao, P. / Mengle, V. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 518
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AIAA-2006-2437 Novel In-flight Noise Analysis SystemHutto, F. / Bultemeier, E. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 523
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AIAA-2006-2438 Flight Test Results for Uniquely Tailored Propulsion-Airframe Aeroacoustic Chevrons: Community NoiseNesbitt, E. / Mengle, V. / Callender, B. / Thomas, R. / Czech, M. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 536
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AIAA-2006-2439 Flight Test Results for Uniquely Tailored Propulsion-Airframe Aeroacoustic Chevrons: Shockcell NoiseMengle, V. / Ganz, U. / Nesbitt, E. / Bultemeier, E. / Thomas, R. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 553
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AIAA-2006-2440 Effect of Uniform Chevrons on Cruise Shockcell NoiseBultemeier, E. / Ganz, U. / Premo, J. / Nesbitt, E. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 568
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AIAA-2006-2441 A Comparative Use of the PSE and LES Approaches for Jet Noise PredictionsPiot, E. / Casalis, G. / Muller, F. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 581
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AIAA-2006-2442 An Approach to Improve High Frequency Noise Prediction in LES of JetsWu, X. / Page, G. / McGuirk, J. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 594
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AIAA-2006-2443 Computation of the Noise Radiated by Jets with Laminar/Turbulent Nozzle-Exit ConditionsBarre, S. / Bogey, C. / Bailly, C. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 609
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AIAA-2006-2444 Phased-Array Imaging of Jet Noise Sources in a Large-Eddy SimulationBrusniak, L. / Shur, M. / Spalart, P. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 628
-
AIAA-2006-2445 Computation of the Flow and Noise of Round and Beveled NozzlesViswanathan, K. / Shur, M. / Strelets, M. / Spalart, P. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 658
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AIAA-2006-2447 Direct Computation of the Sound Generated by Isothermal and Non-Isothermal Mixing LayersMoser, C. / Lamballais, E. / Gervais, Y. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 671
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AIAA-2006-2449 Accurate Prediction of Sonic Boom SignalsPilon, A. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 681
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AIAA-2006-2450 Effect of Pressure Distortion and Sampling Rate on Shaped Sonic Boom PredictionsLaflin, K. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 694
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AIAA-2006-2451 Ray Tracing for Long Range Atmospheric Propagation of InfrasoundGainville, O. / Blanc-Benon, P. / Piserchia, P. / Scott, J. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 695
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AIAA-2006-2452 Sonic Boom Prediction: A New Empirical Formulation and Animated Graphical ModelClare, A. / Oman, R. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 709
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AIAA-2006-2453 Acoustic Characterization of a Pulse Detonation EngineGlaser, A. / Caldwell, N. / Gutmark, E. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 720
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AIAA-2006-2455 Zero Splice Intake Technology and Acoustic BenefitsGantie, F. / Batard, H. / Baker, N. / Schwaller, P. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 729
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AIAA-2006-2456 Far-field Directivity of Rotor-Alone Tones Radiated From Fan Intakes with Spliced Liners for Different Intake Shapes, with FlowTester, B. / De Mercato, L. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 747
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AIAA-2006-2458 Quiet Technology Demonstrator 2 Intake Liner Design and ValidationYu, J. / Nesbitt, E. / Kwan, H. / Uellenberg, S. / Chien, E. / Premo, J. / Ruiz, M. / Czech, M. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 760
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AIAA-2006-2459 Scattering of Acoustic Duct Modes by Axial Liner SplicesTam, C. / Ju, H. / Chien, E. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 784
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AIAA-2006-2460 Nonlinear Modeling of Shock Wave Trains in Ducts with Wall DiscontinuitiesAlonso, J. / Anderson, J. / Burdisso, R. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 798
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AIAA-2006-2461 Application of a Piston Radiation Model to Liner Non-Uniformities and Rigid SplicesAlonso, J. / Burdisso, R. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 808
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AIAA-2006-2462 Static and Flight Aeroacoustic Evaluations of a Scarf InletWeir, D. / Bouldin, B. / Mendoza, J. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 827
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AIAA-2006-2463 Aero-Engine Noise Investigated from Flight TestsGuerin, S. / Michel, U. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 839
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AIAA-2006-2464 Reduction of Approach Noise of the MD-11Siller, H. / Michel, U. / Zwiener, C. / Saueressig, G. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 852
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AIAA-2006-2465 Measurement of Approach Noise Footprints of a C-17 STOL Aircraft During Conventional and Noise-Mitigating Approach TrajectoriesHorne, W. / Burnside, N. / Kitaplioglu, C. / Schein, D. / Welborn, A. / Liddle, A. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 872
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AIAA-2006-2467 Reducing Propulsion Airframe Aeroacoustic Interactions with Uniquely Tailored Chevrons: 1. Isolated NozzlesMengle, V. / Elkoby, R. / Brusniak, L. / Thomas, R. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 890
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AIAA-2006-2468 Computational Analysis of the Effect of Porosity on Shock Cell Strength at CruiseMassey, S. / Elmiligui, A. / Thomas, R. / Pao, P. / Abdol-Hamid, K. / Hunter, C. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 908
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AIAA-2006-2469 Optimized Boundary Compact Finite Difference Schemes for Computational AeroacousticsKim, J. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 922
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AIAA-2006-2471 Analysis of Aeroacoustic Wave Propagation Simulations Using a Higher-Order Accurate MethodEfraimsson, G. / Biela, C. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 932
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AIAA-2006-2472 Applications of Dual-Time Stepping and Finite-Volume Schemes in Computational AeroacousticsLin, W. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 947
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AIAA-2006-2473 Improving an Unstructured CFD Solver for Aeroacoustics ApplicationsGeuzaine, P. / Georges, L. / Bogaerts, S. / Hillewaert, K. / Caro, S. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 952
-
AIAA-2006-2474 Noise Scattering by the Blended Wing Body Airplane: Measurements and PredictionReimann, C. / Tinetti, A. / Dunn, M. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 969
-
AIAA-2006-2475 Prediction of Sound Scattered by Moving Bodies with Applications to Propeller-Driven AirplanesTesta, C. / Gennaretti, M. / Iemma, U. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 981
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AIAA-2006-2476 Experimental Investigation Into Trailing Edge Noise SourcesGarcia-Sagrado, A. / Hynes, T. / Hodson, H. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1003
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AIAA-2006-2477 Incident Turbulence Interaction Noise from an Axial FanFedala, D. / Kouidri, S. / Rey, R. / Carolus, T. / Schneider, M. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1014
-
AIAA-2006-2479 Noise Validation of Model Fan Rig with EngineSchwaller, P. / Baker, N. / Tomlinson, D. / Sijtsma, P. / Hemmings, R. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1026
-
AIAA-2006-2480 Space-Time Correlations and Trailing Edge Flow Structure in Fan-Blade Wakes with Trailing Edge BlowingBorgoltz, A. / Devenport, W. / Craig, L. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1055
-
AIAA-2006-2483 Leapfrogging of Two Vortex-Rings as Test Case for Volume Source ComputationsJacob, M. / Benyahia, A. / Casalino, D. / Eschricht, D. / Thiele, F. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1068
-
AIAA-2006-2484 A Look Inside the Lighthill Source TermCabana, M. / Fortune, V. / Jordan, P. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1087
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AIAA-2006-2485 From Primitive-Variable Boundary-Integral Formulation to FWH EquationMorino, L. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1097
-
AIAA-2006-2486 Propagation and Stability of Vorticity-Entropy Waves in a Nonuniform FlowAtassi, O. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1122
-
AIAA-2006-2488 Evaluation of Far-Field Sound with Open Surface Corrections to Lighthill's EquationCheung, L. / Lele, S. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1137
-
AIAA-2006-2489 Direct Simulation of Acoustic Waves Emitted from Moving Bodies by the Finite Difference Lattice Boltzmann MethodTamura, A. / Tsutahara, M. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1146
-
AIAA-2006-2490 TBL Noise Generated by a Simplified Side Mirror Configuration and Acoustic Transfer Through the Window: Modelling Using Actran and FluentCaro, S. / Ramonda, A. / Perot, F. / Vergne, S. / Pechabat, M. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1169
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AIAA-2006-2491 Interior Noise Sources Identifications, In-Flight Measurements and Numerical Correlations of an Advanced Business AircraftMarulo, F. / Sollo, A. / Aversano, M. / Russo, G. / Polito, T. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1176
-
AIAA-2006-2492 Hermite High-Order Finite Elements for Aeroacoustic AnalysisMorino, L. / Cetta, F. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1189
-
AIAA-2006-2493 Simulation of Aero-acoustic Sources in Aircraft Climate Control SystemsMathey, F. / Morin, O. / Caruelle, B. / Debatim, K. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1198
-
AIAA-2006-2494 Experimental and Numerical Investigation of a Flow-Induced Cavity Resonance with Application to Automobile BuffetingCrouse, B. / Senthooran, S. / Freed, D. / Balasubramanian, G. / Gleason, M. / Puskarz, M. / Lew, P. / Mongeau, L. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1216
-
AIAA-2006-2495 Investigating Broadband Shock-Associated Noise of Axisymmetric Jets Using Large-Eddy SimulationBodony, D. / Ryu, J. / Ray, P. / Lele, S. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1227
-
AIAA-2006-2496 Large Eddy Simulation of Screech Tone Generation in a Planar Underexpanded JetBerland, J. / Bogey, C. / Bailly, C. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1251
-
AIAA-2006-2497 Large-Eddy Simulation of Hot Coaxial JetsTristanto, I. / Page, G. / McGuirk, J. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1264
-
AIAA-2006-2499 High Frequency Noise Generation in the Near-Nozzle Region of a JetUzun, A. / Hussaini, M. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1296
-
AIAA-2006-2500 Investigation Of The Noise From Cold And Heated Subsonic JetsMoore, P. / Boersma, B. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1306
-
AIAA-2006-2501 Adjoint-Based Control of the Noise from a Turbulent Mixing LayerKleinman, R. / Freund, J. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1316
-
AIAA-2006-2502 Numerical Simulation of the Generation of Airfoil Tones at Moderate Reynolds NumbersTam, C. / Ju, H. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1339
-
AIAA-2006-2503 Direct Noise Computation Around a 3-D NACA 0012 AirfoilMarsden, O. / Bogey, C. / Bailly, C. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1350
-
AIAA-2006-2504 Direct Numerical Simulation of Noise from an Airfoil in a Uniform FlowHatakeyama, N. / Inoue, O. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1361
-
AIAA-2006-2505 Computation of Trailing-Edge Noise Using a Zonal RANS-LES Approach and Acoustic AnalogyMathey, F. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1369
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AIAA-2006-2507 Transmission of Acoustic Perturbation Through Cavity/Slots in an Airfoil for Stall ControlZaman, K. / Culley, D. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1381
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AIAA-2006-2508 Cavity Noise Generation for Circular and Rectangular Vent HolesCzech, M. / Crouch, J. / Stoker, R. / Strelets, M. / Garbaruk, A. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1394
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AIAA-2006-2509 Generic Wind Tunnel Study on Side Edge NoiseDrobietz, R. / Borchers, I. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1405
-
AIAA-2006-2510 Effects of Surface Roughness on Airframe NoiseLiu, Y. / Dowling, A. / Shin, H. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1426
-
AIAA-2006-2511 Unsteady Boundary Control for Optimal Control of Trailing Edge NoiseChen, G. / Hussaini, M. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1443
-
AIAA-2006-2512 A Combined RANS/Vortex Method for Predicting Noise from Vortex/Airfoil InteractionsZheng, Z. / Xu, Y. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1451
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AIAA-2006-2513 Prediction of Flat Plate Self-NoiseChang, K. / Seo, J. / Moon, Y. / Roger, M. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1465
-
AIAA-2006-2514 DNS of Trailing-Edge Noise Generated by Boundary-Layer InstabilitiesSandberg, R. / Sandham, N. / Joseph, P. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1478
-
AIAA-2006-2515 Aeroacoustic Study of Airfoil Leading Edge High-Lift DevicesAndreou, C. / Graham, W. / Shin, H. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1491
-
AIAA-2006-2516 Prediction of Sound Generated by a Pitching Airfoil: A Comparison of RANS and LESNagarajan, S. / Hahn, S. / Lele, S. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1504
-
AIAA-2006-2517 The Computational Investigation of Resonant Sound-Absorbing Structures ModelsBaklanov, V. / Zayakin, A. / Orlenko, E. / Postnov, S. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1509
-
AIAA-2006-2518 Investigation of Vortex Sound Propagation Using a FE ImplementationEscobar, M. / Kaltenbacher, M. / Ali, I. / Becker, S. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1520
-
AIAA-2006-2519 Simulation of Acoustic Fields in Resonator-Type Problems Using Unstructured MeshesAbalakin, I. / Gorobets, A. / Kozubskaya, T. / Mironov, A. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1530
-
AIAA-2006-2520 Validation and Application of a Hybrid Prediction Scheme for Bypass Duct NoiseSugimoto, R. / Astley, J. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1543
-
AIAA-2006-2521 PML Absorbing Boundary Condition for Nonlinear Aeroacoustics ProblemsHu, F. / Li, X. / Lin, D. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1558
-
AIAA-2006-2522 Cartesian Cut-Cell Method with Local Grid Refinement for Wave ComputationsPopescu, M. / Shyy, W. / Tai, C. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1577
-
AIAA-2006-2523 A Statistical Approach to Optimum Design of Inlet Acoustic TreatmentZlavog, G. / Eversman, W. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1602
-
AIAA-2006-2524 Optimization of an Electromechanical Helmholtz ResonatorLiu, F. / Horowitz, S. / Cattafesta, L. / Sheplak, M. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1614
-
AIAA-2006-2525 Optimisation of Traditional and Blown Liners for a Silent AircraftLaw, T. / Dowling, A. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1631
-
AIAA-2006-2527 Comparison of Time-Domain Impedance Boundary Conditions by Lined Duct FlowsRichter, C. / Thiele, F. / Li, X. / Zhuang, M. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1652
-
AIAA-2006-2528 A Computational Mode Matching Approach for Propagation in Three-Dimensional Ducts with FlowAstley, R. / Hii, V. / Gabard, G. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1675
-
AIAA-2006-2529 Investigation of a Single-Point Nonlinearity Indicator in the Propagation of High-Amplitude Jet NoiseFalco, L. / Atchley, A. / Gee, K. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1681
-
AIAA-2006-2530 On the Perception of Crackle in Noise Radiated from Military Jet AircraftGee, K. / Sparrow, V. / Atchley, A. / Gabrielson, T. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1690
-
AIAA-2006-2531 Measurement and Prediction of Noise Propagation from a High-Power Jet AircraftGee, K. / Sparrow, V. / James, M. / Downing, J. / Hobbs, C. / Gabrielson, T. / Atchley, A. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1698
-
AIAA-2006-2532 Density Fluctuations in a Supersonic JetStern, C. / Aguilar, C. / Alvarado, M. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1705
-
AIAA-2006-2533 An Experimental Investigation of Density Gradient Fluctuations in High-Speed Jets Using Optical DeflectometryPetitjean, B. / McLaughlin, D. / Morris, P. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1722
-
AIAA-2006-2534 Effect of Heat on Space-Time Correlations in JetsBridges, J. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1738
-
AIAA-2006-2535 Experimental and Numerical Investigation of the Near Field Pressure of a High Subsonic Hot JetMuller, F. / Vuillot, F. / Rahier, G. / Casalis, G. / Piot, E. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1752
-
AIAA-2006-2536 Wake Acoustic Analysis and Image Decomposition via Beamforming of Microphone Signal Projections on Wavelet SubspacesWassaf, H. / Zhang, Y. / Ibe, O. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1768
-
AIAA-2006-2537 Use of a Commercial Wind SODAR for Measuring Wake VorticesMackey, S. / Burnham, D. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1779
-
AIAA-2006-2538 Influence of Vortex Core on Wake Vortex Sound EmissionZheng, Z. / Li, W. / Wang, F. / Wassaf, H. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1793
-
AIAA-2006-2539 Atmospheric Effects on Microphone Array Analysis of Aircraft Vortex SoundWassaf, H. / Hardin, J. / Wang, F. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1802
-
AIAA-2006-2540 Scale Model Testing of Infrasound Produced by Various Jet Engine Test Cell ConfigurationsHatlestad, K. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1809
-
AIAA-2006-2542 A Contribution to the Understanding and Prediction of Jet Noise Generation by Forced Mixers: Part III ApplicationsTester, B. / Fisher, M. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1831
-
AIAA-2006-2543 An MDOE Assessment of Nozzle Vanes for High Bypass Ratio Jet Noise ReductionHenderson, B. / Norum, T. / Bridges, J. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1841
-
AIAA-2006-2546 Variable Geometry Chevrons for Jet Noise ReductionCalkins, F. / Butler, G. / Mabe, J. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1852
-
AIAA-2006-2550 Measurement of Acoustic Quantity Fields in Duct Flow by Laser Doppler VelocimetryLavieille, M. / Simon, F. / Micheli, F. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1861
-
AIAA-2006-2551 RACE Aero Acoustic Test Facility: Fan Forward and Rearward 3D Noise MeasurementsGenoulaz, N. / Julliard, J. / Lozachmeur, C. / Caujolle, C. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1879
-
AIAA-2006-2553 Potential Errors Introduced in the use of Static Engine Noise Data not Acquired in Geometric FarfieldAhuja, K. / Turkdogru, N. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1895
-
AIAA-2006-2554 A Method to Account for Engine Noise Component Source LocationsSalikuddin, M. / Stimpert, D. / Majjigi, R. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1912
-
AIAA-2006-2555 Numerical Study of Aeroacoustic Oscillations in a Transonic Flow Downstream a Sudden Duct EnlargementEmmert, T. / Lafon, P. / Bailly, C. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1925
-
AIAA-2006-2558 The Sub-Critical Flow Past a Generic Side Mirror and its Impact on Sound Generation and PropagationAsk, J. / Davidson, L. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1945
-
AIAA-2006-2559 Prediction of Wall Pressure Fluctuations on an Automobile Side-Glass Using a Lattice Boltzmann MethodSenthooran, S. / Crouse, B. / Noelting, S. / Freed, D. / Duncan, B. / Balasubramanian, G. / Powell, R. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1960
-
AIAA-2006-2560 Simulation of the Acoustics Behind a Wall Due to a Moving VehicleAberg, M. / Szasz, R. / Fuchs, L. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1972
-
AIAA-2006-2561 Localisation of Flap Edge Sound Sources by Use of Spectral Analysis and Flow InvestigationTiedemann, C. / Neuwerth, G. / Henke, R. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 1986
-
AIAA-2006-2562 Low Noise Design Trends Derived from Wind Tunnel Testing on Advanced High-Lift DevicesFischer, M. / Friedel, H. / Holthusen, H. / Golling, B. / Emunds, R. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2001
-
AIAA-2006-2563 Effect of Blade Design at Equal Loading on Broadband NoiseRozenberg, Y. / Roger, M. / Moreau, S. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2021
-
AIAA-2006-2564 Airframe Noise Prediction by Acoustic Analogy: RevisitedFarassat, F. / Casper, J. / Tinetti, A. / Dunn, M. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2045
-
AIAA-2006-2565 Phased Array Measurement of High Lift Devices in Low Speed Wind TunnelUra, H. / Yokokawa, Y. / Ito, T. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2056
-
AIAA-2006-2566 Acoustic Beamforming and Holography Measurements of Modified Boundary Layer Trailing-Edge NoiseFaszer, A. / Hynes, T. / Blaabjerg, C. / Shin, H. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2069
-
AIAA-2006-2567 Airframe Noise Characteristics from Flyover Measurements and PredictionPott-Pollenske, M. / Dobrzynski, W. / Buchholz, H. / Guerin, S. / Saueressig, G. / Finke, U. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2083
-
AIAA-2006-2568 Dicontinuous Galerkin Method for Computational AeroacousticsPeyret, C. / Delorme, P. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2091
-
AIAA-2006-2569 Discontinuous Galerkin Implementation of the Extended Helmholtz Resonator Model in Time DomainChevaugeon, N. / Remacle, J. / Gallez, X. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2111
-
AIAA-2006-2570 Direct Simulation of Acoustic Waves by Finite Volume Lattice Boltzmann MethodTsutahara, M. / Kondo, T. / Mochizuki, K. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2120
-
AIAA-2006-2571 Fundamental Aeroacoustic Capabilities of the Lattice-Boltzmann MethodCrouse, B. / Freed, D. / Senthooran, S. / Balasubramanian, G. / Lew, P. / Mongeau, L. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2137
-
AIAA-2006-2572 A Hermite-Taylor Algorithm for Simulating Subsonic Shear FlowsHagstrom, T. / Goodrich, J. / Zhu, G. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2151
-
AIAA-2006-2573 Aerodynamic Noise Prediction for Long-Span BodiesSeo, J. / Chang, K. / Moon, Y. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2167
-
AIAA-2006-2574 An Attempt to Calculate Acoustic Directivity Using LBMLeung, R. / So, R. / Kam, E. / Li, X. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2175
-
AIAA-2006-2575 Rotational Effects on the Aerodynamics and Aeroacoustics of Wind Turbine AirfoilsMiller, S. / Morris, P. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2189
-
AIAA-2006-2576 Large Eddy Simulation of Gust Noise Sources in a Low Pressure Axial CompressorReese, H. / Kato, C. / Carolus, T. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2204
-
AIAA-2006-2577 Acoustic Monitoring of Axial Compressor Rotor Blade VibrationsAnderson, J. / Bailie, S. / Ng, W. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2221
-
AIAA-2006-2578 Noise Reduction and Efficiency Improvement Through Vane Indexing of a Two-Stage TurbineBlaszczak, J. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2230
-
AIAA-2006-2579 Sound Generation in Centrifugal CompressorsRaitor, T. / Neise, W. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2249
-
AIAA-2006-2580 Procedure for Separating Noise Sources in Measurements of Turbofan Engine Core NoiseMiles, J. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2265
-
AIAA-2006-2581 Restricted Acoustic Modal Analysis Applied to Internal Combustor Spectra and Cross-Spectra MeasurementsMiles, J. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2292
-
AIAA-2006-2582 Sound Transmission in Strongly-Curved Slowly-Varying Cylindrical and Annular Lined Ducts with FlowBrambley, E. / Peake, N. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2310
-
AIAA-2006-2583 Continuous Spectrum Growth and Modal Instability in Swirling Duct FlowHeaton, C. / Peake, N. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2325
-
AIAA-2006-2584 Mode Matching in Engine Ducts with Vortical FlowsVilenski, G. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2336
-
AIAA-2006-2585 Development and Validation of a 3D Linearized Euler SolverLan, J. / Breard, C. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2361
-
AIAA-2006-2586 Further Investigation of Acoustic Propagation Codes for Three-Dimensional GeometriesNark, D. / Watson, W. / Jones, M. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2378
-
AIAA-2006-2587 CDUCT-LaRC Status - Shear Layer Refraction, and Noise RadiationNark, D. / Farassat, F. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2397
-
AIAA-2006-2588 New Advances in the Use of Actran/TM for Nacelle Simulations and Optimisation of IBM Clusters for Actran Parallel ComputationsMosson, A. / Caro, S. / Gontier, M. / Knapen, T. / Enault, L. / Drouilhet-Peyre, S. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2409
-
AIAA-2006-2589 A study in the near pressure field of co-axial subsonic jetsTinney, C. / Jordan, P. / Coiffet, F. / Guitton, A. / Delville, J. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2432
-
AIAA-2006-2590 Superdirective Acoustic Radiation by Vortex Pairing in Subsonic Excited JetsFleury, V. / Bailly, C. / Juve, D. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2448
-
AIAA-2006-2592 Noise Generation Mechanisms in Single and Coaxial JetsGroschel, E. / Schroder, W. / Meinke, M. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2466
-
AIAA-2006-2593 Comparison of Jet Noise ModelsAfsar, M. / Dowling, A. / Karabasov, S. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2480
-
AIAA-2006-2595 Experimental Validation of Instability Wave Theory for Round Supersonic JetKopiev, V. / Chernyshev, S. / Zaitsev, M. / Kuznetsov, V. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2504
-
AIAA-2006-2596 Prediction of Noise from High Speed Subsonic Jets Using an Acoustic AnalogyRaizada, N. / Morris, P. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2526
-
AIAA-2006-2597 Unstructured CFD and Noise Prediction Methods for Propulsion Airframe AeroacousticsPao, S. / Abdol-Hamid, K. / Campbell, R. / Hunter, C. / Massey, S. / Elmiligui, A. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2542
-
AIAA-2006-2598 Improved Jet Noise Modeling Using a New Acoustic Time ScaleAzarpeyvand, M. / Self, R. / Golliard, J. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2553
-
AIAA-2006-2599 RANS-Based Noise Predictions of Jets with Internal Forced MixersGarrison, L. / Lyrintzis, A. / Blaisdell, G. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2574
-
AIAA-2006-2600 Noise Predictions for Chevron Nozzle FlowsBirch, S. / Lyubimov, D. / Maslov, V. / Secundov, A. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2584
-
AIAA-2006-2601 Pulsed Microjet Control of Supersonic Impinging Jets: A Reduced-Order ModelChoi, J. / Annaswamy, A. / Alvi, F. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2598
-
AIAA-2006-2602 A Review of Axisymmetric Jet Flow Data for Noise ApplicationsBirch, S. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2613
-
AIAA-2006-2603 Integrated Aero-Acoustic Rotor Simulation and Design OptimizationXue, S. / Docker, B. / Narramore, J. / Han, Z. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2625
-
AIAA-2006-2604 Helicopter Interior Noise Reduction by Using Active Gearbox StrutsHoffmann, F. / Maier, R. / Janker, P. / Hermle, F. / Berthe, A. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2635
-
AIAA-2006-2605 On Propeller Acoustics Design Synthesis Using Source Distributions Along Blade SpanCampos, L. / Lau, F. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2651
-
AIAA-2006-2606 Aeroelastic Modeling Effect in Rotor BVI Noise PredictionBernardini, G. / Serafini, J. / Ianniello, S. / Gennaretti, M. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2660
-
AIAA-2006-2607 Vortex-Shedding Noise and Potential-Interaction Noise Modeling by a Reversed Sears' ProblemRoger, M. / Moreau, S. / Guedel, A. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2678
-
AIAA-2006-2608 Numerical Analysis of Noise Scattering Effects Due to the Airframe in Tilt Rotor SystemsCasalino, D. / Genito, M. / Visingardi, A. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2694
-
AIAA-2006-2609 Comparison of Noise Reduction Effect Between AFC and Conventional IBC by Moving Overlapped Grid MethodAoyama, T. / Yang, C. / Kondo, N. / Saito, S. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2706
-
AIAA-2006-2610 The Influence of the Flame Structure on the Combustion Oscillations in a Cylindrical ChamberLacava, P. / Carvalho, J. / Ferreira, D. / Ferreira, M. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2716
-
AIAA-2006-2611 Adaptive Control of a Combustion Acoustics Model with Input Saturation Using Control HedgingBansal, R. / Ananthkrishnan, N. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2731
-
AIAA-2006-2612 Premixed Combustion Noise: Measurements and CorrelationsRajaram, R. / Gray, J. / Lieuwen, T. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2740
-
AIAA-2006-2613 Experimental and Numerical Investigation of the Acoustic Field in a Bluff Body CombustorSivakumar, R. / Chakravarthy, S. / Babu, V. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2753
-
AIAA-2006-2614 Prediction of Combustion-Generated Noise in Non-Premixed Turbulent Jet Flames Using LESIhme, M. / Bodony, D. / Pitsch, H. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2769
-
AIAA-2006-2615 Time Resolved Combustion Noise Investigation Based on a Wave Equation ApproachFlemming, F. / Freitag, M. / Sadiki, A. / Janicka, J. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2782
-
AIAA-2006-2617 Aft Fan Noise Shielding by Lifting Surfaces: Analytical, Numerical and Experimental ResultsChappuis, J. / Ricouard, J. / Roger, M. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2799
-
AIAA-2006-2618 A Ray Tracing Approach to Calculate Acoustic Shielding by the Silent Aircraft AirframeAgarwal, A. / Dowling, A. / Shin, H. / Graham, W. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2819
-
AIAA-2006-2619 Aircraft Conceptual Design and Risk Analysis Using Physics-Based Noise PredictionOlson, E. / Mavris, D. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2841
-
AIAA-2006-2620 Auralisation of Turbofan Engine Noise ComponentsShin, H. / Hall, C. / Crichton, D. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2855
-
AIAA-2006-2621 Optimal Conceptual Design of Aircraft Including Community Noise PredictionIemma, U. / Diez, M. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2865
-
AIAA-2006-2622 The Low-Noise Potential of Distributed Propulsion on a Catamaran AircraftPosey, J. / Dunn, M. / Tinetti, A. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2878
-
AIAA-2006-2623 Prediction of Low Noise Aircraft Landing Gears and Comparison with Test ResultsMolin, N. / Piet, J. / Chow, L. / Smith, M. / Dobrzynski, W. / Seror, C. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2888
-
AIAA-2006-2625 Aerodynamic Measurements of the 777 Main Landing Gear ModelRingshia, A. / Ravetta, P. / Ng, W. / Burdisso, R. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2902
-
AIAA-2006-2626 Control of Noise Sources on Aircraft Landing Gear BogiesSmith, M. / Fenech, B. / Chow, L. / Molin, N. / Dobrzynski, W. / Seror, C. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2912
-
AIAA-2006-2627 A Semi-Empirical Model for Aircraft Landing Gear Noise PredictionGuo, Y. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2931
-
AIAA-2006-2628 Prediction of Sound Generated by a Rod-Airfoil Configuration Using a Cubic Explicit Algebraic Stress Model for Detached Eddy Simulation and the Generalised Lighthill/FW-H AnalogyGreschner, B. / Gurr, A. / Thiele, F. / Casalino, D. / Jacob, M. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2943
-
AIAA-2006-2629 Noise Radiation from Single and Multiple Rods ConfigurationsHutcheson, F. / Brooks, T. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2967
-
AIAA-2006-2631 A Hybrid RANS/LES Approach for Predicting Jet NoiseGoldstein, M. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2980
-
AIAA-2006-2632 An Assessment of Filtering Techniques for High-Order Aeroacoustics SimulationsAl-Qadi, I. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 2986
-
AIAA-2006-2633 Large Eddy Simulations of Low-Mach Number Aeroacoustics for Complex Wall-Bounded Turbulent Flows via a Multiblock/Characteristic Interface ApproachSuh, J. / Frankel, S. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3010
-
AIAA-2006-2634 An Optimized Large-Stencil Approach for Capturing Near-Pl FrequenciesGhasemi, A. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3023
-
AIAA-2006-2635 A Computational Method of Evaluating Non-Compact Sound Based on the Vortex Sound TheoryTakaishi, T. / Miyazawa, M. / Kato, C. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3037
-
AIAA-2006-2636 An Investigation of Spectral Collocation Boundary Element Method for the Computation of Exact Green's Function in Acoustic AnalogyJones, A. / Hu, F. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3054
-
AIAA-2006-2637 Development of an Experimental Rig for Investigation of Higher Order Modes in DuctsGerhold, C. / Cabell, R. / Brown, M. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3073
-
AIAA-2006-2638 Optimization of Sensor Arrays for Radial Mode Analysis in Flow DuctsTapken, U. / Enghardt, L. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3093
-
AIAA-2006-2639 Validation of an Inverse Analytical Technique to Educe Liner Impedance with Grazing FlowElnady, T. / Boden, H. / Musharraf, M. / Elhadidi, B. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3108
-
AIAA-2006-2640 Development and Qualification of an In-Situ Grazing Flow Impedance Measurement TechniqueSimonich, J. / Narayanan, S. / Morin, B. / Patrick, W. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3119
-
AIAA-2006-2641 Turbofan Duct-Mode Identification Using Farfield Noise Measurements and Numerical PredictionsVenditti, D. / Ali, A. / Mehdizadeh, O. / Joshi, N. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3131
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AIAA-2006-2642 Fan Inlet Mode Detection from Measurements of the Radiated Sound FieldCastres, F. / Joseph, P. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3145
-
AIAA-2006-2643 Comparison of a Convected Helmholtz and Euler Model for Impedance Eduction in FlowWatson, W. / Jones, M. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3168
-
AIAA-2006-2644 Localization of Multiple Types of Jet Noise SourcesPapamoschou, D. / Dadvar, A. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3185
-
AIAA-2006-2645 Acoustic Efficiency of Azimuthal Modes in Jet Noise Using Chevron NozzlesBrown, C. / Bridges, J. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3199
-
AIAA-2006-2646 Coherent Noise Radiation from a Jet Investigated with a Beam-Forming TechniqueSuzuki, T. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3213
-
AIAA-2006-2647 Phased-Array Study of Dual-Flow Jet Noise: Effect of Nozzles and MixersLee, S. / Bridges, J. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3248
-
AIAA-2006-2648 Dynamics of Free Jets Modulated by Plane Acoustic Waves: Part 1. ExperimentsBirbaud, A. / Durox, D. / Ducruix, S. / Candel, S. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3264
-
AIAA-2006-2649 Experimental Study of the Properties of Near-Field and Far-Field Jet NoiseBarre, S. / Fleury, V. / Bogey, C. / Bailly, C. / Juve, D. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3278
-
AIAA-2006-2650 Noise Sources in Controlled High Reynolds Number and High Speed JetsKastner, J. / Kim, J. / Samimy, M. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3291
-
AIAA-2006-2651 Design and Implementation of a Phased Microphone Array in a Closed-Section Wind TunnelShin, H. / Graham, W. / Sijtsma, P. / Andreou, C. / Faszer, A. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3303
-
AIAA-2006-2652 A Large Polar Array for Full-Scale Aero-Engine Noise Source Location and BreakdownBattaner-Moro, J. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3315
-
AIAA-2006-2653 Phased-Array Measurement of Modern Regional Aircraft Turbofan Engine NoiseLee, S. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3337
-
AIAA-2006-2654 Extension of DAMAS Phased Array Processing for Spatial Coherence Determination (DAMAS-C)Brooks, T. / Humphreys, W. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3355
-
AIAA-2006-2656 Combined PSP and Microphone Array Measurements for Analysis of Unsteady FlowsLong, D. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3365
-
AIAA-2006-2657 Analysis and Test of Spacecraft Structural Response Under Launch Acoustic EnvironmentCheng, M. / Shyu, R. / Cheng, D. / Hsiao, C. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3373
-
AIAA-2006-2658 The Computational Investigation of Low-Frequency Vibroisolation Mounting Dynamic ModelBaklanov, V. / Postnov, S. / Zayakin, A. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3378
-
AIAA-2006-2659 Probabilistic Finite Elements for Vibroacoustic ApplicationsPolito, T. / Marulo, F. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3388
-
AIAA-2006-2661 Nonlinear Vibration of Clamped 2024-T3 Aluminum Panels Subject to High Intensity NoiseBurgess, B. / Frendi, K. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3396
-
AIAA-2006-2662 Smart Tuneable Dynamic Vibration AbsorbersTiseo, B. / Concilio, A. / Koopmann, G. / Gianvito, A. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3405
-
AIAA-2006-2663 Numerical Simulation of the System "Engine-Mounting-Airframe" According to Experimental Data ResultsBaklanov, V. / Denisov, S. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3413
-
AIAA-2006-2664 Effects of Geometric Details on Slat Noise Generation and PropagationKhorrami, M. / Lockard, D. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3439
-
AIAA-2006-2665 Effect of Slat Settings (Gap and Overlap) on Slat Noise Based on a Test Vortex Injected Upstream of the SLAT-HookEmunds, R. / Fischer, M. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3454
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AIAA-2006-2666 Attenuation of Slat Trailing Edge Noise Using Slat Gap Acoustic LinersSmith, M. / Chow, L. / Molin, N. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3465
-
AIAA-2006-2667 Slat Noise Trend Predictions Using CAA with Stochastic Sound Sources from a Random Particle Mesh Method (RPM)Ewert, R. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3498
-
AIAA-2006-2668 3D Unsteady Flow Computations in a Slat Cove Using Large Eddy SimulationImamura, T. / Enomoto, S. / Yamamoto, K. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3513
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AIAA-2006-2670 Dynamics of Free Jets Modulated by Plane Acoustic Waves: Part 2. Numerical SimulationsBirbaud, A. / Ducruix, S. / Durox, D. / Candel, S. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3530
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AIAA-2006-2672 Contrasting Code Performances for Computational Aeroacoustics of JetsTucker, P. / Coupland, J. / Eastwood, S. / Liu, Y. / Jefferson-Loveday, R. / Hassan, O. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3550
-
AIAA-2006-2673 Adjoint Linearised Euler Solver in the Frequency Domain for Jet Noise ModellingKarabasov, S. / Hynes, T. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3564
-
AIAA-2006-2674 A Nonlinear Shock-Refracted Acoustic Wave Model for the Prediction of Screech Amplitude in Underexpanded Supersonic JetsKandula, M. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3580
-
AIAA-2006-2675 A Numerical Study of Nozzle Boundary Layer Thickness on Axisymmetric Supersonic Jet Screech TonesGao, J. / Li, X. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3592
-
AIAA-2006-2676 Determination of Combustor Noise from a Modern Regional Aircraft Turbofan EngineMartinez, M. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3611
-
AIAA-2006-2677 Narrowband Model for Gas Turbine Engine Combustion Noise PredictionSchuster, B. / Lieber, L. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3624
-
AIAA-2006-2678 Source Term Evaluation of the APE-RF SystemBui, P. / Meinke, M. / Schroder, W. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3635
-
AIAA-2006-2681 Folding Cavity Acoustic Liner For Combustion Noise ReductionYu, J. / Chien, E. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3645
-
AIAA-2006-2683 The Effect of Blade Loading on Sound Sources in a Ducted RotorStephens, D. / Morris, S. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3657
-
AIAA-2006-2684 Fan Broadband Noise SimulationTester, B. / Sijtsma, P. / Joseph, P. / Lowis, C. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3674
-
AIAA-2006-2685 Time-Domain Impedance Formulation Based on Recursive ConvolutionReymen, Y. / Baelmans, M. / Desmet, W. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3688
-
AIAA-2006-2686 Impedance Models in Time Domain, Including the Extended Helmholtz Resonator ModelRienstra, S. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3708
-
AIAA-2006-2687 Aero-Acoustics of Flow Duct Singularities at Low Mach NumbersAbom, M. / Allam, S. / Boij, S. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3718
-
AIAA-2006-2688 Surface-Waves, Stability, and Scattering for a Lined Duct with FlowBrambley, E. / Peake, N. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3746
-
AIAA-2006-2689 Time-Domain Characterization of Acoustic Liner in a DuctFung, K. / Yang, X. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3769
-
AIAA-2006-2690 Sound Propagation in Ducts Lined with Porous Materials by Multimode Propagation MethodBi, W. / Lafarge, D. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3778
-
AIAA-2006-2691 On the Propagation of Plane Acoustic Waves in a Duct with Flexible and Impedance WallsFrendi, K. / Vu, B. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3795
-
AIAA-2006-2692 Validation of a CAA Formulation Based on Lighthill's Analogy Using AcuSolve and Actran/LA on an Idealized Automotive HVAC Blower and on an Axial FanCaro, S. / Sandboge, R. / Shakib, F. / Ambs, R. / Schillemeit, B. / Washburn, K. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3813
-
AIAA-2006-2694 Adaptive Mesh Refinement Computation of Acoustic Radiation from an Engine IntakeHuang, X. / Zhang, X. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3826
-
AIAA-2006-2695 Comparison of the Two Microphone Method and the Modal Decomposition Method for Acoustic Impedance TestingSchultz, T. / Cattafesta, L. / Sheplak, M. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3839
-
AIAA-2006-2696 Experimental Training and Validation of a System for Aircraft Acoustic Signature IdentificationQuaranta, V. / Dimino, I. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3849
-
AIAA-2006-2699 Sound Generation by Flow Around Simple Geometries: Simulation and ExperimentBecker, S. / Kaltenbacher, M. / Ali, I. / Escubar, M. / Hahn, C. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3864
-
AIAA-2006-2700 Aeroacoustic Noise Source Mechanisms in Simple Expansion ChambersRubio, G. / De Roeck, W. / Baelmans, M. / Sas, P. / Desmet, W. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3873
-
AIAA-2006-2701 Numerical Analysis of a Blast Wave Using CFD-CAA Hybrid MethodLee, I. / Lee, D. / Ko, S. / Kang, G. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3882
-
AIAA-2006-2702 Extent of Nonlinear Aeroacoustic Propagation from Single Frequency-Domain Noise MeasurementsLundberg, W. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3885
-
AIAA-2006-2703 Toward Noise Mitigation in High Speed and High Reynolds Number Jets Using Plasma ActuatorsSamimy, M. / Kim, J. / Adamovich, I. / Utkin, Y. / Kastner, J. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3902
-
AIAA-2006-2704 Experiments on High-Speed Jets from Thrust Vectoring Rectangular NozzlesLee, J. / Goss, A. / McLaughlin, D. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3917
-
AIAA-2006-2705 Effect of microjets on a high-subsonic jet. Parametric study of far-field noise reductionCastelain, T. / Sunyach, M. / Bera, J. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3928
-
AIAA-2006-2706 Aeroacoustic Improvements to Fluidic Chevron NozzlesHenderson, B. / Kinzie, K. / Whitmire, J. / Abeysinghe, A. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3937
-
AIAA-2006-2707 Effect of Nozzle Geometry on Jet Noise Reduction Using Fan Flow DeflectorsPapamoschou, D. / Shupe, R. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3957
-
AIAA-2006-2709 Modeling of Piezoelectric Actuators for Active Control of Jet NoiseButler, G. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3973
-
AIAA-2006-2710 A Focused Beamformer Technique for Separating Rotor and Stator-Based Broadband SourcesLowis, C. / Joseph, P. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 3987
-
AIAA-2006-2711 A Comparison of Iterative Deconvolution Algorithms for the Mapping of Acoustic SourcesEhrenfried, K. / Koop, L. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 4006
-
AIAA-2006-2713 Noise Source Localization and Optimization of Phased Array ResultsRavetta, P. / Burdisso, R. / Ng, W. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 4029
-
AIAA-2006-2714 Acoustic Source Localization in Aircraft Interiors Using Microphone Array TechnologiesSklanka, B. / Tuss, J. / Buehrle, R. / Klos, J. / Williams, E. / Valdivia, N. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 4036
-
AIAA-2006-2715 Acoustic Imaging of Aircraft Noise Sources Using Large Aperture Phased ArraysBrusniak, L. / Underbrink, J. / Stoker, R. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 4056
-
AIAA-2006-2717 New Noise Source Mechanism of Flow/Surface Interaction as Applied to Airframe Noise ReductionKopiev, V. / Zaitsev, M. / Ostrikov, N. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 4075
-
AIAA-2006-2718 Sound Radiation from an Annular Duct with Jet Flow and a Lined CenterbodyDemir, A. / Rienstra, S. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 4076
-
AIAA-2006-2719 Far-Field Evaluation of the Noise Radiated by a Side Mirror Using LES and Acoustic AnalogyPosson, H. / Perot, F. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006
- 4079
-
AIAA-2006-2720 The Quiet Technology Demonstrator Program: Flight Validation of Airplane Noise-Reduction ConceptsHerkes, W. / Olsen, R. / Uellenberg, S. / American Institute of Aeronautics and Astronautics / CEAS et al. | 2006