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Program For Monday, 08-May-2006
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0800 - 0900 |
Keynote Address
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President's Ballroom A-C |
| Meeting Environmental Challenges for Airplane Design - A Boeing Perspective |
| Speaker/s: D. Anderson, Boeing Commercial Airplanes, Seattle, WA |
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| Session
1-
AA-1
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Acoustic Liner Concepts and Materials
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Crispus Attucks |
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Chaired by: M. JONES, NASA Langley Research Center, Hampton, VA
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0900
AIAA-2006-2400
A Self- Powered Wireless Active Acoustic Liner
S. Kadirvel, F. Liu, S. Horowitz, T. Nishida, K. Ngo, L. Cattafesta, and M. Sheplak, University of Florida, Gainesville, FL
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0930
AIAA-2006-2401
Experimental Study of Acoustic Impedance of MEMS- Based
Micro- Perforated Liners
V. Chandrasekharan, M. Sheplak, and L. Cattafesta, University of Florida, Gainesville, FL
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1000
AIAA-2006-2402
Cascaded Perforates as One- Dimensional, Bulk Absorbers
T. Parrott and M. Jones, NASA Langley Research Center, Hampton, VA
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1030
AIAA-2006-2403
Assessment of Bulk Absorber Properties for Multi- Layer Perforates in Porous Honeycomb Liners
M. Jones and T. Parrott, NASA Langley Research Center, Hampton, VA
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1100
AIAA-2006-2404
Experimental Investigation of Nonlinear Acoustic Properties for Perforates
H. Bodén, Y. Guo, and H. Tözün, Royal Institute of Technology, Stockholm, Sweden
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1130
AIAA-2006-2405
The Sound Absorbing Potential of Carbon- Graphite Foam
R. Gaeta, Georgia Tech Research Institute, Smyrna, GA
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| Session
2-
AA-2
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Acoustic/Fluid Dynamic Phenomena: Boundary Layer
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Cambridge |
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Chaired by: A. AGARWAL, University of Cambridge, Cambridge, Great Britain
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0900
AIAA-2006-2406
Self- Sustained Oscillations in Shock Wave/Turbulent Boundary Layer Interaction
S. Pirozzoli and F. Grasso, University of Rome “La Sapienza”, Rome, Italy
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0930
AIAA-2006-2407
Correlation characteristics of the pressure- fluctuations at
shock- boundary layer interaction
B. Efimtsov and N. Kozlov, TsAGI, Moscow, Russia; and A. Andersson, The Boeing Company, Seattle, WA
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1000
AIAA-2006-2408
Sound and Vibration Produced by an Airfoil Tip in a Turbulent Boundary Layer Flow with an Elastic End Wall
P. Slaboch and S. Morris, University of Notre Dame, Notre Dame, IN
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1030
AIAA-2006-2409
Rough Wall Boundary Layer Noise
D. Grissom, B. Smith, and W. Devenport, Virginia Polytechnic Institute and State University, Blacksburg, VA; and S. Glegg, Florida Atlantic University, Boca Raton, FL
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1100
AIAA-2006-2410
Characteristic Lifelength of Coherent Structure in the
Turbulent Boundary Layer
D. Palumbo, NASA Langley Research Center, Hampton, VA
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1130
AIAA-2006-2411
Sound Level Effect on Perforated Panel Boundary Layer Growth
M. Drouin and J. Gallman, Spirit AeroSystems, Wichita, KS; and R. Olsen, The Boeing Company, Renton, WA
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1200
AIAA-2006-2412
Prediction of Boundary Layer Sound Radiation from Wall Shear Stresses Using DNS Data
Z. Hu, C. Morfey and N. Sandham, University of Southampton, Southampton, Great Britain
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| Session
3-
AA-3
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CAA Methods I
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Paul Revere B |
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Chaired by: D. HIXON, University of Toledo, Fairview Park, OH
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0900
AIAA-2006-2413
Shock- Capturing Dissipation Schemes for High- Accuracy Computational Aeroacoustics (CAA) Codes
R. Hixon and D. Bhate, University of Toledo, Toledo, OH; M. Nallasamy, QSS Group Inc, Cleveland, OH; S. Sawyer, University of Akron, Akron, OH
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0930
AIAA-2006-2414
Aeroacoustic Computations Using a High Order Shock Capturing Scheme
V. Daru and X. Gloerfelt, Ecole Nationale Supérieure d'Arts et Métiers, Paris, France
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1000
AIAA-2006-2415
A New High- Resolution Balance- Characteristic Method for Aeroacoustics
S. Karabasov, University of Cambridge, Cambridge, Great Britain; V. Goloviznin, Moscow Institute of Nuclear Safety, Moscow, Russia; T. Kozubskaya and I. Abalakin, Institute for Mathematical Modelling, Moscow, Russia
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1030
AIAA-2006-2416
Non- Reflecting Boundary Conditions for
One- Step LBM Simulation of Aeroacoustics
E. Kam, R. So, and R. Leung, Hong Kong Polytechnic University, Hung Hom, Hong Kong
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1100
AIAA-2006-2417
CAA Using 3D CESE Method with a Simplified Courant Number Insensitive Scheme
J. Yen, E. Duell and W. Martindale, Jacobs Sverdrup, Tullahoma, TN
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1130
AIAA-2006-2418
Aeroacoustic Simulations for Complex Geometries Based on Hybrid Meshes
J. Utzmann, F. Lörcher, M. Dumbser, and C. Munz, University of Stuttgart, Stuttgart, Germany
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1200
AIAA-2006-2419
The Influence of Flow Domain Modeling on the Accuracy of Direct and Hybrid Aeroacoustic Noise Calculations
W. De Roeck, G. Rubio, M. Baelmans, P. Sas, and W. Desmet, Katholieke Universiteit Leuven, Leuven, Belgium
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| Session
4-
AA-4
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CAA: Fan/Airfoil
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Paul Revere A |
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Chaired by: V. GOLUBEV, Embry-Riddle Aeronautical University, Daytona Beach, FL
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0900
AIAA-2006-2420
The Prediction of Fan Exhaust Noise Propagation
Y. Zhao and P. Morris, Pennsylvania State University, University Park, PA
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0930
AIAA-2006-2421
Numerical Prediction of Propagation and Radiation of Aft Fan and Core Nozzle Noise
R. Arina, Politecnico di Torino, Torino, Italy
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1000
AIAA-2006-2423
A 3D Parabolic Equation Method for Wind Turbine
Noise Propagation in Moving Inhomogeneous
Atmosphere
R. Cheng, P. Morris, and K. Brentner, Pennsylvania State University, State College, PA
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1030
AIAA-2006-2424
Leading Edge Noise
S. Glegg, Florida Atlantic University, Boca Raton, FL; J. Staubs and W. Devenport, Virginia Polytechnic Institute and State University, Blacksburg, VA
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1100
AIAA-2006-2426
A Parametric Study of Nonlinear Gust- Airfoil Interaction
V. Golubev and R. Mankbadi, Embry-Riddle Aeronautical University, Daytona Beach, FL; M. Visbal, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH; J. Scott, NASA Glenn Research Center, Cleveland, OH; and R. Hixon, University of Toledo, Toledo, OH
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| Session
5-
AA-5
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Cavity Aeroacoustics
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William Dawes A |
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Chaired by: L. UKEILEY, University of Mississippi, Oxford, MS
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0900
AIAA-2006-2427
Analysis of Control Concepts for Cavity Flows
S. Arunajatesan, C. Kannepalli, and N. Sinha, Combustion Research and Flow Technology, Inc., Pipersville, PA
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0930
AIAA-2006-2428
Flow Field Dynamics in Open Cavity Flows
N. Murray and L. Ukeiley, University of Mississippi, University, MS
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1000
AIAA-2006-2429
An Investigation into Supersonic Swept Cavity Flows
S. Gai, E. Samanes, and J. Milthorpe, University of New South Wales, Canberra, Australia
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1030
AIAA-2006-2430
Coupling of a Jet- Slot Oscillator With the Flow- Supply Duct: Flow- Acoustic Interaction Modeling
M. Glesser and A. Billon, University of La Rochelle, La Rochelle, France; V. Valeau, University of Poitiers, Poitiers, France; and A. Sakout, University of La Rochelle, La Rochelle, France
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1100
AIAA-2006-2431
Two and Three Dimensional Simulations of Supersonic Cavity Flow
H. Kim, SUPAERO, Toulouse, France; S. Aradag and D. Knight, Rutgers University, Piscataway, NJ
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1130
AIAA-2006-2432
Compressible POD/Galerkin Reduced- Order Model of Self- Sustained Oscillations in a Cavity
X. Gloerfelt, Ecole Nationale Supérieure d'Arts et Métiers, Paris, France
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1200
AIAA-2006-2433
Aeroacoustic Computations of High- Reynolds Number Cavity Flows on Staggered Grids
X. Gloerfelt, Ecole Nationale Supérieure d'Arts et Métiers, Paris, France
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| Session
6-
AA-6
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Flight Acoustics Research: Quiet Technology Demonstrator
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President's Ballroom A-C |
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Chaired by: B. SHIVASHANKARA, The Boeing Company, Seattle, WA
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0900
AIAA-2006-2720
The Quiet Technology Demonstrator Program: Flight Validation of Airplane Noise- Reduction Concepts
W. Herkes, R. Olsen and S. Uellenberg, The Boeing Company, Seattle, WA
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0930
AIAA-2006-2467
Reducing Propulsion Airframe Aeroacoustic Interactions with Uniquely Tailored Chevrons: 1. Isolated Nozzles
V. Mengle, R. Elkoby and L. Brusniak, The Boeing Company, Seattle, WA; R. Thomas, NASA Langley Research Center, Hampton, VA
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1000
AIAA-2006-2434
Reducing Propulsion Airframe Aeroacoustic Interactions with Uniquely Tailored Chevrons: 2. Installed Nozzles
V. Mengle, R. Elkoby and L. Brusniak, The Boeing Company, Seattle, WA; R. Thomas, NASA Langley Research Center, Hampton, VA
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1030
AIAA-2006-2436
Computational Analysis of a Chevron Nozzle Uniquely Tailored for Propulsion Airframe Aeroacoustics
S. Massey, Eagle Aeronautics Inc, Hampton, VA; A. Elmiligui, Analytical Services and Materials Inc., Hampton, VA; C. Hunter, R. Thomas and P. Pao, NASA Langley Research Center, Hampton, VA; V. Mengle, The Boeing Company, Seattle, WA
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1100
AIAA-2006-2439
Flight Test Results for Uniquely Tailored Propulsion Airframe Aeroacoustic Chevrons: Shockcell Noise
V. Mengle, U. Ganz, E. Nesbitt and E. Bultemeier, The Boeing Company, Seattle, WA; R. Thomas, NASA Langley Research Center, Hampton, VA
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1130
AIAA-2006-2438
Flight Test Results for Uniquely Tailored Propulsion- Airframe Aeroacoustic Chevrons: Community Noise
E. Nesbitt, V. Mengle, and M. Czech, The Boeing Company, Seattle, WA; B. Callender, GE Transportation, Cincinnati, OH; and R. Thomas, NASA Langley Research Center, Hampton, VA
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1200
AIAA-2006-2440
Effect of Uniform Chevrons on Cruise Shockcell Noise
E. Bultemeier, U. Ganz, J. Premo, and E. Nesbitt, The Boeing Company, Seattle, WA
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| Session
7-
AA-7
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Jet Noise Modeling I: LES
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Molly Pitcher |
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Chaired by: C. BOGEY, Ecole Centrale de Lyon, Ecully, France
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0900
AIAA-2006-2441
A Comparative Use of the PSE and LES Approaches for Jet Noise Predictions
E. Piot, G. Casalis and F. Muller, ONERA, Toulouse, France
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0930
AIAA-2006-2442
An Approach to Improve High Frequency Noise Prediction in LES of Jets
X. Wu, G. Page, and J. McGuirk, Loughborough University, Loughborough, Great Britain
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1000
AIAA-2006-2443
Computation of the Noise Radiated by Jets with Laminar/Turbulent Nozzle- Exit Conditions
S. Barre, C. Bogey and C. Bailly, Ecole Centrale de Lyon, Ecully, France
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1030
AIAA-2006-2444
Phased- Array Imaging of Jet Noise Sources in a Large- Eddy Simulation
L. Brusniak, The Boeing Company, Seattle, WA; M. Shur, St. Petersburg Polytechnic University, St. Petersburg, Russia; P. Spalart, The Boeing Company, Seattle, WA
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1100
AIAA-2006-2445
Computation of the Flow and Noise of Round and Beveled Nozzles
K. Viswanathan, The Boeing Company, Seattle, WA; M. Shur, St. Petersburg Polytechnic University, St. Petersburg, Russia; P. Spalart, The Boeing Company, Seattle, WA; and M. Strelets, St. Petersburg Polytechnic University, St. Petersburg, Russia
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1130
AIAA-2006-2447
Direct Computation of the Sound Generated by Isothermal and Non- Isothermal Mixing Layers
C. Moser, E. Lamballais and Y. Gervais, Université de Poitiers, Poitiers, Vienne, France
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| Session
8-
AA-8
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Sonic Boom & Pulse Detonation Engine
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William Dawes B |
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Chaired by: A. PILON, Lockheed Martin Aeronautics Company, Palmdale, CA
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0900
AIAA-2006-2449
Accurate Prediction of Sonic Boom Signals
A. Pilon, Lockheed Martin Aeronautics Company, Palmdale, CA
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0930
AIAA-2006-2450
Effect of Pressure Distortion and Sampling Rate on Shaped Sonic Boom Predictions
K. Laflin, Cessna Aircraft Company, Wichita, KS
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1000
AIAA-2006-2451
Ray Tracing for Long Range Atmospheric Propagation of Infrasound
O. Gainville and P. Piserchia, Commissariat à l'Energie Atomique, Bruyères le Châtel, France; P. Blanc-Benon, Centre National de la Recherche Scientifique, Ecully, France; and J. Scott, Ecole centrale Lyon, Ecully, France
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1030
AIAA-2006-2452
Sonic Boom Prediction: A New Empirical Formulation and Animated Graphical Model
A. Clare, Massachusetts Institute of Technology, Cambridge, MA; R. Oman, Oman Moments Inc., Huntington, NY
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1100
AIAA-2006-2453
Acoustic Characterization of a Pulse Detonation Engine
A. Glaser, N. Caldwell and E. Gutmark, University of Cincinnati, Cincinnati, OH
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| Session
9-
AA-9
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Acoustic Liner Implementation Issues
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Molly Pitcher |
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Chaired by: J. YU, Goodrich Corporation, Chula Vista, CA
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1400
AIAA-2006-2455
Zero Splice Technology and Acoustic Benefits
F. Gantie and H. Batard, Airbus France, Toulouse, France; N. Baker and P. Schwaller, Rolls-Royce, Derby, Great Britain
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1430
AIAA-2006-2456
Far- field directivity of rotor- alone tones radiated from fan
intakes with spliced liners for different intake shapes, with flow
B. Tester and L. De Mercato, University of Southampton, Southampton, Great Britain
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1500
AIAA-2006-2458
Quiet Technology Demonstrator 2 Intake Liner Design and Validation
J. Yu, Goodrich Aerostructures Group, San Diego, CA; E. Nesbitt, Boeing Commercial Airplanes, Seattle, WA; H. Kwan, Goodrich Aerostructures Group, San Diego, CA; S. Uellenberg, Boeing Commercial Airplanes, Seattle, WA; E. Chien, Goodrich Aerostructures Group, San Diego, CA; J. Premo, Boeing Commercial Airplanes, Seattle, WA
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1530
AIAA-2006-2459
Scattering of Acoustic Duct Modes by Axial Liner Splices
C. Tam and H. Ju, Florida State University, Tallahassee, FL; and E. Chien, Goodrich, San Diego, CA
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1600
AIAA-2006-2460
Nonlinear Modeling of Shock Wave Trains in Ducts with Wall Discontinuities
J. Alonso and R. Burdisso, Virginia Polytechnic Institute and State University, Blacksburg, VA; and J. Anderson, Techsburg Inc., Blacksburg, VA
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1630
AIAA-2006-2461
Application of a Piston Radiation Model to Liner Nonuniformities and Rigid Splices
J. Alonso and R. Burdisso, Virginia Polytechnic Institute and State University, Blacksburg, VA
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| Session
10-
AA-10
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Aircraft Configuration Effects: Experiment
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President's Ballroom A-C |
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Chaired by: R. ELKOBY, The Boeing Company, Seattle, WA
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1400
AIAA-2006-2462
Static and Flight Aeroacoustic Evaluations of a Scarf Inlet
D. Weir, B. Bouldin and J. Mendoza, Honeywell Aerospace, Phoenix, AZ
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1430
AIAA-2006-2463
Aeroengine Noise Investigated from Flight Tests
S. Guerin and U. Michel, DLR, German Aerospace Research Center, Berlin, Germany
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1500
AIAA-2006-2464
Reduction of Approach Noise of the MD- 11
H. Siller, DLR, German Aerospace Research Center, Berlin, Germany; C. Zwiener, Deutsche Flugsicherung, Langen, Germany; U. Michel, DLR, German Aerospace Research Center, Berlin, Germany; and G. Saueressig, Deutsche Lufthansa, Frankfurt, Germany
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1530
AIAA-2006-2465
Measurement of Approach Noise Footprints of a C- 17 STOL Aircraft During Conventional and Noise- Mitigating Approach Trajectories
W. Horne and C. Kitaplioglu, NASA Ames Research Center, Moffett Field, CA; N. Burnside, AerospaceComputing, Inc, Moffett Field, CA; D. Schein, Northrop Grumman Corporation, El Segundo, CA; A. Liddle and A. Welborn, California State University, San Luis Obispo, CA
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1600
AIAA-2006-2468
Computational Analysis of the Effect of Porosity on Shock Cell Strength at Cruise
S. Massey, Eagle Aeronautics, Inc., Hampton, VA; A. Elmiligui, Analytical Services and Materials, Inc., Hampton, VA; R. Thomas, P. Pao, K. Abdol-Hamid, and C. Hunter, NASA Langley Research Center, Hampton, VA
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1630
AIAA-2006-2435
Reducing Propulsion Airframe Aeroacoustic Interactions with Uniquely Tailored Chevrons: 3. Jet- Flap Interaction
V. Mengle, L. Brusniak and R. Elkoby, The Boeing Company, Seattle, WA; R. Thomas, NASA Langley Research Center, Hampton, VA
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| Session
11-
AA-11
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CAA Methods II
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Paul Revere A |
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Chaired by: D. LOCKARD, NASA Langley Research Center, Hampton, VA
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1400
AIAA-2006-2469
Optimized Boundary Compact Finite Difference Schemes for Computational Aeroacoustics
J. Kim, University of Southampton, Southampton, Great Britain
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1430
AIAA-2006-2471
Analysis of Aeroacoustic Wave Propagation Simulations Using a Higher- Order Accurate Method
G. Efraimsson and C. Biela, Royal Institute of Technology, Stockholm, Sweden
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1500
AIAA-2006-2472
Application of Dual- Time Stepping and Finite- Volume Scheme in Computational Aeroacoustics
W. Lin, Pratt & Whitney Rocketdyne, Canoga Park, CA; and P. Rocketdyne, , Canoga Park, CA
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1530
AIAA-2006-2473
Improving an Unstructured CFD Solver for Aeroacoustics Applications
P. Geuzaine, S. Bogaerts, L. Georges, and K. Hillewaert, CENAERO, Gosselies, Belgium; and S. Caro, Free Field Technologies, Mont-Saint-Guibert, Belgium
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1600
AIAA-2006-2474
Noise Scattering by the Blended Wing Body Airplane: Measurements and Prediction
C. Reimann, North Carolina State University, Raleigh, NC; A. Tinetti, NCI Information Systems Inc., Hampton, VA; M. Dunn, National Institute of Aerospace, Hampton, VA
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1630
AIAA-2006-2475
Prediction of Sound Scattered by Moving Bodies with Applications to Propeller- Driven Airplanes
M. Gennaretti and U. Iemma, University Roma Tre, Rome, Italy; and C. Testa, Centro Italiano Ricerche Aerospaziali, Capua, Italy
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| Session
12-
AA-12
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Fan Noise Measurement & Modeling
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Cambridge |
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Chaired by: E. ENVIA, NASA Glenn Research Center, Cleveland, OH
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1400
AIAA-2006-2476
Experimental Investigation Into Trailing Edge Noise Sources
A. Garcia-Sagrado, T. Hynes and H. Hodson, Whittle Laboratory, Cambridge, Great Britain
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1430
AIAA-2006-2477
Incident Turbulence Interaction Noise from an Axial Fan
D. Fedala, S. Kouidri and R. Rey, Ecole Nationale Supérieure d'Arts et Métiers, Paris, France; T. Carolus and M. Schneider, University of Siegen, Siegen, Germany
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1500
AIAA-2006-2479
Noise Validation of Model Fan Rig with Engine
P. Schwaller, N. Baker, and D. Tomlinson, Rolls-Royce, Derby, Great Britain; P. Sijtsma, National Aerospace Laboratory/NLR, Emmeloord, The Netherlands; and R. Hemmings, INBIS Ltd., Bristol, Great Britain
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1530
AIAA-2006-2480
Space- Time Correlations and Trailing Edge Flow Structure in Fan- Blade Wakes with Trailing Edge Blowing
A. Borgoltz, W. Devenport, and E. Craig, Virginia Polytechnic Institute and State University, Blacksburg, VA
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| Session
13-
AA-13
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General Acoustics I
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Paul Revere B |
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Chaired by: F. FARASSAT, NASA, Hampton, VA
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1400
AIAA-2006-2483
Leapfrogging of Two Vortex- Rings as Test Case for Volume Source Computations
M. Jacob and A. BenYahia, Ecole Centrale de Lyon, Ecully, France; D. Casalino, Centro Italiano Ricerche Aerospaziali, Capua, Italy; D. Eschricht and F. Thiele, Technical University of Berlin, Belin, Germany
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1430
AIAA-2006-2484
A Look Inside the Lighthill Source Term
M. Cabana, V. Fortuné, and P. Jordan, Centre National de la Recherche Scientifique, Poitiers, France
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1500
AIAA-2006-2485
From Primitive- Variable Boundary- Integral Formulation to FWH Equation
L. Morino, University Roma Tre, Rome, Italy
|
1530
AIAA-2006-2486
Propagation and Stability of Vorticity- Entropy Waves
in a Nonuniform Flow
O. Atassi, Pratt and Whitney Aircraft, United Technologies Corporation, East Hartford, CT
|
1600
AIAA-2006-2488
Evaluation of Far- Field Sound with Open Surface Corrections to Lighthill's Equation
L. Cheung and S. Lele, Stanford University, Stanford, CA
|
1630
AIAA-2006-2489
Direct Simulation of Acoustic Waves Emitted from Moving Bodies by the Finite Difference Lattice Boltzmann Method
A. Tamura and M. Tsutahara, Kobe University, Kobe, Japan
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| Session
14-
AA-14
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Interior Noise
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William Dawes A |
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Chaired by: S. CARO, Free Field Technologies, Louvain la Neuve, Belgium
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1400
AIAA-2006-2490
TBL Noise Generated by a Simplified Side Mirror Configuration and Acoustic Transfer Through the Window: Modelling Using Actran and Fluent
S. Caro and A. Ramonda, Free Field Technologies, Mont-St-Guibert, Belgium; F. Pérot, S. Vergne, and M. Pechabat, PSA Peugeot Citroën, Velizy, France
|
1430
AIAA-2006-2491
Interior Noise Sources Identifications, In- Flight Measurements and Numerical Correlations of an Advanced Business Aircraft
F. Marulo, University of Naples, Naples, Italy; A. Sollo and M. Aversano, Piaggio Aero Industries, Pozzuoli, Italy; G. Russo and T. Polito, University of Naples, Naples, Italy
|
1500
AIAA-2006-2493
Simulation of Aeroacoustic Sources in Aircraft Climate Control System
F. Mathey and O. Morin, Fluent France, Montigny le Bretonneux, France; B. Caruelle and K. Debatim, Airbus France, Toulouse, France
|
1530
AIAA-2006-2494
Experimental and Numerical Investigation of a Flow- Induced Cavity Resonance with Application to Automobile Buffeting
B. Crouse, Exa Corporation, Brisbane, CA; S. Senthooran, Exa Corporation, Livonia, MI; D. Freed and G. Balasubramanian, Exa Corporation, Brisbane, CA; M. Gleason and M. Puskarz, DaimlerChrysler Corporation, Auburn Hills, MI; P. Lew and L. Mongeau, Purdue University, West Lafayette, IN
|
1600
AIAA-2006-2492
Hermite High–Order Finite Elements
for Aeroacoustic Analysis
L. Morino and F. Cetta, University Roma Tre, Rome, Italy
|
1630
AIAA-2006-2437
Novel Inflight Noise Analysis System
E. Bultemeier and F. Hutto, The Boeing Company, Seattle, WA
|
| Session
15-
AA-15
|
Jet Noise Modeling II: LES/DNS
|
Crispus Attucks |
|
Chaired by: A. LYRINTZIS, Purdue University, West Lafayette, IN
|
|
1400
AIAA-2006-2495
Investigating Broadband Shock- Associated Noise of Axisymmetric Jets Using Large- Eddy Simulation
D. Bodony, J. Ryu, P. Ray and S. Lele, Stanford University, Stanford, CA
|
1430
AIAA-2006-2496
Large Eddy Simulation of Screech Tone Generation in a Planar Underexpanded Jet
J. Berland, École Centrale de Lyon, Ecully, France; C. Bogey and C. Bailly, École Centrale de Lyon, Lyon, France
|
1500
AIAA-2006-2497
Large- Eddy Simulation of Hot Coaxial Jets
I. Tristanto, G. Page, and J. McGuirk, Loughborough University, Loughborough, Great Britain
|
1530
AIAA-2006-2499
High Frequency Noise Generation in the Near- Nozzle Region of a Jet
A. Uzun and M. Hussaini, Florida State University, Tallahassee, FL
|
1600
AIAA-2006-2500
Investigation of the noise from cold and heated subsonic jets
P. Moore and B. Boersma, Delft University of Technology, Delft, The Netherlands
|
1630
AIAA-2006-2501
Adjoint- Based Control of the Noise from a Turbulent Mixing Layer
R. Kleinman and J. Freund, University of Illinois at Urbana-Champaign, Urbana, IL
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