Deriving features of reacting hypersonic flow from gradients at a curved shock

5th AIAA Theoretical Fluid Mechanics Conference

Volumn , Issue , 2008, Pages

  Hornung, H G ^a  

^a CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CURVED SHOCK; EXOTHERMIC CHEMICAL REACTION; FLOW VARIABLE; FREE STREAM; HIGHER ORDER; JUMP RELATIONS; NUMERICAL COMPUTATIONS; NUMERICAL SCHEME; SHOCK-FITTING;

FLUID MECHANICS;

CONTACTS (FLUID MECHANICS);

EID: 78049262051     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (22)

1. Hayes, W. D. and Probstein, R. F., Hypersonic Flow Theory, Academic Press, 1959.
2. Oswatitsch, K., Gasdynamik, Springer-Verlag, 1952.
3. Lighthill, M. J., "The flow behind a stationary shock, " Philosophical Magazine, Vol. 40, 1949, pp. 214-220.
4. Munk, M. M. and Prim, R. C., "Surface-pressure gradient and shock-front curvature at the edge of a plane ogive with attached shock front, " Journal of the Aeronautical Sciences, Vol. 15, 1948, pp. 691-695.
5. Gerber, N. and Bartos, J. M., "Calculation of flow-variable gradients behind curved shock waves, " Journal of the Aerospace Sciences, Vol. 27, 1960, pp. 958-959.
6. Chen, P. J. and Gurtin, M. J., "Growth and decay of one-dimensional shock waves in fluids with internal state variables, " Physics of Fluids, Vol. 14, 1971, pp. 1091-1094.
7. Gilinskii, S. M. and Chernyi, G. G., "Supersonic flow of combustible gas mixture past sphere with account for ignition delay time, " Fluid Dynamics, Vol. 3, 1968, pp. 12-19.
8. Clarke, J. F., Non-equilibrium flows Part II, edited by P. P. Wegener, Marcel Dekker, 1969.
9. Mölder, S., "Reflection of curved shock waves in steady supersonic flow, " CASI Transactions, Vol. 4, 1971, pp. 73-80.
10. Mölder, S., "Polar streamline directions at the triple point of Mach interaction of shock waves, " CASI Transactions, Vol. 5, 1972, pp. 88-89.
11. Hornung, H. G., "Non-equilibrium ideal-gas dissociation after a curved shock wave, " Journal of Fluid Mechanics, Vol. 74, 1976, pp. 143-159.
12. Hornung, H. G., "Gradients at a curved shock in reacting flow, " Shock Waves, Vol. 8, 1998, pp. 11-21.
13. Kaneshige, M. J. and Hornung, H. G., "Erratum: Gradients at a curved shock in reacting flow, " Shock Waves, Vol. 9, 1999, pp. 219-220.
14. Hornung, H. G., "Features of the density field of dissociating hypersonic flows, " Zeitschrift für angewandte Mathematik und Mechanik, Vol. 80, 2000, pp. 755-763.
15. Quirk, J. J., "A computational facility (for CFD modelling), " VKI 29th CFD Lecture Series, ISSN 0377-8312, von Karman Institute, Brussels, 1998.
16. Billig, F. S., "Shock wave shapes around spherical- and cylindrical-nosed bodies, " Journal of Spacecraft and Rockets, Vol. 4, 1967, pp. 822-823.
17. Candler, G. V., "On the computation of shock shapes in nonequilibrium hypersonic flows, " 27th Areospace Sciences Meeting, AIAA, Reno, NV, 1989.
18. Klomfass, A., Hyperschallströmungen im thermodynamischen Nichtgleichgewicht, Dipl.-Ing. thesis, Technical University of Aachen, 1995.
19. Hornung, H. G. and Smith, G. H., "The influence of relaxation on shock detachment, " Journal of Fluid Mechanics, Vol. 93, 1979, pp. 225-239.
20. Hornung, H. G. and Leyva, I. A., "Sonic line and shock detachment in hypervelocity cone flow, " Transsonicum IV, edited by H. Sobieczky, Kluwer Academic Publishers, 2003, pp. 363-368.
21. Bondar, Y. A., Khotyanovsky, D. V., Kudryavtsev, A. N., Shoev, G. V., and Ivanov, M. S., "Viscosity effects on Mach reflection in steady flows, " AIAA paper 2008-1187, Jan. 2008.
22. Hornung, H. G. and Lemieux, P., "Shock layer instability near the Newtonian limit of hypersonic flows, " Physics of Fluids, Vol. 13, 2001, pp. 2394-2402.