Atering turbulence in compressible base flow using axisymmetric sub-boundary-layer disturbances

AIAA Journal

Volumn 40, Issue 11, 2002, Pages 2217-2224

  Bourdon, C J ^a,b   Dutton, J C ^a  

^a UNIVERSITY OF ILLINOIS AT URBANA CHAMPAIGN   (United States)

^b SANDIA NATIONAL LABORATORIES   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; COMPRESSIBLE FLOW; PRESSURE EFFECTS; RAYLEIGH SCATTERING; TURBULENCE; VISUALIZATION;

MACH NUMBER;

AERODYNAMICS;

EID: 0036848273     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1583     Document Type: Article

References (25)

1. Wishart, D.P., Krothapalli, A., and Mungal, M.G., "Supersonic Jet Control via Point Disturbances Inside the Nozzle," AIAA Journal, Vol. 31, No. 7, 1993, pp. 1340, 1341.
2. Glawe, D.D., Samimy, M., Nejad, A.S., and Chen, T.H., "Effects of Nozzle Geometry on Parallel Injection into a Supersonic Flow," Journal of Propulsion and Power, Vol. 12, No. 6, 1996. pp. 1159-1168.
3. Raman, G., and Rice, E.J., "Supersonic Jet Mixing Enhancement Using Impingement Tones from Obstacles of Various Geometries," AIAA Journal, Vol. 33, No. 3, 1995, pp. 454-462.
4. Viswanath, P.R., and Narasimha, R., "Two-Dimensional Boat-Tailed Bases in Supersonic Flow," Aeronautical Quarterly, Vol. 25, No. 3, 1974, pp. 210-224.
5. Viswanath, P.R., and Patil, S.R., "Effectiveness of Passive Devices for Axisymmetric Base Drag Reduction at Mach 2," Journal of Spacecraft and Rockets, Vol. 27, No. 6, 1990, pp. 234-237.
6. Island, T.C., Urban, W.D., and Mungal, M.G., "Mixing Enhancement in Compressible Shear Layers via Sub-Boundary Layer Disturbances,"Physics of Fluids, Vol. 10, No. 4, 1998, pp. 1008-1020.
7. King, C.J., Krothapalli, A., and Strykowski, P.J., "Streamwise Vorticity Generation in Supersonic Jets with Minimal Thrust Loss," AIAA Paper 94-0661, Jan. 1994.
8. Bourdon, C.J., and Dutton, J.C., "Mixing Enhancement in Compressible Base Flows via Generation of Streamwise Vorticity," AIAA Journal, Vol. 39, No. 8, 2001, pp. 1633-1635.
9. Herrin, J.L., and Dutton, J.C., "Effect of a Rapid Expansion on the Development of Compressible Free Shear Layers," Physics of Fluids, Vol. 7, No. 1, 1995, pp. 159-171.
10. Arnette, S.A., Samimy, M., and Elliott, G.S., "The Effects of Expansion on the Turbulence Structure of Compressible Boundary Layers," Journal of Fluid Mechanics, Vol. 367, 1998, pp. 67-105.
11. Smith, D.R., and Smits, A.J., "Multiple Distortion of a Supersonic Turbulent Boundary Layer," Applied Scientific Research, Vol. 51, No. 1-2, 1993, pp. 223-229.
12. Bradshaw, P., "The Effect of Mean Compression or Dilatation on the Turbulence Structure of Supersonic Boundary Layers," Journal of Fluid Mechanics, Vol. 63, No. 3, 1973, pp. 449-464.
13. Smith, K.M., and Dutton, J.C., "Investigation of Large-Scale Structures in Supersonic Planar Base Flows," AIAA Journal, Vol. 34, No. 6, 1996, pp. 1146-1152.
14. Bourdon, C.J., and Dutton, J.C., "Planar Visualizations of Large-Scale Turbulent Structures in Axisymmetric Supersonic Separated Flows," Physics of Fluids, Vol. 11, No. 1, 1999, pp. 201-213.
15. Bourdon, C.J., and Dutton, J.C., "Shear-Layer Flapping and Interface Convolution in a Separated Supersonic Flow," AIAA Journal, Vol. 38, No. 10, 2000, pp. 1907-1915.
16. Bourdon, C.J., and Dutton, J.C., "Effects of Boattailing on the Turbulence Structure of a Compressible Base Flow," Journal of Spacecraft and Rockets, Vol. 38, No. 4, 2001, pp. 534-541.
17. Herrin, J.L., and Dutton, J.C., "Supersonic Base Flow Experiments in the Near Wake of a Cylindrical Afterbody," AIAA Journal, Vol. 32, No. 1, 1994, pp. 77-83.
18. Krothapalli, A., Strykowski, P.J., and King, C.J., "Origin of Streamwise Vortices in Supersonic Jets," AIAA Journal, Vol. 36, No. 5, 1998, pp. 869-872.
19. Herrin, J.L., "An Experimental Investigation of Supersonic Axisymmetric Base Flows Including the Effects of Afterbody Boattailing," Ph.D. Dissertation, Dept. of Mechanical and Industrial Engineering, Univ. of Illinois at Urbana-Champaign, Urbana, IL, July 1993.
20. Clemens, N.T., and Mungal, M.G., "A Planar Mie Scattering Technique for Visualizing Supersonic Mixing Flows," Experiments in Fluids, Vol. 11, No. 2, 1991, pp. 175-185.
21. Elliott, G.S., Samimy, M., and Arnette, S.A., "The Characteristics and Evolution of Large-Scale Structures in Compressible Mixing Layers," Physics of Fluids, Vol. 7, No. 4, 1995, pp. 864-876.
22. Messessmith, N.L., and Dutton, J.C., "Characteristic Features of Large Structures in Compressible Mixing Layers," AIAA Journal, Vol. 34, No. 9, 1996, pp. 1814-1821.
23. Smith, K.M., "The Role of Large Structures in Compressible Reattaching Shear Flows," Ph.D. Dissertation, Dept. of Mechanical and Industrial Engineering, Univ. of Illinois at Urbana-Champaign, Urbana, IL, Aug. 1996.
24. Smith, K.M., and Dutton, J.C., "Procedure for Turbulent Structure Convection Velocity Measurements Using Time-Correlated Images," Experiments in Fluids, Vol. 27, No. 3, 1999, pp. 244-250.
25. Tourbier, D., and Fasel, H., "Numerical Investigation of Transitional Axisymmetric Wakes at Supersonic Speeds," AIAA Paper 94-2286, Jan. 1994.