Numerical study of hypersonic reacting boundary layer transition on cones

Physics of Fluids

Volumn 10, Issue 10, 1998, Pages 2676-2685

  Johnson, Heath B ^a   Seipp, Trevor G ^a   Candler, Graham V ^a  

^a University of Minnesota   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0006092396     PISSN: 10706631     EISSN: None     Source Type: Journal    
DOI: 10.1063/1.869781     Document Type: Article

References (25)

1. M. R. Malik and E. C. Anderson, "Real gas effects on hypersonic boundary-layer stability," Phys. Fluids A 3, 803 (1991).
2. G. K. Stuckert and H. L. Reed, "Linear disturbances in hypersonic, chemically reacting shock layers," AIAA J. 32, 1384 (1994).
3. M. L. Hudson, N. Chokani, and G. V. Candler, "Linear stability of hypersonic flow in thermochemical nonequilibrium," AIAA J. 35, 958 (1997).
4. P. D. Germain and H. G. Hornung, "Transition on a slender cone in hypervelocity flow," Exp. Fluids 22, 183 (1997).
5. P. H. Adam and H. G. Hornung, "Enthalpy effects on hypervelocity boundary-layer transition: Ground test and flight data," J. Spacecr. Rockets 34, 614 (1997).
6. P. Martin and G. V. Candler, "Effect of chemical reactions on decaying Isotropic turbulence," Phys. Fluids 10, 1715 (1998); Also AIAA Paper No. 96-2060, June 1996.
7. P. Martin and G. V. Candler, "Effect of chemical reactions on decaying Isotropic turbulence," Phys. Fluids 10, 1715 (1998); Also AIAA Paper No. 96-2060, June 1996.
8. G. V. Candler and R. W. MacCormack, "The computation of hypersonic ionized flows in chemical and thermal nonequilibrium," J. Thermophys. Heat Transfer 5, 266 (1991).
9. S. G. Rock, G. V. Candler, and H. G. Hornung, "Analysis of thermochemical nonequilibrium models for carbon dioxide flows," AIAA J. 31, 2255 (1993).
10. C. Park, J. T. Howe, R. L. Jaffe, and G. V. Candler, "Review of chemical-kinetic problems of future NASA missions, H; Mars entries," J. Thermophys. Heat Transfer 8, 9 (1994).
11. R. W. MacCormack and G. V. Candler, "The solution of the Navier-Stokes equations using Gauss-Seidel line relaxation," Comput. Fluids 17, 135 (1989).
12. G. V. Candler, M. J. Wright, and J. D. McDonald, "Data-parallel lower-upper relaxation method for reacting flows," AIAA J. 32, 1280 (1994).
13. E. Reshotko, "Remark on engineering aspects of transition," in Transition and Turbulence (Academic, New York, 1981), p. 147.
14. L. M. Mack, "Linear stability theory and the problem of supersonic boundary-layer transition," AIAA J. 13, 278 (1975).
15. C. L. Chang, M. R. Malik, G. Erlebacher, and M. Y. Hussaini, "Compressible stability of growing boundary layers using parabolized stability equations," AIAA Paper 91-1636, June 1991.
16. M. L. Hudson, "Linear stability theory of hypersonic, chemically reacting viscous flow," Ph.D. thesis, North Carolina State University, Feb. 1996.
17. G. K. Stuckert, "Linear stability theory of hypersonic, chemically reacting viscous flow," Ph.D. thesis, Arizona State University, Dec. 1991.
18. C. L. Chang, M. R. Malik, and M. Y. Hussaini, "Effects of shock on the stability of hypersonic boundary layers," AIAA Paper 90-1448, June 1990.
19. M. R. Malik, "Numerical methods for hypersonic boundary layer stability," J. Comput. Phys. 86, 376 (1990).
20. N. A. Jaffe, T. T. Okamura, and A. M. O. Smith, "Determination of spatial amplification factors and their application to predicting transition," AIAA J. 8, 301 (1970).
21. F.-J. Chen, M. R. Malik, and I. E. Beckwith, "Boundary-layer transition on a cone and flat plate at mach 3.5," AIAA J. 27, 687 (1989).
22. E. R. G. Eckert, "Engineering relations for friction and heat transfer to surfaces in high velocity flow," J. Aeronaut. Sci. 22, 585 (1955).
23. H. L. Reed, R. L. Kimmel, S. Schneider, and D. Arnal, "Drag prediction and transition in hypersonic flow," AIAA Paper 97-1818, June 1997.
24. R. L. Kimmel, S. N. Schwoerke, and M. A. Klein, "Three-dimensional hypersonic laminar boundary layer computations for transonic experiment design," AIAA Paper 96-2080, Jan. 1996.
25. P. Germain, "The boundary layer on a sharp cone in high-enthalpy flow," Ph.D. thesis. Graduate Aeronautical Laboratories, California Institute of Technology, 1994.