Investigation of high frequency noise generation in the near-nozzle region of a jet using large eddy simulation

Theoretical and Computational Fluid Dynamics

Volumn 21, Issue 4, 2007, Pages 291-321

  Uzun, Ali ^a   Hussaini, M Yousuff ^a  

^a FLORIDA STATE UNIVERSITY   (United States)

Author keywords

Computational aeroacoustics; Jet noise; Large eddy simulation; Shear layers

Indexed keywords

COMPUTATIONAL AEROACOUSTICS; JET NOISE; SHEAR LAYERS;

BOUNDARY LAYERS; COMPUTATION THEORY; LARGE EDDY SIMULATION; MACH NUMBER; NOZZLES; NUMERICAL METHODS;

JET ENGINES;

BOUNDARY LAYERS; COMPUTATION THEORY; JET ENGINES; LARGE EDDY SIMULATION; MACH NUMBER; NOZZLES; NUMERICAL METHODS;

ACOUSTICS; ISOTHERM; JET; LARGE EDDY SIMULATION; NOISE; SHEAR FLOW; TURBULENT BOUNDARY LAYER;

EID: 34250309279     PISSN: 09354964     EISSN: 14322250     Source Type: Journal    
DOI: 10.1007/s00162-007-0048-z     Document Type: Article

References (56)

1. http://www.ncsa.uiuc.edu/UserInfo/Resources/Hardware/XeonCluster
2. http://www.psc.edu/machines/cray/xt3/
3. Andersson, N., Eriksson, L.E., Davidson, L.: Investigation of an isothermal Mach 0.75 jet and its radiated sound using large-eddy simulation and Kirchhoff surface integration. Int. J. Heat Fluid Flow 26, 393-410 (2005)
4. Andersson, N., Eriksson, L.E., Davidson, L.: Large-eddy simulation of subsonic turbulent jets and their radiated sound. AIAA J. 43(9), 1899-1912 (2005)
5. Andersson, N., Eriksson, L.E., Davidson, L.: LES prediction of flow and acoustic field of a coaxial jet. AIAA Paper 2005-2884 (2005)
6. Ashcroft, G., Zhang, X.: Optimized prefactored compact schemes. J. Comput. Phys. 190(2), 459-457 (2003)
7. Barré, S., Bogey, C., Bailly, C.: Computation of the noise radiated by jets with laminar/turbulent nozzle-exit conditions. AIAA Paper 2006-2443 (2006)
8. Beam, R.M., Warming, R.F.: An implicit factored scheme for the compressible Navier-Stokes equations. AIAA J. 16(4), 393-402 (1978)
9. Benek, J.A., Steger, J.L., Dougherty, F.C., Buning, P.G.: Chimera: A grid-embedding technique. Arnold Engineering Development Center Report AEDC-TR-85-64, Arnold Air Force Station, TN, USA (1986)
10. Biancherin, A., Lupoglazoff, N., Rahier, G., Vuillot, F.: Comprehensive 3d unsteady simulations of subsonic and supersonic hot jet flow-fields: Part 2: Acoustic analysis. AIAA Paper 2002-2600 (2002)
11. Birch, S.F.: A review of axisymmetric jet flow data for noise applications. AIAA Paper 2006-2602 (2006)
12. Bodony, D.J., Lele, S.K.: Review of the current status of jet noise predictions using large eddy simulation (invited). AIAA Paper 2006-0468 (2006)
13. Bridges, J.E., Hussain, A.K.M.F.: Roles of initial condition and vortex pairing in jet noise. J. Sound Vibrat. 117(2), 289-311 (1987)
14. Choi. H.. Moin. P.: Effects of the computational time step on numerical solutions of turbulent flow. J. Comput. Phys. 113(1), 1-4 (1994)
15. Constantinescu, G.S., Lele, S.K.: A highly accurate technique for the treatment of flow equations at the polar axis in cylindrical coordinates using series expansions. J. Comput. Phys. 183, 165-186 (2002)
16. DeBonis, J.R.: A large-eddy simulation of a high Reynolds number Mach 0.9 jet. AIAA Paper 2004-3025 (2004)
17. DeBonis, J.R., Scott, J.N.: Large-eddy simulation of a turbulent compressible round jet. AIAA J. 40(7), 1346-1354 (2002)
18. Dong, T.Z.: On boundary conditions for acoustic computations in non-uniform mean flows. J. Comput. Acoust. 5(3), 297-315 (1997)
19. Drubka, R.E.: Instabilities in the near field of turbulent jets and their dependence on initial conditions and Reynolds number. PhD Thesis, Illinois Institute of Technology, Chicago (1981)
20. Ekaterinaris, J.A.: Implicit, high-resolution, compact schemes for gas dynamics and aeroacoustics. J. Comput. Phys. 156(2), 272-299 (1999)
21. Freund, J.B., Lele, S.K., Moin, P.: Calculation of the radiated sound field using an open Kirchhoff surface. AIAA J. 34(5), 909-916 (1996)
22. Gaitonde, D.V., Visbal, M.R.: Padé-type higher-order boundary filters for the Navier-Stokes equations. AIAA J. 38(11), 2103-2112 (2000)
23. Henshaw, W.: Ogen: An overlapping grid generator for overture. http://www.llnl.gov/casc/Overture
24. Hussain, A.K.M.F., Zaman, K.B.M.Q.: An experimental study of organized motions in the turbulent plane mixing layer. J. Fluid Mech. 159, 85-104 (1985)
25. Kim, J.W., Lee, D.J.: Generalized characteristic boundary conditions for computational aeroacoustics. AIAA J. 38(11), 2040-2049 (2000)
26. Kim, J.W., Lee. D.J.: Generalized characteristic boundary conditions for computational aeroacoustics, part 2. AIAA J. 42(1), 47-55 (2004)
27. Lele, S.K.: Compact finite difference schemes with spectral-like resolution. J. Comput. Phys. 103(1), 16-42 (1992)
28. Lund, T.S., Wu, X., Squires, K.D.: Generation of turbulent inflow data for spatially-developing boundary layer simulations. J. Comput. Phys. 140(2), 233-258 (1998)
29. Lupoglazoff, N., Biancherin, A., Vuillot, F., Rahier, G.: Comprehensive 3d unsteady simulations of subsonic and supersonic hot jet flow-fields: Part 1 : Aerodynamic analysis. AIAA Paper 2002-2599 (2002)
30. Lyrintzis, A.S.: Surface integral methods in computational aeroacoustics - from the (cfd) near-field to the (acoustic) far-field. Int. J. Aeroacoust. 2(2), 95-128 (2003)
31. Mohseni, K., Colonius, T.: Numerical treatment of polar coordinate singularities. J. Comput. Phys. 157(2), 787-795 (2000)
32. Narayanan, S., Barber, T.J., Polak, D.R.: High subsonic jet experiments: Turbulence and noise generation studies. AIAA J. 40(3), 430-437 (2002)
33. Paliath, U., Morris, P.J.: Prediction of noise from jets with different nozzle geometries. AIAA Paper 2004-3026 (2004)
34. Paliath, U., Morris, P.J.: Prediction of jet noise from circular beveled nozzles. AIAA Paper 2005-3096 (2005)
35. Piomelli, U., Balaras, E.: Wall-layer models for large-eddy simulations. Ann. Rev. Fluid Mech. 34, 349-374 (2002)
36. Pulliam, T.H.: Artificial dissipation models for the Euler equations. AIAA J. 24(12), 1931-1940 (1986)
37. Rai, M.M., Moin, P.: Direct numerical simulation of transition and turbulence in a spatially evolving boundary layer. J. Comput. Phys. 109(2), 169-192 (1993)
38. Rizzetta, D.P., Visbal, M.R., Blaisdell, G.A.: A time-implicit high-order compact differencing and filtering scheme for large-eddy simulation. Int. J. Numer. Methods Fluids 42(6), 665-693 (2003)
39. Sagaut, P., Gamier, E., Tromeur, E., Larchevêque, L., Labourasse, E.: Turbulent inflow conditions for large-eddy simulation of compressible wall-bounded flows. AIAA J. 42(3), 469-477 (2004)
40. Schlichting, H.: Boundary-layer theory. 6th edn, chap. 14, pp 689-690. McGraw-Hill Book Company. New York (1968)
41. Sherer, S.E., Scott, J.N.: High-order compact finite-difference methods on general overset grids. J. Comput. Phys. 210(2), 459-496 (2005)
42. θ = 1410. J. Fluid Mech. 187, 61-98 (1988)
43. Spalding, D.B.: A single formula for the law of the wall. J. Appl. Mech. 28, 455-457 (1961)
44. Townsend, A.A.: The structure of turbulent shear flow. Cambridge University Press, Great Britain (1976)
45. Uzun, A.: 3-d large eddy simulation for jet aeroacoustics. PhD Thesis, School of Aeronautics and Astronautics, Purdue University, West Lafayette (2003)
46. Uzun, A., Blaisdell, G.A., Lyrintzis, A.S.: Application of compact schemes to large eddy simulation of turbulent jets..I. Sci. Comput. 21(3), 283-319 (2004)
47. Uzun. A., Hussaini, M.Y.. Streett. C.L.: Large-eddy simulation of a wing tip vortex on overset grids. AIAA J. 44(6), 1229-1242 (2006)
48. Uzun, A., Lyrintzis, A.S., Blaisdell, G.A.: Coupling of integral acoustics methods with LES for jet noise prediction. Int. J. Aeroacoust. 3(4), 297-346 (2004)
49. Visbal, M.R., Gaitonde, D.V.: Very high-order spatially implicit schemes for computational acoustics on curvilinear meshes. J. Comput. Acoust.9(4). 1259-1286 (2001)
50. Visbal, M.R., Morgan, P.E., Rizzetta, D.P.: An implicit LES approach based on high-order compact differencing and filtering schemes (invited). AIAA Paper 2003-4098 (2003)
51. Visbal, M.R., Rizzetta, D.P.: Large-eddy simulation on curvilinear grids using compact differencing and filtering schemes. J. Fluids Eng. 124(4), 836-847 (2002)
52. Viswanathan. K.: Aeroacoustics of hot jets. J. Fluid Mech. 516. 39-82 (2004)
53. Viswanathan, K., Clark, L.T.: Effect of nozzle internal contour on jet aeroacoustics. Int. J. Aeroacoust. 3(2), 103-135 (2004)
54. Viswanathan, K., Shur, M.L., Spalart, P.R., Strelets, M.K.: Computation of the flow and noise of round and beveled nozzles. AIAA Paper 2006-2445 (2006)
55. Wu, X., Tristanto, I.H., Page, G.J., McGuirk, J.J.: Influence of nozzle modelling in LES of turbulent free jets. AIAA Paper 2005-2883 (2005)
56. Zaman, K.B.M.Q.: Effect of initial condition on subsonic jet noise. AIAA J. 23(9), 1370-1373 (1984)