Towards an airframe noise prediction methodology: Survey of current approaches

Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting

Volumn 4, Issue , 2006, Pages 2496-2507

  Farassat, F ^a   Casper, Jay H ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC NOISE; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; DATABASE SYSTEMS; NUMERICAL METHODS;

ACOUSTIC ANALOGY; NOISE PREDICTION; TURBULENCE SIMULATION;

AIRFRAMES;

EID: 34250880212     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-210     Document Type: Conference Paper

References (63)

1. M.G. Macaraeg: Fundamental investigations of airframe noise, AIAA-98-2224, 1998, AIAA/CEAS Aeroacoustics Conference, 4th (19th AIAA Aeroacoustics Conference), Toulouse, France, June 2-4, 1998
2. C.L. Streett, D.P. Lockard, B.A. Singer, M.R. Khorrami, and M.M. Choudhari: In search of physics: The interplay of experiment and computation in airframe noise research; flap-edge noise, AIAA 2003-0979, 41st Aerospace Sciences Meeting & Exhibit, January 6-9, 2002, Reno, Nevada
3. Mehdi R. Khorrami, Meelan Choudhari, Bart A. Singer, David P. Lockard, and Craig L. Streett: In search of the physics: The interplay of experiment and computation in slat aeroacoustics, AIAA 2003-0980, 41st Aerospace Sciences Meeting & Exhibit, January 6-9, 2002, Reno, Nevada
4. T. F. Brooks, and William M. Humphreys, Jr., Flap edge aeroacoustic measurements and predictions, AIAA Paper No. 2000-1975, 6th AIAA/CEAS Aeroacoustics Conference June 12-14, 2000 Lahaina, Hawaii
5. Mehdi R. Khorrami and Meelan M. Choudhari: Application of passive porous treatment to slat trailing edge noise, NASA/-TM-2003-212416, 2003
6. David G. Crighton: Airframe Noise, in Aeroacoustics of Flight Vehicles, Volume 1, Harvey H. Hubbard (Editor), Acoustical Society of America, 1995
7. David P. Lockard and Geoffrey M. Lilley: The airframe noise reduction challenge, NASA TM-2004-213013, 2004
8. Bart A. Singer and Yueping Guo: Development of computational aeroacoustics tools for airframe noise calculations, International Journal of Computational Fluid Dynamics, 18 (6), 2004, 455-469
9. Meng Wang, Jonathan B, Freund and Sanjiva K. Lele: Computational Prediction of Flow-Generated Sound, Annual Reviews of Fluid Mechanics, 38, 2006, 483-512
10. B. A. Singer, D. P. Lockard and G. M. Lilley: Hybrid acoustic prediction, International Journal of Computers & Mathematics with Applications, 46, 2003, 647-669
11. Kenneth S. Brentner and F. Farassat: Modeling aerodynamically generated sound of helicopter rotors, Progress in Aerospace Sciences, 39, 2003, 83-120
12. W. E. Zorumski, Aircraft Noise Prediction Program Theoretical Manual, Parts 1 and 2, NASA Technical Memorandum-83199-PT-l andPT-2, National Aeronautics and Space Administration, Langley Research Center, Hampton, VA, 1982
13. J. E. Ffowcs Williams and L. H. Hall. Aerodynamic sound generation by turbulent flow in the vicinity of a scattering half plane, Journal of Fluid Mechanics, 40, 1970, 657-670
14. D. G. Crighton, Radiation from vortex filament motion near a half-plane, Journal of Fluid Mechanics, 51, 1972, 357-362
15. M. S. Howe: A review of theory of trailing edge noise, Journal of Sound and Vibration, 61, 1978, 437-465
16. M. S. Howe: Trailing edge noise at low Mach numbers, Journal of Sound and Vibration, 225, 1999, 211-238
17. M. S. Howe: Trailing edge noise at low Mach numbers, Part 2: Attached and separated edge flows, Journal of Sound and Vibration, 234, 2000, 761-775
18. R. K. Amiet: Acoustic radiation from an airfoil in a turbulent stream, Journal of Sound and Vibration, 41(4), 1975, 407-420
19. R. K. Amiet: Noise due to turbulent flow past a trailing edge, Journal of Sound and Vibration, 47(3), 1976, 387-393
20. R. K. Amiet: A Note on edge noise theories, Journal of Sound and Vibration, 78(4), 1981, 485-488
21. Robert W. Paterson and Roy K. Amiet: Acoustic radiation and surface pressure characteristics of an airfoil due to incident turbulence, NASA Contractor Report CR-2733, 1976
22. Robert H. Schlinker and R. K. Amiet: Helicopter rotor trailing edge noise, NASA Contractor report CR-3470, 1981
23. M. S. Howe: Theory of Vortex Sound, Cambridge University Press, 2003
24. M. S. Howe: Edge-source acoustic Green's function for an airfoil of arbitrary chord, with application to trailing-edge noise, Quarterly Journal of Mechanics and Applied Mathematics, 54, 2001, 139-155
25. F. Farassat and J. W. Posey: The Role of Analytical Methods in Computational Aeroacoustics, Aerospace National Simulation Symposium, Tokyo, Japan, June 12-13, 2003, paper available at: http://techreports.larc.nasa.gov/ ltrs/-PDF/2003/mtg/NASA-2003-anss-ff.pdf, slides available at: http://techreports.larc.nasa.gov/ltrs/PDF/2003/mtg/NASA-2003-anss-ffslides.pdf
26. J. E. Ffowcs Williams and D. L. Hawkings: Sound generated by turbulence and surfaces in arbitrary motion, Philosophical Transactions of the Royal Society, A264, 1969, 321-342
27. Kenneth S. Brentner and F. Farassat: An analytical comparison of the acoustic analogy and Kirchhoff formulation for moving surfaces, AIM Journal, 36(8), 1998, 1379-138628.
28. F. Farassat, Introduction to Generalized Functions With Applications in Aerodynamics and Aeroacoustics, May 1994 (Corrected April 1996), NASA Technical Paper 3428
29. F. Farassat, G, P. Succi, A review of propeller discrete frequency noise prediction technology with emphasis on two current methods for time domain calculations, 1980, Journal of Sound and Vibration, 71(3), 399-419
30. Kenneth K. Brentner, Prediction of Helicopter Discrete Frequency Rotor Noise- A Computer Program Incorporating Realistic Blade Motions and Advanced Formulation, October 1986, NASA TM 87721
31. P. di Francescantonio: A new boundary integral formulation for the prediction of sound radiation, Journal of Sound and Vibration, 202(4), 1997, 491-509.
32. I, E. Garrick, and Charles E. Watkins: A Theoretical Study of the Effect of Forward Speed on the Free-Space Sound-Pressure Field Around Propellers, NACA Report 1198, 1954
33. David P. Lockard: A. Comparison of Ffowcs Williams-Hawkings solvers for airframe noise applications, AIAA-2002-2580, 8th AIAA/CEAS Aeroacoustics Conference & Exhibit, Breckenridge, Colorado, June 17-19, 2002
34. F. Farassat: Linear acoustic formulas for calculation of rotating blade noise, AIAA Journal, 19(9), 1981, 1122-1130
35. F. Farassat and M. K. Myers: Extension of Kirchhoff's formula to radiation from moving sources, Journal of Sound and Vibration, 123 (3), 1988, 451-460
36. F. Farassat: The Kirchhoff Formulas for Moving Surfaces in Aeroacoustics - The Subsonic and Supersonic Cases, NASA Technical Memorandum 110285, September 1996
37. J. Casper and F. Farassat: A new time domain formulation for broadband noise prediction, International Journal of Aeroacoustics, 1(3), 2002, 207-240
38. Mehdi R. Khorrami, Bart A. Singer and Mert E. Berkman: Time-accurate simulations and acoustic analysis of slat free-shear layer, AIAA-2001-2155, 7th AIAA/CEAS Aeroacoustics Conference and Exhibit, Maastricht, Netherlands, May 28-30, 2001
39. Bart A. Singer, Kenneth S. Brentner, David P. Lockard, and Geoffrey M. Lilley: Simulation of acoustic scattering from a trailing edge, Journal of Sound and Vibration, 230(3), 2000, 541-560
40. Bart A. Singer and David P. Lockard: Shear effects in aeroacoustic predictions, Journal of Sound and Vibration, 267 (4), 2003, 961-966
41. Jay H. Casper, David P. Lockard, Mehdi Khorrami and Craig Streett: Investigation of volumetric sources in airframe noise simulations, AIAA-2004-2805, 10th AIAA/CEAS Aeroacoustics Conference , Manchester, United Kingdom, May 10-12, 2004
42. Kefan Tang: Numerical Simulation of Flow-Induced Noise by Means of the Hybrid Method with LES and Aeroacoustic Analogy, Dissertation zur Erlangung des akademischen Grades Doktor-Ingenieur, University of Siegen, Germany
43. D. Casalino: An advanced time approach for acoustic analogy predictions, Journal of Sound and Vibration, 261, 2003, 583-612
44. Yueping Guo: Airframe noise prediction by acoustic analogy: NASA Contract Informal Report, February 2004
45. Martin R. Fink: Propulsive lift noise, in Aeroacoustics of Flight Vehicles, Volume 1, Harvey H. Hubbard (Editor), Acoustical Society of America, 1995
46. Martin R. Fink: Airframe noise prediction, FAA-RD-77-29, 1977
47. T. F. Brooks and C. L, Burley: Rotor broadband noise prediction with comparison to model data, AIAA Paper 2001-2210, AIAA/CEAS Aeroacoustics Conference and Exhibit, Maastricht, Netherlands, May 28-30, 2001
48. C. L. Burley and T. F. Brooks, M. A. Marcolini, A. G. Brand and D. A. Conner: Tiltrotor aeroacoustic code (TRAC) predictions and comparisons with measurements, Journal of American Helicopter Society, 45(2), 2000, 80-89
49. Y. P. Guo, K. J. Yamamoto and R.W. Stoker: Component-based empirical model for high-lift system noise prediction, Journal of Aircraft, 40, 2003, 914-922
50. C. Bailly, C. Bogey, and D. Juvé: Computation of the flow noise using source terms in linearized Euler's equations. 2000. AIAA Paper 2000-2047.
51. C. K. W. Tam and Z. Dong: A study of the short wave components in computational acoustics, Journal of Computational Acoustics, 1(1), 1993, 1-30
52. Christopher K.W. Tam , Jay C. Webb: Dispersion-relation-preserving finite difference schemes for computational acoustics, Journal of Computational Physics, v.107 n.2, p. 262-281, Aug. 1993
53. F. Q. Hu, Y. H. Hussaini, and J. L. Manthey: Low-dissipation and low-dispersion Runge-Kutta schemes for computational acoustics, Journal of Computational Physics, 124, 1996, 177-191
54. 54-Christophe Bogey and Christophe Bailly: A family of low dispersive and low dissipative explicit schemes for flow and noise computations, Journal of Computational Physics, 194(1), 2004, 194 - 214
55. C. K. W. Tam and Z. Dong: Wall boundary condition for high-order finite-difference schemes in computational aeroacoustics. Theoretical and Computational Fluid Dynamics, 6(6), 1994, 303-322
56. D. Stanescu, J. Xu, M.Y. Hussaini and F. Farassat: Computation of engine noise propagation and scattering off an aircraft, International Journal of Aeroacoustics, 1(4), 2002, 403-420
57. D. Stanescu, M. Y. Hussaini and F. Farassat: Aircraft engine noise scattering from fuselage and wings- a computational approach, Journal of Soundand Vibration, 261(2), 2003, 319-333
58. Mark H. Dunn and Ana F. Tinetti: Aeroacoustic Scattering Via The Equivalent Source Method, AIAA-2004-2937, 10th AIAA/CEAS Aeroacoustics Conference , Manchester, United Kingdom, May 10-12, 2004
59. Ana F. Tinetti and Mark H. Dunn: Aeroacoustic Noise Prediction Using the Fast Scattering Code, AIAA 2005-3061, 11th Aeroacoustics Conference, Monterey, California, May 23-25, 2005
60. D. G. Crighton, A. P. Dowling, J. E. Ffowcs Williams, M. Heckl and F. G. Leppington: Modern Methods in Analytical Acoustics- Lecture Notes, Springer-Verlag, 1992
61. F. Q. Hu, Y. P. Guo and A. D. Jones: On the computation and application of exact Green's function in acoustic analogy, AIAA 2005-2986, 11th Aeroacoustics Conference, Monterey, California, May 23-25, 2005
62. N. Curie: The influence of solid boundaries upon aerodynamic sound, Proceedings of the Royal Society of London, A231, 1955, 505-514
63. A. Powell: Aerodynamic noise and the plane boundary, Journal of the Acoustical Society of America, 32, 1960, 962-990