Detached-eddy simulation with compressibility corrections applied to a supersonic axisymmetric base flow

Journal of Fluids Engineering, Transactions of the ASME

Volumn 124, Issue 4, 2002, Pages 911-923

  Forsythe, James R ^a   Hoffmann, Klaus A ^b   Cummings, Russell M ^c   Squires, Kyle D ^d  

^a UNITED STATES AIR FORCE ACADEMY   (United States)

^b Wichita State University   (United States)

^c CALIFORNIA POLYTECHNIC STATE UNIVERSITY   (United States)

^d Arizona State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DETACHED-EDDY SIMULATION (DES); LARGE-EDDY SIMULATION (LES); REYNOLDS-AVERAGED NAVIER STOKES (RANS) SIMULATIONS; SUPERSONIC AXISYMMETRIC BASE FLOW; TURBULENCE MODEL;

AERODYNAMICS; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; DRAG; MATHEMATICAL MODELS; NAVIER STOKES EQUATIONS; PRESSURE EFFECTS; REYNOLDS NUMBER; SUPERSONIC FLOW; TRANSPORT PROPERTIES; TURBULENCE;

COMPRESSIBLE FLOW;

EID: 0038149982     PISSN: 00982202     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1517572     Document Type: Article

References (53)

1. Forsythe, J R., Hoffmann, K. A , and Dieteker, F.-F., 2000, "Detached-Eddy Simulation of a Supersonic Axisymmetnc Base Flow With an Unstructured Solver," AIAA Paper No 2000-2410.
2. Cummings, R. M., Yang, H. T., and Oh, Y. H., 1995, "Supersonic. Turbulent Flow Computation and Drag Optimization for Axisymmetric Afterbodies," Comput Fluids, 24(4), pp. 487-507.
3. Spalart, P. R., 1999, "Strategies for Turbulence Modeling and Simulations," 4th International Symposium on Engineering Turbulence Modelling and Measurements, Elsevier Science, Oxford, UK, pp 3-17.
4. Spalart, P. R., Jou, W-H., Strelets, M., and Allmaras, S. R., 1997, "Comments on the Feasibility of LES for Wings, and on a Hybrid RANS/LES Approach," Advances in DNS/LES, 1st AFOSR International Conference an DNS/LES, Greyden Press, Columbus, OH.
5. Shur, M. Spalart, P. R., Strelets, M , and Travin, A , 1999, "Detached-Eddy Simulation of an Airfoil at High Angle of Attack," 4th International Symposium on Engineering Turbulence Modelling and Measurements, Elsevier Science, Oxford, UK, pp. 669-678.
6. Constantinescu, G. S., and Squires, K. D., 2000, "LES and DES Investigations of Turbulent Flow Over a Sphere," AIAA Paper No. 2000-0540
7. Travin, A., Shur, M., Strelets, M , and Spalart, P. R , 2000, "Detached-Eddy Simulation Past a Circular Cylinder," Int J Flow, Turb. Combust, 63(1-4), pp 293-313
8. Strelets, M., 2001, "Detached Eddy Simulation of Massively Separated Flows," AIAA Paper No. 2001-0879.
9. Herrin, J. L., and Dutton, J. C., 1994, "Supersonic Base Flow Experiments in the Near Wake of a Cylindrical Afterbody," AIAA J , 32(1), pp 77-83.
10. Bourdon, C. J., Smith, K M. Dutton, M., and Mathur, T. 1998, "Planar Visualizations of Large-Scale Turbulent Structures in Axisymmetnc Supersonic Base Flows," AIAA Paper No. 98-0624.
11. Murthy, S. N. B., and Osborn, J. R., 1976, "Base Flow Phenomena With and Without Injection: Experimental Results, Theories, and Bibliography," Aerodynamics of Base Combustion, S. N. B. Murthy et al, eds. (Vol. 40 of Progress in Astronautics and Aeronautics). AIAA. Melville, NY, pp. 7-210
12. Dutton, J C , Herrin, J. L , Molezzi, M. J., Mathur, T., and Smith, K. M., 1995, "Recent Progress un High-Speed Separated Base Flows," AIAA Paper No. 95-0472
13. Morkovin, M V., 1964, "Effects of Compressibility on Turbulent Flows," The Mechanics of Turbulence, A. Favre, ed., Gordon and Breach, New York, pp. 367-380.
14. Rubesin, M. W , "Compressibility Effects in Turbulence Modeling," 1980-81 AFOSR-HTTM-Stanford Conference On Complex Turbulent Flows, Stanford University, Department of Mechanical Engineering, pp. 713-723.
15. Goebel, S. G., and Duttori, J. C., 1991, "Experimental Study of Compressible Turbulent Mixing Layers," AIAA J , 29(4), pp. 538-546.
16. Clemens, N T., and Mungal, M. G., 1992, "Two- and Three-Dimensional Effects in the Supersonic Mixing Layer," AIAA J., 30(4), pp 973-981
17. Delery, J., and Lacau, R. G., 1987, "Prediction of Base Flows, " AGARD Report 654
18. Pope, S. B., and Whitelaw, J. H . 1976, "The Cakulation of Near-Wake Flows," J. Fluid Mech., 73(1), pp. 9-32.
19. Putnam, L. E., and Bissinger, N. C , 1985, "Results of AGARD Assessment of Prediction Capabilities for Nozzle Afterbody Flows," AIAA Paper No 85-1464.
20. Petrie, H. L., and Walker, B. J., 1985, "Comparison of Experiment and Computation lor a Missile Base Region Flow field With a Centered Propulsive Jet," AIAA Paper No. 85-1618.
21. Benay, R., Coet, M. C., and Delery, J., 1987, "Validation of Turbulence Models Applied to Transonic Shock-Wave/Boundary-Layer Interaction," Rech. Aerosp , 3. pp. 1-16
22. Caruso, S. C. and Childs, R. E., 1988, "Aspects of Grid Topology for Reynolds-Averaged Navier-Stokes Base Flow Computations," AIAA Paper No. 88-0523.
23. Childs, R. E , and Caruso, S. C , 1987, "On the Accuracy of Turbulent Base Flow Predictions," AIAA Paper No. 87-1439
24. Childs, R. E., and Caruso, S. C., 1989, "Assessment of Modeling and Discretization Accuracy for High Speed Afterbody Flows," AIAA Paper No 89-0531.
25. Peace, A. J., 1991, "Turbulent Flow Predictions for Afterbody/ Nozzle Geometries Including Base Effects," J. Propul Power, 24(3), pp. 396-403.
26. Tucker, P. K , and Shyy, W., 1993, "A Numerical Analysis of Supersonic Flow Over an Axisymmetric Afterbody," AIAA Paper No. 93-2347.
27. Suzen, Y. B., Hoffmann, K A , and Forsythe, J. R , 1999, "Application of Several Turbulence Models for High Speed Shear Layer Flows," AIAA Paper No 99-0933.
28. Sahu, J., 1994, "Numerical Computations of Supersonic Base Flow with Special Emphasis on Turbulence Modeling," AIAA J., 32(7), pp. 1547-1549
29. Chuang, C. C., and Chieng, C. C., 1996, "Supersonic Base Flow Computations Using Higher Order Turbulence Models," J. Spacecr. Rockets, 33(3), pp. 374-380.
30. Forsythe, J. R., Strang, W., and Hoffmann, K. A., 2000, "Validation of Several Reynolds-Averaged Turbulence Models in a 3D Unstructured Grid Code," AIAA Paper No. 2000-2552.
31. Harris, P J., and Fasel, H. F., 1998, "Numerical Investigation of the Unsteady Behavior of Supersonic Plane Wakes," AIAA Paper No. 98-2947
32. Fureby, C. Nikson, Y., and Andersson, K., 1999, "Large Eddy Simulation of Supersonic Base Flow," AIAA Paper No. 99-0426.
33. Mathur, T., and Dutton, J. C , 1996, "Base Bleed Experiments With a Cylindrical Afterbody in Supersonic Flow,'' J. Spacecr. Rockets. 33(1), pp. 30-37.
34. Baurle, R A., Tam. C.-J., Edwards, J R., and Hassan, H. A , 2001, "An Assessment of Boundary Treatment and Algorithm Issues on Hybrid RANS/ LES Solution Strategies," AIAA Paper No. 2001-2562.
35. 60: A Parallel, Implicit, Unstructured Euler/Navier-Stokes Flow Solver," AIAA Paper No. 99-0786.
36. Tomaro, R F, Strang, W. Z , and Sankar, L N , 1997, "An Implicit Algorithm for Solving Time Dependent Flows on Unstructured Grids," AIAA Paper No 97-0333.
37. Grismer, M. J., Strang, W Z., Tomaro, R. F., and Witzemman, F. C., 1998, "Cobalt A Parallel, Implicit, Unstructured Euler/Navier-Stokes Solver,'' Adv. Eng. Software, 29(3-6), pp. 365-373.
38. Karypis, G , and Kumar, V., 1997, "METIS Unstructured Graph Partitioning and Sparse Matrix Ordering System Version 2.0," Department of Computer Science, University of Minnesota, Minneapolis, MN
39. Karypis, G., Schloegel, K , and Kumar, V. 1997, "ParMETIS- Parallel Graph Partitioning and Sparse Matrix Ordering Library Version 1 0," Department of Computer Science, University of Minnesota, Minneapolis, MN.
40. Gottlieb, J J., and Groth, C. P. T., 1988, "Assessment of Reimann Solvers for Unsteady One-Dimensional Inviscid Flows of Perfect Gases," J. Comput. Phys., 78, pp. 437-458.
41. Spalart, P R., and Allmaras, S. R., 1992, "A One-Equation Turbulence Model for Aerodynamic Flows," AIAA Paper No 92-0439.
42. Spalart, P. R., 2000, "Trends in Turbulence Treatments," AIAA Paper No. 2000-2306.
43. Shur, M., Strelets, M , Zatkov, L., Gulyaev, A , Kozlov, V., and Secundov, A., "Comparative Numerical Testing of One- and Two-Equation Turbulence Models for Flows with Separation and Reattachment," AIAA Paper No. 95-0863.
44. Menter, F R , 1991, "Influence of Freestream Values on k - ω Turbulence Model Predictions," AIAA J., 30(6), pp. 1657-1659.
45. Menter, F. R., 1992, "Improved Two-Equation k - ω Turbulence Models for Aerodynamic Flows," NASA-TM-103975.
46. Menter, F. R , 1994, "Two-Equation Eddy-Viscosity Turbulence Models for Engineering Applications," AIAA J., 32(8), pp. 1598-1605.
47. Suzen, Y. B., and Hoffmann, K A., 1998, "Investigation of Supersonic Jet Exhaust Flow by One- and Two-Equation Turbulence Models," AIAA Paper No. 98-0322
48. Forsythe, J. R., Hoffmann, K A., and Suzen, Y. B., 1999, "Investigation of Modified Menter's Two-Equation Turbulence Models for Supersonic Applications," AIAA Paper No. 99-0873.
49. Wilcov D. C., 1998, Turbulence Modeling for CFD, 2nd Ed., DCW Industries, La Canada, CA.
50. Pirzadeh, S , 1996, "Three-Dimensional Unstructured Viscous Grids by the Advancing Layers Method," AIAA J , 34(1), pp. 43-49.
51. Steinbrenner, J., Weyman, N., and Chawner, J., 2000, "Development and Implementation of Gndgen's Hyperbolic PDE and Extrusion Methods," AIAA Paper No. 2000-0679.
52. Spalart, P., 2001, "Young-Person's Guide to Detached-Eddy Simulation Grids," NASA CR 2001-211032.
53. Forsythe, J. R , Hoffmann, K A , and Squires, K. D., 2002, "Detached-Eddy Simulation With Compressibility Corrections Applied to a Supersonic Axisymmetric Base Flow," AIAA Paper No. 2002-0586.