High accuracy DNS and les of high reynolds number, supersonic base flows and passive control of the near wake

Department of Defense High Performance Computing Modernization Program: Proceedings of the HPCMP Users Group Conference 2005

Volumn 2005, Issue , 2005, Pages 119-127

  Von Terzi, D A ^a   Sandberg, R D ^a   Sivasubramanian, J ^a   Fasel, H F ^a  

^a UNIVERSITY OF ARIZONA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DETACHED EDDY SIMULATIONS (DES); FLOW SIMULATION METHODOLOGY (FSM); NEAR WAKE; PASSIVE CONTROL;

COMPUTER SIMULATION; DRAG REDUCTION; FLOW CONTROL; MACH NUMBER; MISSILES; PROJECTILES; REYNOLDS NUMBER; VISUALIZATION;

SUPERSONIC FLOW;

EID: 33947716899     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/DODUGC.2005.32     Document Type: Conference Paper

References (25)

1. Rollstin, L., "Measurement of inflight base-pressure on an artillery-fired projectile." AIAA Paper, 1987, pp. 87-2427.
2. Sahu, J., C. Nietubicz, and J. Steger, "Navier-Stokes computations of projectile base flow with and without mass injection." AIAA J., 23(9), Sept 1985, pp. 1348-1355.
3. Nietubicz, C. and H. Gibeling, "Navier-Stokes computations for a reacting, M864 base bleed projectile." AIAA Paper, 93-0504, 1993.
4. Sahu, J. and C. Nietubicz, Three-dimensional flow calculations for a projectile with standard and dome bases." J. Spacecraft Rockets, 31:103, 1994.
5. Mathur, T. and C.J. Dutton, "Base-bleed experiments with a cylindrical afterbody in supersonic flow." J. Spacecraft Rockets, 33:30, 1996.
6. Mathur, T. and C.J. Dutton, "Velocity and turbulence measurements in a supersonic base flow with mass bleed." AIAA J., 34:1153, 1996.
7. Bourdon, C.J. and J.C. Dutton, "Effects of boat-tailing on the turbulence structure of a compressible base flow." AIAA Paper 2000-2312, 2000.
8. Bourdon, C.J. and J.C. Dutton, "Planar visualizations of large-scale turbulent structures in axisymmetric supersonic separated flows." Phys. Fluids, 11, 1999.
9. Bourdon, C.J. and J.C. Dutton, "Visualizations and measurements of axisymmetric base flows altered by surface disturbances." AIAA Paper 2001-0286, 2001.
10. Herrin, J.L. and J.C. Dutton, "Supersonic near-wake afterbody boat-tailing effects on axisymmetric bodies." J. Spacecraft Rockets, 31:1021, 1994.
11. Sahu, J., "Numerical computations of supersonic base flow with special emphasis on turbulence modeling." AIAA Paper 9-4352, 1992.
12. Krishnamurty, V.S. and W. Shyy, "Study of compressibility modifications to the k - ε turbulence model." Phys. Fluids, 9, 1997, pp. 2769-2788.
13. Fureby, C., "Large-eddy simulation of supersonic baseflow." AIAA Paper 99-0426, 1999.
14. Forsythe, J.R. K.A. Hoffmann, R.M. Cummings, and K.D. Squires, "Detached-eddy simulation with compressibility corrections applied to a supersonic axisymmetric base flow." J. Fluid Engng, 124, 2002, pp. 911-923.
15. Sandberg, R.D. and H.F. Fasel, "Instability mechanisms in supersonic base flows. AIAA Paper 2004-0593, Jan. 2004.
16. Sandberg, R.D. and H.F. Fasel, "High-accuracy DNS of supersonic base flows and control of the near wake." IEEE Proceedings of DoD UGC 2004, Dee. 2004.
17. Sandberg, R.D. and H.F. Fasel, "Direct numerical simulation of transitional supersonic base flows." AIAA Paper 2005-0098, 2005.
18. Fasel, H.F., D.A. von Terzi, and R.D. Sandberg, "A methodology for simulating compressible turbulent flows." FEDSM, 2003-45334, July 2003,
19. accepted for publication in J. Appl. Mech.
20. Sandberg, R.D. and H.F. Fasel, "A flow simulation methodology for supersonic high Reynolds number axisymmetric wakes." AIAA Paper 2004-0067, Jan. 2004.
21. Speziale, C.G., "A combined large-eddy simulation and time-dependent RANS capability for high-speed compressible flows." J. Sci. Comput., 13(3), Sept 1998, pp. 253-74.
22. Sandberg. R.D., "Numerical Investigation of Transitional and Turbulent Supersonic Axisymmetric Wakes." PhD thesis, The University of Arizona, 2004.
23. http://www.cobaltcfd.com/Codes/cobalt.htm.
24. Wurtzler, K.E., R.F. Tomaro, W.Z. Strang, M.J. Grismer, J.R. Forsythe, K.D. Squires, and P.R. Spalart, "Analysis of full aircraft with massive separation using detached-eddy simulation." DoD Challenge Project FY 2001/2002, AFRL.
25. Herrin, J.L. and J.C. Dutton, "Supersonic base flow experiments in the near wake of a cylindrical afterbody." AIAA J., 32(1), 1994, p. 77.