Large-eddy simulation of a wing tip vortex on overset grids

AIAA Journal

Volumn 44, Issue 6, 2006, Pages 1229-1242

  Uzun, Ali ^a,c,d   Yousuff Hussaini, M ^a,e   Streett, Craig L ^b,f  

^a FLORIDA STATE UNIVERSITY   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

^c Robotics Institute   (United States)

^d AIAA   (United States)

^e Department of Mathematics and Computational Science and Engineering

^f Aerospace Technologist   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERONAUTICAL APPLICATIONS; GRID CAPABILITY; GRID TOPOLOGY; LARGE EDDY SIMULATION (LES);

ACOUSTIC NOISE; BOUNDARY CONDITIONS; COMPUTER SIMULATION; NUMERICAL ANALYSIS; TOPOLOGY; TURBOMACHINE BLADES; WIND TURBINES;

VORTEX FLOW;

EID: 33746349222     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.17999     Document Type: Article

References (42)

1. Chow, J., Zilliac, G., and Bradshaw, P., "Turbulence Measurements in the Near Field of a Wingtip Vortex," NASA TM 110418, Feb. 1997.
2. Chow, J. S., "Turbulence Measurements in the Near-Field of a Wingtip Vortex," Ph.D. Dissertation, Dept. of Mechanical Engineering, Stanford Univ., Stanford, CA, Aug. 1994.
3. Radeztsky, R. H., Singer, B. A., and Khorrami, M. R., "Detailed Measurements of a Flap Side-Edge How Field," AIAA Paper 98-0700, 1998.
4. Dacles-Mariani, J., Zilliac, G. G., Chow, J. S., and Bradshaw, P., "Numerical/Experimental Study of a Wingtip Vortex in the Near Field," AIAA Journal, Vol. 33, No. 9, 1995, pp. 1561-1568.
5. Dacles-Mariani, J., Kwak, D., and Zilliac, G., "On Numerical Errors and Turbulence Modeling in Tip Vortex Flow Prediction," International Journal for Numerical Methods in Fluids, Vol. 30, No. 1, 1999, pp. 65-82.
6. Kim, S.-E., and Rhee, S. H., "Prediction of Tip-Vortex Flow past a Finite Wing," AIAA Paper 2005-0058, Jan. 2005.
7. Takallu, M. A., and Laflin, K. R., "Reynolds-Averaged Navier-Stokes Simulations of Two Partial-Span Flap Wing Experiments," AIAA Paper 98-0701, 1998.
8. Khorrami, M. R., Singer, B. A., and Radeztsky, R. H., "Reynolds Averaged Navier-Stokes Computations of a Flap Side-Edge Flow Field," AIAA Paper 98-0768, 1998.
9. Fleig, O., Iida, M., and Arakawa, C., "Wind Turbine Blade Tip Flow and Noise Prediction by Large-Eddy Simulation," Journal of Solar Energy Engineering, Vol. 126, No. 4, 2004, pp. 1017-1024.
10. Fleig, O., Iida, M., and Arakawa, C., "Wind Turbine Flow and Noise Prediction by Large Eddy Simulation," AIAA Paper 2005-1188, Jan. 2005.
11. Cai, J., Deng, S., Xie, P., and Liu, C., "High-Order LES for Wing Tip Vortex in the Near Field," AIAA Paper 2005-1125, Jan. 2005.
12. Ghias, R., Mittal, R., Dong, H., and Lund, T., "Study of Tip-Vortex Formation Using Large-Eddy Simulation," AIAA Paper 2005-1280, Jan. 2005.
13. Imamura, T., Enomoto, S., Kato, H., Yokokawa, Y., and Yamamoto, K., "Numerical Simulation of NACA0012 Wingtip Flow Leading to Noise Generation," AIAA Paper 2005-2864, 2005.
14. Mittal, R., and Moin, P., "Suitability of Upwind-Biased Finite Difference Schemes for Large-Eddy Simulation of Turbulent Flows," AIAA Journal, Vol. 35, No. 8, 1997, pp. 1415-1417.
15. Visbal, M. R., and Gaitonde, D. V., "Very High-Order Spatially Implicit Schemes for Computational Acoustics on Curvilinear Meshes," Journal of Computational Acoustics, Vol. 9, No. 4, 2001, pp. 1259-1286.
16. Ashcroft, G., and Zhang, X., "Optimized Prefactored Compact Schemes," Journal of Computational Physics, Vol. 190, No. 2, 2003, pp. 459-457.
17. Uzun, A., "3-D Large Eddy Simulation for Jet Aeroacoustics," Ph.D. Dissertation, School of Aeronautics and Astronautics, Purdue Univ., West Lafayette, IN, Dec. 2003.
18. Uzun, A., Blaisdell, G. A., and Lyrintzis, A. S., "Application of Compact Schemes to Large Eddy Simulation of Turbulent Jets," Journal of Scientific Computing, Vol. 21, No. 3, 2004, pp. 283-319.
19. 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, 2004, pp. 297-346.
20. Gaitonde, D. V., and Visbal, M. R., "Padé-Type Higher-Order Boundary Filters for the Navier-Stokes Equations," AIAA Journal, Vol. 38, No. 11, 2000, pp. 2103-2112.
21. Lele, S. K., "Compact Finite Difference Schemes with Spectral-Like Resolution," Journal of Computational Physics, Vol. 103, No. 1, 1992, pp. 16-42.
22. Beam, R. M., and Warming, R. F., "An Implicit Factored Scheme for the Compressible Navier-Stokes Equations," AIAA Journal, Vol. 16, No. 4, 1978, pp. 393-402.
23. Ekaterinaris, J. A., "Implicit, High-Resolution, Compact Schemes for Gas Dynamics and Aeroacoustics," Journal of Computational Physics, Vol. 156, No. 2, 1999, pp. 272-299.
24. Pulliam, T. H., "Artificial Dissipation Models for the Euler Equations," AIAA Journal, Vol. 24, No. 12, 1986, pp. 1931-1940.
25. Tam, 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.
26. Bogey, C., and Bailly, C., "Three-Dimensional Non-Reflective Boundary Conditions for Acoustic Simulations: Far Field Formulation and Validation Test Cases," Acta Acustica, Vol. 88, No. 4, 2002, pp. 463-471.
27. Kim, J. W., and Lee, D. J., "Generalized Characteristic Boundary Conditions for Computational Aeroacoustics," AIAA Journal, Vol. 38, No. 11, 2000, pp. 2040-2049.
28. Kim, J. W., and Lee, D. J., "Generalized Characteristic Boundary Conditions for Computational Aeroacoustics, Part 2," AIAA Journal, Vol. 42, No. 1, 2004, pp. 47-55.
29. Visbal, M. R., and Rizzetta, D. P., "Large-Eddy Simulation on Curvilinear Grids Using Compact Differencing and Filtering Schemes," Journal of Fluids Engineering, Vol. 124, No. 4, 2002, pp. 836-847.
30. Visbal, M. R., Morgan, P. E., and Rizzetta, D. P., "An Implicit LES Approach Based on High-Order Compact Differencing and Filtering Schemes (Invited)," AIAA Paper 2003-4098, June 2003.
31. Bogey, C., and Bailly, C., "Decrease of the Effective Reynolds Number with Eddy-Viscosity Subgrid-Scale Modeling," AIAA Journal, Vol. 43, No. 2, 2005, pp. 437-439.
32. Benek, J. A., Steger, J. L., Dougherty, F. C., and Buning, P. G., "Chimera: A Grid-Embedding Technique," Arnold Engineering Development Center, Rept. AEDC-TR-85-64, Arnold Air Force Station, TN, April 1986.
33. Henshaw, W., "Ogen: An Overlapping Grid Generator for Overture," Lawrence Livermore National Lab., Livermore, CA, URL: http://www.llnl.gov/casc/Overture [cited 24 June 2005].
34. Sherer, S. E., and Scott, J. N., "High-Order Compact Finite-Difference Methods on General Overset Grids," Journal of Computational Physics, Vol. 210, No. 2, 2005, pp. 459-496.
35. Sherer, S. E., "Investigation of High-Order and Optimized Interpolation Methods with Implementation in a High-Order Overset Grid Fluid Dynamics Solver," Ph.D. Dissertation, Dept. of Aeronautical and Astronautical Engineering, Ohio State Univ., Columbus, OH, Dec. 2002.
36. Brentner, K. S., and Farassat, F., "Analytical Comparison of the Acoustic Analogy and Kirchhoff Formulation for Moving Surfaces," AIAA Journal, Vol. 36, No. 8, 1998, pp. 1379-1386.
37. Chow, J. S., Zilliac, G. G., and Bradshaw, P., "Mean and Turbulence Measurements in the Near Field of a Wingtip Vortex," AIAA Journal, Vol. 35, No. 10, 1997, pp. 1561-1567.
38. National Computational Science Alliance, Univ. of Illinois, Urbana, IL, URL: http://www.ncsa.uiuc.edu/UserInfo/Resources/Hardware/XeonCluster [cited 22 Feb. 2006].
39. Tennekes, H., and Lumley, J. L., A First Course in Turbulence, MIT Press, Cambridge, MA, 1972, Chap. 5.
40. Choi, H., and Moin, P., "Effects of the Computational Time Step on Numerical Solutions of Turbulent Flow," Journal of Computational Physics, Vol. 113, No. 1, 1994, pp. 1-4.
41. McAlister, K. W., and Takahashi, R. T., "NACA 0015 Wing Pressure and Trailing Vortex Measurements," NASA TP 3151, Nov. 1991.
42. Batchelor, G. K., "Axial Flow in Trailing Line Vortices," Journal of Fluid Mechanics, Vol. 20, No. 4, 1964, pp. 645-658.