Formation and stability of near chapman-jouguet standing oblique detonation waves

AIAA Journal

Volumn 43, Issue 7, 2005, Pages 1591-1604

  Fusina, Giovanni ^a,d   Sislian, Jean P ^b,e   Parent, Bernard ^c,f  

^a DEFENCE RESEARCH AND DEVELOPMENT CANADA   (Canada)

^b UNIVERSITY OF TORONTO   (Canada)

^c Seoul National University   (South Korea)

^d Institute for Aerospace Studies   (Canada)

^e Department of Aerospace Engineering ^*

^f UNIVERSITY OF TORONTO   (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

AIR; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; DETONATION; ENTROPY; FLUID DYNAMICS; GIBBS FREE ENERGY; HYDROGEN; HYPERSONIC FLOW; NAVIER STOKES EQUATIONS; POLYNOMIALS; SUPERSONIC FLOW; VECTORS;

NONEQUILIBRIUM HYDROGEN-AIR COMBUSTION MODEL; OBLIQUE DETONATION WAVES (ODW); QUASIHYPERBOLIC SYSTEMS; STABLE STRUCTURES;

SHOCK WAVES;

EID: 22544483829     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.9128     Document Type: Article

References (38)

1. Nettleton, M., Gaseous Detonations: Their Nature and Control, Chapman and Hall, Bristol, England, U.K., 1987.
2. Lee, J.,"Initiation of Gaseous Detonation," Annual Review of Physical Chemistry, vol. 28, no. 75, 1977, pp. 75-104.
3. Li, C., Kailasanath, K., and Oran, E.,"Detonation Structures Behind Oblique Shocks," Physics of Fluids, vol. 6, no. 4, 1994, pp. 1600-1611.
4. Kailasanath, K., Oran, E., Boris, J., and Young, T.,"Determination of Detonation Cell Size and the Role of Transverse Waves in Two-Dimensional Detonations," Combustion and Flame, vol. 61, Sept. 1985, pp. 199-209.
5. Shepherd, J., Moen, I., Murray, S., and Thibault, P.,"Analyses of the Cellular Structure of Detonations," 21st International Symposium on Combustion, Combustion Inst., Pittsburgh, PA, 1988, pp. 1649-1658.
6. Lehr, H. F.,"Experiments in Shock-Induced Combustion," Astronautica Acta, vol. 17, Nos. 4-5, 1972, pp. 589-597.
7. Choi, J. Y., Jeung, I. S., and Yoon, Y.,"Computational Fluid Dynamics Algorithms for Unsteady Shock-Induced Combustion, Part 1: Validation," AIAA Journal, vol. 38, no. 7, 2000, pp. 1179-1187.
8. Matsuo, A., Fujii, K., and Fujiwara, T.,"Flow Features of Shock-Induced Combustion Around Projectile Travelling at Hypervelocities,"AIAA Journal, vol. 33, no. 8, 1995, pp. 1056-1062.
9. Wilson, G. J., and Sussman, M. A.,"Computation of Unsteady Shock-Induced Combustion Using Logarithmic Species Conservation Equations, " AIAA Journal, vol. 31, no. 2, 1993, pp. 294-301.
10. McClinton, C. R., Raush, D. R., Sitz, J., and Reukauf, P.,"Hyper-X Program Status," AIAA Paper 2001-1910, April 2001.
11. Dudebout, R., Sislian, J. P., and Oppitz, R.,"Numerical Simulation of Hypersonic Shock-Induced Combustion Ramjets," Journal of Propulsion and Power, vol. 14, no. 6, 1998, pp. 869-879.
12. Papalexandris, M. V.,"A Numerical Study of Wedge-Induced Detonations," Combustion and Flame, vol. 120, no. 4, 2000, pp. 526-538.
13. Viguier, C., Figueira da Silva, L., Desbordes, D., and Deshaies, B.,"Onset of Oblique Detonation Waves: Comparison Between Experimental and Numerical Results for Hydrogen-Air Mixtures," 26th International Symposium on Combustion, Combustion Inst., Pittsburgh, PA, 1997, pp. 3023-3031.
14. Dudebout, R.,"Numerical Simulation of Hypersonic Shock-Induced Combustion Ramjet Flowfields," Ph.D. Dissertation, Graduate Dept. of Aerospace Science and Engineering, Univ. of Toronto, Toronto, 1995.
15. Fusina, G.,"Numerical Investigation of Oblique Detonation Waves for a Shcramjet Combustor," Ph.D. Dissertation, Graduate Dept. of Aerospace Science and Engineering, Univ. of Toronto, Toronto, 2003,
16. Powers, J., and Gonthier, K.,"Reaction Zone Structure for Strong, Weak Overdriven and Weak Underdriven Oblique Detonations," Physics of Fluids A, vol. 4, no. 9, 1992, pp. 2082-2089.
17. Grismer, M., and Powers, J.,"Numerical Predictions of Oblique Detonation Stability Boundaries," Shock Waves, vol. 6, no. 3, 1996, pp. 147-156.
18. Yee, H. C., and Shinn, J. L.,"Semi-Implicit and Fully Implicit Shock-Capturing Methods for Nonequilibrium Flows," AIAA Journal, vol. 27, no. 3, 1989, pp. 299-307.
19. Singh, D., Ahuja, J., and Carpenter, M.,"Numerical Simulation of Shock-Induced Combustion/Detonation," Computing Systems in Engineering, vol. 3, Nos. 1-4, 1992, pp. 201-215.
20. Vlasenko, V., and Sabelnikov, V.,"Numerical Solution of Inviscid Flows with Hydrogen Combustion After Shock Waves and in Detonation Waves," AIAA Paper 94-3177, June 1994.
21. Thaker, A. A., and Chelliah, H. K.,"Numerical Prediction of Oblique Detonation Wave Structures Using Detailed and Reduced Reaction Mechanisms, " Combustion Theory Modelling, vol. 1, no. 4, 1997, pp. 347-376.
22. Morris, C. I., Kamel, M. R., and Hanson, R. K.,"Expansion Tube Investigation of Ram Accelerator Projectile Flowfields," AIAA Paper 96-2680, July 1996.
23. Choi, J., Jeung, L., and Yoon, Y.,"Numerical Study of Structure and Stability of Oblique Detonation Waves over a 40° Wedge," 27th International Symposium on Combustion, Combustion Inst., Pittsburgh, PA, 1998.
24. Li, C., Kailasanath, K., and Oran, E.,"Effects of Boundary Layers on Oblique-Detonation Structures," AIAA Paper 93-0450, Jan. 1993.
25. Viviand, H.,"Conservative Forms of Gas Dynamics Equations," La Recherche Aérospatiale, no. 1, Jan. 1974, pp. 65-68.
26. Vinokur, M.,"Conservative Equations of Gas-Dynamics in Curvilinear Coordinate Systems," Journal of Computational Physics, vol. 14, Feb. 1974, pp. 105-125.
27. Parent, B.,"Computational Study of Fuel Injection in a Shcramjet Inlet," Ph.D. Dissertation, Graduate Dept. of Aerospace Science and Engineering, Univ. of Toronto, Toronto, 2002.
28. McBride, B. J., and Reno, M. A.,"Coefficients for Calculating Thermodynamic and Transport Properties of Individual Species," NASA TM 4513, Oct. 1993.
29. Chase, M. W.,"JANAF Thermochemical Tables, 3rd ed., Parts I and II," Journal of Physical and Chemical Reference Data,vol. 14, Suppl. 1, 1985.
30. Dixon-Lewis, G.,"Computer Modelling of Combustor Reactions," Combustion Chemistry, edited by W. C. Gardiner, Springer-Verlag, New York, 1984, Chap. 2, pp. 21-125.
31. Anderson, J. D., Hypersonic and High-Temperature Gas Dynamics, McGraw-Hill, New York, 1989.
32. 1,2-Hydrocarbon Fuels," 22nd International Symposium on Combustion, Combustion Inst., Pittsburgh, PA, 1988, pp. 1683-1693.
33. Parent, B., and Sislian, J. P.,"The Use of Domain Decomposition in Accelerating the Convergence of Quasihyperbolic Systems," Journal of Computational Physics, vol. 179, no. 1, 2002, pp. 140-169.
34. Roe, P. L.,"Approximate Riemann Solvers, Parameter Vectors, and Difference Schemes," Journal of Computational Physics, vol. 43, no. 2, 1981, pp. 357-372.
35. Jenssen, C. B., and Weinerfelt, P. A.,"Parallel Implicit Time-Accurate Navier-Stokes Computations Using Coarse Grid Correction," AIAA Journal, vol. 36, no. 6, 1998, pp. 946-951.
36. Holden, M. S., and Moselle, J. R.,"Theoretical and Experimental Studies of the Shock Wave-Boundary Layer Interaction on Compression Surfaces in Hypersonic Flow," Aerospace Research Lab., Technical Rept. ARL 70-0002, Wright-Patterson AFB, OH, 1970.
37. Jachimowski, C. J.,"An Analytical Study of the Hydrogen-Air Reaction Mechanism with Application to Scramjet Combustion," NASA TP 2791, 1988.
38. Strauss, W. A., and Scott, J. N.,"Experimental Investigation of the Detonation Properties of Hydrogen-Oxygen and Hydrogen-Nitric Oxide Mixtures at Initial Pressures of up to 40 Atmospheres," Combustion and Flame, vol. 19, Aug.-Dec. 1972, pp. 141-143.