Supersonic mixing and combustion control using streamwise vortices

34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 1998, Pages

  Sunami, Tetsuji ^a   Wendt, Michael N ^b   Nishioka, Michio ^c  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b UNIVERSITY OF QUEENSLAND   (Australia)

^c Osaka Prefecture University   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC STREAMING; COMBUSTION; HYDROGEN FUELS; PROPULSION; SHOCK WAVES; STRUTS; VORTEX FLOW;

COMBUSTION CONTROL; FORMATION MECHANISM; MIXING ENHANCEMENT; NUMERICAL RESULTS; ROTATIONAL DIRECTIONS; STREAMWISE VORTICES; SUPERSONIC MIXING; TOTAL PRESSURE;

MIXING;

EID: 85088195575     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-3271     Document Type: Conference Paper

References (33)

1. Ferri, A., “Mixing-Controlled Supersonic Combustion,” Ann. Rev. Fluid Mech. Vol. 5, 301-338, 1973.
2. Gutmark, E. J., Schadow, K. C. and Yu, K. H., “ Mixing Enhancement in Supersonic Free Shear Flows,” Ann. Rev. Fluid Mech. Vol. 27, 375-417, 1995.
3. Sunami, T., Sakuranaka, N., Tani, K., Hiraiwa, T. and Shimura, T., “ Mach 4 Tests of a Scramjet Engine - Effects of Isolator,” 13th ISABE,Vol. 1,615-625, 1997.
4. Bogdanoff, D. W.,” Compressibility Effects in Turbulent Shear Layers,” AIAA J. Vol. 21, 926-927, 1982.
5. Papamoschou, D. and Roshko, A., “The Compressible Turbulent Shear Layer: Experimental Study,” J. Fluid Mech. Vol. 197, 453-477, 1988.
6. Chinzei, N., Masuya, G., Komuro, T., Murakami, A. and Kudou, K.,” Spreading of Two-Stream Supersonic Mixing Layers,” Phys. Fluids Vol. 29(5), 1345-1347, 1986.
7. Brown, G.L. and Roshko, A., “ On Density Effects and Large Structure in Turbulent Mixing Layers,” J. Fluid Mech. Vol. 64, 775-816, 1974.
8. Lessen, M., Fox, J. A. and Zien, H. M.,” On the Inviscid Stability of the Laminar Mixing of Two Parallel Streams of a Compressible Fluid,” J. Fluid Mech. Vol. 23, 355-367, 1965.
9. Sandham, N. D. and Reynolds, W. C., “ Compressible Mixing Layer: Linear Theory and Direct Simulation,” AIAA J. Vol. 28, 618-624, 1990.
10. Sandham, N. D. and Reynolds, W. C., “ Three-dimensional simulations of large eddies in the compressible mixing layer,” J. Fluid Mech. Vol. 224, 133-158, 1991.
11. Clements, N. T. and Mungal, M. G., “ Twoand Three- Dimensional Effects in the Supersonic Mixing Layer,” AIAA J. Vol. 30(4), 973-981, 1992.
12. Elliott, G. S. and Samimy, M., “ Compressibility Effects in Free Shear Layers,” Phys. Fluids A2, 1231-1240, 1990.
13. Samimy, M., Reeder, M. F. and Elliott, G. S., “ Compressibility Effects on Large Structures in Free Shear Flows,” Phys. Fluids A4,1251-1258, 1992.
14. Swithenbank, J. and Chigier, N. A., “ Vortex Mixing for Supersonic Combustion,” 12th Symp. on Combustion, 1153-1162, 1968.
15. Marble, F. E., Hendricks, G. J. and Zukoski, E. E., “ Progress Toward Shock Enhancement of Supersonic Combustion Processes,” AIAA Paper 87-1880, 1987.
16. Waitz, I. A., Marble, F. E. and Zukoski, E. E., “ An Investigation of a Contoured Wall Injector for Hypervelocity Mixing Augmentation,” AIAA Paper 91-2265, 1991.
17. Yang, J., Kubota, T. and Zukoski, E.E., “A Model for Characterization of a Vortex Pair Formed by Passage Over a Light-Gas Inhomogeneity,” J. Fluid Mech. Vol. 258, 217-244, 1994.
18. Northam, G. B., Greenberg, I. and Byington, C. S., “ Evaluation of Parallel Injector Configurations for Supersonic Combustion,” AIAA Paper 89-2525, 1989.
19. Northam, G. B., Capriotti, D. P., Byington, C. S. and Greenberg, I., “ Mach 2 and Mach 3 Mixing and Combustion in Scramjets,” AIAA Paper 91-2394, 1991.
20. Drummond, J. P., Carpenter, M. H., Riggins, D. W. and Adams, M. S., “ Mixing Enhancement in a Supersonic Combustor,” AIAA Paper 89-2794, 1989.
21. Stouffer, S. D., Vandsburger, U. and Northam, G. B., “ Comparison of Wall Mixing Concepts for Scramjet Combustors,” AIAA 94-0587, 1994.
22. Cox, S. K., Fuller, R.P., Schetz, J.A. and Walters, R. W.,” Vortical Interactions Generated by an Injector Array to Enhance Mixing in Supersonic Flow,” AIAA Paper 94-0708, 1994.
23. Fuller, R.P., Wu, P. K., Nejad, A. S. and Schetz, J. A.,” Fuel-Vortex Interactions for Enhanced Mixing in Supersonic How,” AIAA Paper 96-2661, 1996.
24. Scherrer, D., Montmayeur, N. and Ferrandon, O., “ Scramjet Injectors Calculation and Design,” AIAA Paper 93-5171, 1993.
25. Nishioka, M., “Control of Supersonic Mixing,” NAL SP-12, 39-42, 1990.
26. Nishioka, M. and Sunami, T., “Some Thoughts and Experiments on the Supersonic Mixing Enhancement”, J. Japan Society of Fluid Mech. Vol. 14, 377-389, 1995.
27. Sunami, T., Tokunaga, H. and Nishioka, M., “Control of Supersonic Mixing Using Streamwise Vortices,” NAL SP-28, 32-36, 1995.
28. Sunami, T. and Nishioka, M., “Breakdown Processes of Supersonic Streamwise Vortices in Spanwise-Row Configurations,” J. Japan Society of Fluid Mech. Vol. 16, 415-424, 1997.
29. Michael, N. W, Sunami, T., Sato, S. and Nishioka, M.,” Strut Injection in a Supersonic Combustor,” 7th symposium on Ram/Scramjets,Sendai, 247-252, 1997.
30. Chakravarthy, S. R. and Osher, S., “A New Class of High Accuracy TVD Schemes for Hyperbolic Conservation Laws,” AIAA Paper 85-0306, 1985.
31. Baldwin, B. S. and Lomax, H., “Thin Layer Approximation and Algebraic Model for Separated Turbulent Rows,” AIAA Paper 78-275, 1978.
32. Laufer, J. and McClellan, R., “Measurements of heat transfer from fine wires in supersonic flows,” J. Fluid Mech. Vol. 1,276-289, 1956.
33. Smits, A. J., Hayakawa, K. and Much, K. C, “Constant Temperature Hot-Wire Anemometer Practice in Supersonic Flows Part 1,” Experiments in Fluids 1,83-92, 1983. 15