Influence of formation processes on oblique detonation wave stabilization

Journal of Propulsion and Power

Volumn 12, Issue 3, 1996, Pages 509-517

  Ghorbanian, K ^a,b,c   Sterling, J D ^a,c,d  

^a Advanced Projects Research Inc   (United States)

^b CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

^c AIAA ^*

^d CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION; FLOW INTERACTIONS; GEOMETRY; SHOCK WAVES; STABILIZATION;

OBLIQUE DETONATION WAVE; SUPERSONIC REACTIVE FLOW; VARIABLE DOUBLE RAMP GEOMETRY;

SUPERSONIC FLOW;

EID: 0030141442     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/3.24064     Document Type: Article

References (32)

1. Dunlap, R., Brehm, R. L., and Nicholls, J. A., "A Preliminary Study of the Application of Steady-State Detonative Combustion to a Reaction Engine," Jet Propulsion, Vol. 28, No. 7, 1958, pp. 451-456.
2. Rubins, P. M., and Bauer, R. C., "A Hypersonic Ramjet Analysis with Premixed Fuel Combustion," AIAA Paper 66-648, June 1966.
3. Jachimowski, C. J., "An Analytical Study of the Hydrogen-Air Reaction Mechanism with Application to Scramjet Combustion," NASA TP-2791, Feb. 1988.
4. Heiser, W. H., and Pratt, D. T., Hypersonic Airbreathing Propulsion, AIAA Education Series, AIAA, Washington, DC, 1994.
5. Gross, R. A., and Chinitz, W., "A Study of Supersonic Combustion," Journal of the Aerospace Sciences, Vol. 27, No. 7, 1960, pp. 517-524.
6. Rubins, P. M., and Bauer, R. C., "Review of Shock-Induced Supersonic Combustion Research and Hypersonic Applications," Journal of Propulsion and Power, Vol. 10, No. 5, 1994, pp. 593-601.
7. Chernyi, G. G., "Problems of Hydrodynamics and Continuum Mechanics," Supersonic Flow Past Bodies with Formation of Detonation and Combustion Fronts, Society for Industrial and Applied Mathematics, Philadelphia, PA, 1969, pp. 145-169.
8. Ruegg, F. W., and Dorsey, W. W., "A Missile Technique for the Study of Detonation Waves," Journal of Research of the National Bureau of Standards, Vol. 66C, No. 1, 1962, pp. 51-58.
9. Behrens, H., Struth, W., and Wecken, F., "Studies of Hypervelocity Firings into Mixtures of Hydrogen with Air or with Oxygen," 10th Symposium (International) on Combustion, The Combustion Inst., Pittsburgh, PA, 1965, pp. 245-252.
10. McVey, J. B., and Toong, T. Y., "Mechanism of Instabilities of Exothermic Hypersonic Blunt-Body Flows," Combustion Science and Technology, Vol. 3, No. 2, 1971, pp. 63-76.
11. Alpert, R. L., and Toong, T. Y., "Periodicity in Exothermic Hypersonic Flows About Blunt Projectiles," Astronautica Acta, Vol. 17, Nos. 4 and 5, 1972, pp. 539-560.
12. Lehr, H. F., "Experiments on Shock-Induced Combustion," Astronautica Acta, Vol. 17, Nos. 4 and 5, 1972, pp. 589-597.
13. Dabora, E. K., Desbordes, D., Guerraud, C., and Wagner, H. G., "Oblique Detonations at Hypersonic Velocities," Dynamics of Detonations and Explosions: Detonations, Vol. 133, Progress in Astronautics and Aeronautics, AIAA, Washington, DC, 1991, pp. 187-204.
14. Liu, J. C., Liou, J. J., Sichel, M., Kaufmann, C. W., and Nicholls, J. A., "Diffraction and Transmission of a Detonation into a Bounding Explosive Layer," 21st Symposium (International) on Combustion, The Combustion Inst., Pittsburgh, PA, 1987, pp. 1639-1647.
15. Pratt, D. T., Humphrey, J. W., and Glenn, D. E., "Morphology of Standing Oblique Detonation Waves," Journal of Propulsion and Power, Vol. 7, No. 5, 1991, pp. 837-845.
16. Shepherd, J. E., "Detonation Waves and Propulsion," Combustion in High-Speed Flows, 1994, pp. 373-420.
17. Yungster, S., and Rabinowitz, M. J., "Computation of Shock-Induced Combustion Using a Detailed Methane-Air Mechanism," Journal of Propulsion and Power, Vol. 10, No. 5, 1994, pp. 609-617.
18. Rom, J., and Avital, G., "The External Propulsion Accelerator: Scramjet Thrust Without Interaction with Accelerator Barrel," AIAA Paper 92-3717, June 1992.
19. Grismer, M. J., and Powers, J. M., "Calculations for Steady Propagations of a Generic Ram Accelerator Configuration," Journal of Propulsion and Power, Vol. 11, No. 1, 1995, pp. 105-111.
20. Chinitz, W., Bakos, R. J., and Erdos, J. I., "Experimental Requirements for the Study of Shock-Induced Premixed Combustion," AIAA Paper 94-3099, June 1994.
21. Figueira da Silva, L. F., Deshaies, B., and Champion, M., "A Numerical Study of Ignition Within Hydrogen-Air Supersonic Boundary Layers," AIAA Journal, Vol. 31, No. 5, 1993, pp. 884-890.
22. Hertzberg, A., Bruckner, A. P., and Bogdanoff, D. W., "Ram Accelerator: A New Chemical Method for Accelerating Projectiles to Ultrahigh Velocities," AIAA Journal, Vol. 26, No. 2, 1988, pp. 195-203.
23. Pratt, D. T., "Calculation of Chemically Reacting Flows with Complex Chemistry," Studies in Convection, edited by B. E. Launder, Vol. II, Academic, New York, 1977.
24. Ghorbanian, K., "Superdetonative Flow of Gaseous Propellant Mixtures over Sphere-Cone Bodies," Ph.D. Dissertation, Univ. of Washington, Seattle, WA, March 1993.
25. Williams, F. A., Combustion Theory, Addison-Wesley, Reading, MA, 1988.
26. Ghorbanian, K., and Sterling, J. D., "Detonation Initiation on a Wedge in a Supersonic Reacting Flow," AIAA Paper 95-2563, July 1995.
27. Ghorbanian, K., and Pratt, D. T., "An Estimate of the Doomed Propellant Fraction for a Superdetonative Ram Accelerator," AIAA Paper 93-0359, Jan. 1993.
28. Li, C., Kailasanath, K., and Oran, E. S., "Detonation Structures Behind Oblique Shocks," Physics of Fluids, Vol. 6, April 1994, pp. 1600-1611.
29. Lefebvre, M. H., and Fujiwara, T., "Numerical Modeling of Combustion Processes Induced by a Supersonic Conical Blunt Body," Combustion and Flame, No. 100, 1995, pp. 85-93.
30. Ashford, S. A., and Emanuel, G., "Wave Angle for Oblique Detonation Waves," Shock Waves, Vol. 4, No. 3, 1994, pp. 327-329.
31. Chernyi, G. G., Self-Similar Problems in the Flow of Combustible Mixtures of Gases Past Bodies, Izv. Akad. Nauk. SSSR Mehkanika Zhidkosti i Gaza, No. 6, 1966, pp. 10-24.
32. Desbordes, D., Hamada, L., and Guerraud, C., "Supersonic H2-Air Combustions Behind Oblique Shock Waves," Shock Waves, Vol. 4, No. 6, 1995, pp. 339-345.