Direct noise computation of the turbulent flow around a zero-incidence airfoil

AIAA Journal

Volumn 46, Issue 4, 2008, Pages 874-883

  Marsden, Olivier ^a,b   Bogey, Christophe ^a,b   Bailly, Christophe ^a,b  

^a ECOLE CENTRALE DE LYON   (France)

^b CNRS   (France)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; BOUNDARY LAYERS; COMPUTER SIMULATION; LARGE EDDY SIMULATION; MACH NUMBER; REYNOLDS NUMBER; TURBULENT FLOW;

ACOUSTIC ANALOGY; ACOUSTIC SPECTRA; CURVILINEAR GRIDS; RADIATED ACOUSTIC FIELDS; TRAILING EDGE;

ACOUSTIC NOISE;

EID: 44649117394     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.29825     Document Type: Article

References (51)

1. Tam, C. K. W., and Webb, J. C., "Dispersion-Relation-Preserving Finite Difference Schemes for Computational Acoustics," Journal of Computational Physics, Vol. 1.07, No. 2, 1993, pp. 262-281. doi:10.1006/jcph.1993.1143
2. Bogey, C., and Bailly, C., "A Family of Low Dispersive and Low Dissipative Explicit Schemes for Noise Computations," Journal of Computational Physics, Vol. 194, No. 1, 2004, pp. 194-214. doi:10.1016/j.jcp.2003.09.003
3. Lele, S. K., "Compact Finite Difference Schemes with Spectral-Like Resolution," Journal of Computational Physics, Vol. 103, Nov. 1992, pp. 16-42. doi: 10.1016/0021 -9991(92)90324-R
4. Visbal, M., and Gaitonde, D., "High-Order-Accurate Methods for Complex Unsteady Subsonic Flows," AIAA Journal, Vol. 37, No. 10, 1999, pp. 1231-1239.
5. Bogey, C., Bailly, C., and Juvé, D., "Noise Investigation of a High Subsonic, Moderate Reynolds Number Jet Using a Compressible LES," Theoretical and Computational Fluid Dynamics, Vol. 16, No. 4, 2003, pp. 273-297. doi:10.1007/s00162-002-11079-4
6. Bogey, C., and Bailly, C., "Investigation of Downstream, and Sideline Subsonic Jet Noise Using Large Eddy Simulations," Theoretical and Computational Fluid Dynamics, Vol. 20, No. 1, 2006, pp. 23-40. doi:10.1007/s00162-005-0005-7
7. Bodony, D. J., and Lele, S. K., "On Using Large-Eddy Simulation for the Prediction of Noise from Cold and Heated Turbulent Jets," Physics of Fluids, Vol. 17, No. 085103-1, 2005. doi:10.1063/12001689
8. Uzun, A., Lyrintzis, A. S., and Blaisdell, G. A., "Coupling of Integral Acoustics Methods with LES for Jet Noise Prediction," International Journal of Aeroacoustics, Vol. 3, No. 4, Oct. 2004, pp. 297-346. doi:10.1260/1475472043499290
9. Visbal, M., and Gaitonde, D., "Very High-Order Spatially Implicit Schemes for Computational Acoustics on Curvilinear Meshes," Journal of Computational Acoustics, Vol. 9, No. 4, 2000, pp. 1259-1286. doi:10.1142/S0218396X01000541
10. Manoha, E., Herrero, C., Sagaut, P., and Redonnet, S., "Numerical Prediction of Airfoil Aerodynamic Noise," AIAA Paper 2002-2573, 2002.
11. Visbal, M., and Gaitonde, D., "On the Use of Higher-Order Finite Difference Schemes on Curvilinear and Deforming Meshes," Journal of Computational Physics, Vol. 181, Sept. 2002, pp. 155-185. doi:10.1006.jcph.2002.7117
12. Marsden, O., Bogey, C., and Bailly, C., "High-Order Curvilinear Simulations of Flows Around Noncartesian Bodies," Journal of Computational Acoustics, Vol. 13, No. 4, 2005. doi:10.1142/S0218396X05002906
13. Wang, M., and Moin, P., "Computation of Trailing-Edge Flow and Noise Using Large-Eddy Simulation," AIAA Journal, Vol. 38, No. 12, 2000, pp. 2201-2209.
14. Oberai, A., Roknaldin, F., and Hughes, Th., "Computation of Trailing-Edge Noise Due to Turbulent Flow over an Airfoil," AIAA Journal, Vol. 40, No. 11, 2002, pp. 2206-2216.
15. Kim, H.-J., Lee, S., and Fujisawan, N.,"Computation of Unsteady Flow and Aerodynamic Noise of NACA0018 Airfoil Using Large-Eddy Simulation," International Journal of Heat and Fluid Flow, Vol. 27, No. 2, 2006, pp. 229-242. doi:10.1016/j.ijheatfluidflow.2005.08.007
16. Nagarajan, S., Hahn, S., and Lele, S., "Prediction of Sound Generated by a Pitching Airfoil: A Comparison of RANS and LES," AIAA Paper 2006-2516, 2006.
17. Ffowcs Williams, J. E., and Hall, L. H., "Aerodynamic Sound Generation, by Turbulent Flow in the Vicinity of a Scattering Half-Plane," Journal of Fluid Mechanics, Vol. 40, No. 4, Mar. 1970, pp. 657-670. doi:10.1017/S0022112070000368
18. Blake, W. K., "A Statistical Description of Pressure and Velocity Fields at the Trailing Edge of a Flat Strut," David Taylor Naval Ship Research and Development Center, Rept. 4241, Bethesda, MD, Dec. 1975.
19. Gloerfelt, X., Bailly, C., and Juvé, D., "Direct Computation of the Noise Radiated by a Subsonic Cavity Flow and Application of Integral Methods," Journal of Sound and Vibration, Vol. 266, No. 1, 2003, pp. 119-146. doi:10.1016/S0022-460X(02)01531-6
20. Berland, J., Bogey, C., Marsden, O., and Bailly, C., "High-Order, Low Dispersive and Low Dissipative Explicit Schemes for Multiple-Scale and Boundary Problems," Journal of Computational Physics, Vol. 224, No. 2, June 2007, pp. 637-662. doi:10.1016/j.jcp.2006.10.017
21. Visbal, M., and Rizzetta, D., "Large-Eddy Simulation on Curvilinear Grids Using Compact Differencing and Filtering Schemes," Journal of Fluids Engineering, Vol. 124, No. 4, 2002. doi:10.1015/1.1517564
22. Rizzetta, D. P., Visbal, M. R., and Blaisdell, G. A., "A Time-Implicit High-Order Compact Differencing and Filtering Scheme for Large-Eddy Simulation," International Journal for Numerical Methods in Fluids, Vol. 42, June 2003, pp. 665-693. doi:10.1012/fld.551
23. Bogey, C., and Bailly, C., "Effects Of Inflow Conditions and Forcing on a Mach 0.9 Jet and Its Radiated Noise," AIAA Journal, Vol. 43, No. 5, 2005, pp. 1000-1007.
24. Bogey, C., and Bailly, C., "An Analysis of the Correlations Between the Turbulent Flow and the Sound Pressure Fields of Subsonic Jets," Journal of Fluid Mechanics, Vol. 583, 2007, pp. 71-97. doi:10.1017/S002211200700612X
25. Gaitonde, D., and Visbal, M., "Padé-Type Higher-Order Boundary Filters for the Navier-Stokes Equations," AIAA Journal, Vol. 38, No. 11, Nov. 2000, pp. 2103-2112.
26. Tarn, C. K. W., and Dong, Z., "Radiation and Outflow Boundary Conditions for Direct Computation of Acoustic and Flow Disturbances In a Nonuniform Mean Flow," Journal of Computational Acoustics, Vol. 4, No. 2, 1996, pp. 175-201. doi:10.1142/S0218396X96000040
27. Bogey, C., and Bailly, C., "Three-Dimensional Nonreflective Boundary Conditions for Acoustic Simulations: Far Field Formulation and Validation Test Cases," Acta Acustica, Vol. 88, No. 4, 2002, pp. 463-471; also available online at https://www.eaa-fenestra.org/Products/ActaAcustica/ most_cited/acta_88_2002_Bogey.pdf.
28. Hixon, R., Nallasamy, M., and Sawyer, S. D., "Parallelization Strategy for an Explicit Computational Aeroacousties Code," AIAA Paper 2002-2583, 2002.
29. Dahlström, S., and Davidson, L., "Large Eddy Simulation of the Flow Around an Airfoil," AIAA Paper 2001-0425, 2001.
30. Davidson, L., Cokljat, D., Fröhlich, J., Leschziner, M. A., Mellen, C., and Rodi, W., LESFOIL: Large Eddy Simulation of the Flow Around a High-Lift Airfoil, Notes on Numer. Fluid Mech., Vol. 83, Springer, New York, 2003.
31. Mellen, C., Fröhlich, J., and Rodi, W., "Lessons from the European LESFOIL Project on LES of Flow Around an Airfoil," AIAA Paper 2002-0111, 2002.
32. Faikner, V. M., and Skan, W., "Some Approximate Solutions of the Boundary Layer Equations," Aeronautical Research Council Reports and Memoranda No. 1314, London, 1930.
33. Clauser, F. H., "Turbulent Boundary Layers in Adverse Pressure Gradients," Journal of the Aeronautical Sciences, Vol. 21, No. 2, 1954, pp. 91-108.
34. Lee, H. K., and Kang, S. H., "Flow Characteristics of Transitional Boundary Layers on an Airfoil in Wakes," Journal of Fluids Engineering, Vol. 122, No. 3, Sept. 2000, pp. 522-532. doi:10.1115/1.1287592
35. Evans, R. L., "Freestream Turbulence Effects on Turbulent Boundary Layers in Adverse Pressure Gradients," AIAA Journal, Vol. 23, No. 11, 1985, pp. 1814-1816.
36. Hoffman, J. A., Kassir, S. M., and Larwood, S. M., 'The Influence of Freestream Turbulence on Turbulent Boundary Layers with Mild Adverse Pressure Gradients," NASA. CR 177520, 1989.
37. Kerho, M. F., and Bragg, M. B., "Airfoil Boundary-Layer Development and Transition with Large Leading-Edge Roughness," AIAA Journal, Vol. 35, No. 1, 1997.
38. Silverstein, A., and Becker, J. V., "Determination of the Boundary-Layer Transition on Three Symmetrical Airfoils in the N.A.C.A, Full-Scale Wind Tunnel," NACA, TR 637, 1938.
39. Gartenberg, E., and Roberts, A. S., Jr., "Airfoil Transition and Separation Studies Using an Infrared Imaging System," Journal of Aircraft, Vol. 28, No. 4, 1991, pp. 225-230.
40. Afzal, N., "Wake Layer in a Turbulent Boundary Layer with Pressure Gradient: A New Approach," IUTAM Symposium on Asymptotic Methods for Turbulent Shear Flows at High Reynolds Numbers, edited by K. Gersten, Kluwer Academic, Norwell, MA, 1996.
41. Schlichting, H., Boundary Layer Theory, McGraw-Hill, New York, 1968.
42. Panton, R. L., "Overview of the Self-Sustaining Mechanisms of Wall Turbulence," Progress in Aerospace Sciences, Vol. 37, No. 4, 2001, pp. 341-383. doi:10.1016/S0376-0421(01)00009-4
43. Mislevy, S. P., and Wang, T., "The Effects of Adverse Pressure Gradients on Momentum and Thermal Structures in Transitional Boundary Layers, Part 2: Fluctuation Quantities," Journal of Turbomachinery, Vol. 118, No. 4, Oct. 1996, pp. 728-732.
44. Theodorsen, T., "Mechanism of Turbulence," Proceedings of the Second Midwestern Conference on Fluid Mechanics, Ohio State Univ., Columbus, OH, 1952, pp. 1-18.
45. Robinson, S. K., "Coherent Motions in the Turbulent Boundary Layer," Annual Review of Fluid Mechanics, Vol. 23, 1991. doi:10.1146/annurev.fl.23.01019.003125
46. θ = 1.41.0," Journal of Fluid Mechanics, Vol. 187, 1988, pp. 61-98. doi:10.1017/S0022112088000345
47. Kline, S. J., Reynolds, W. C., Schraub, F. A., and Runstadler, P. W., "The Structure of Turbulent Boundary Layers," Journal of Fluid Mechanics, Vol. 30, Dec. 1967, pp. 741-773. doi:10.1017/S0022112067001740
48. Brooks, T., Pope, S., and Marcolini, M., "Airfoil Self-Noise and Prediction," NASA TR 1218, July 1989.
49. Roger, M., Moreau, S., and Wang, M., "An Analytical Model for Predicting Airfoil Self-Noise Using Wall Pressure Statistics," Annual Research Briefs, Center for Turbulence Research, Stanford Univ., Stanford, Ca, 2002.
50. McAlpine, A., Nash, E. C., and Lowson, M. V., "On the Generation of Discrete Tones by the Flow Around an Aerofoil,"Journal of Sound and Vibration, Vol. 222, No. 5, 1999, pp. 753-779. 10.1006/jsvi.1998.2085
51. Anderson, D. A., Tannehill, J. C., and Fletcher, R. H., Computational Fluid Mechanics and Heat Transfer, Hemisphere, New York, 1984.