Shock/shock interaction experiments in the high enthalpy shock tunnel Göttingen

36th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1998, Pages

  Carl, M ^a   Hannemann, V ^a   Eitelberg, G ^a  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; CYLINDERS (SHAPES); ENTHALPY; FLUID DYNAMICS; HOLOGRAPHIC INTERFEROMETRY; THERMOCOUPLES;

BURST PRESSURES; DISSOCIATION REACTIONS; FLOW BEHAVIOURS; FREESTREAM CONDITIONS; HEAT TRANSFER RATE; HIGH ENTHALPY SHOCK TUNNEL; HOLOGRAPHIC INTERFEROGRAMS; SCHLIEREN PICTURE;

HEAT TRANSFER;

EID: 84982318540     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (30)

1. Hannemann, V., "Numerische Simulation von Stoß-Stoß-Wechselwirkungen unter Berūcksichtigung von chemischen und thermischen Nichtgleichgewichtseffekten," DLR-FB 97-07, DLR Inst. f. Strömungsraech., Göttingen, Germany, 1997.
2. Edney, B., "Anomalous Heat Transfer and Pressure Distributions on Blunt Bodies at Hypersonic Speeds in the Presence of an Impinging Shock," FFA Report 115, Aeronautical Research Institute of Sweden, 1968.
3. Brueck, S., "Investigation of Shock-Shock Interactiona in Hypersonic Reentry Flows," 20th International Symposium on Shock Waves, edited by H. Hornung, GALGIT, World Scientific Press, Pasadena, CA, 1996.
4. Vincenti, W. G. and Tkruger, C. H., Introduction to Physical Gas Dynamics, J. Wiley and Sons, 1965.
5. Wen, C.-Y. and Hornung, H. G., "Non-equilibrium dissociating flow over spheres," J. Fluid Mech., Vol. 299, 1995, pp. 389-405.
6. Lind, C. A., A computational analysis of the unsteady phenomena associated with a hypersonic type IV shock interaction, Ph.D. thesis, University of Maryland College Park, USA, 1994.
7. Lind, C. A. and Lewis, M. J., "Unsteady Effects of a Hypersonic Type IV Shock Interaction," AIAA paper, No. 94-2945, 1994, AIAA/SAE/ASME/ASEE 30th Joint Propulsion Conf. and Exhibit.
8. Sanderson, S. R., Shock wave interaction in hypervelocity flow, Ph.D. thesis, GALCIT Caltech, Pasadena, USA, 1995.
9. Furumoto, G. H. and Zhong, X., "Numerical simulation of viscous unsteady type iv shock/shock interaction with thermochemical nonequilibrium," AIAA Paper, No. 97-0982, 1997, 35th AIAA Aerospace Sciences Meeting.
10. Krek, R. M. and Eitelberg, G., "Classical Characterisation of the HEG (Nozzle, Freestream Flow Field)," DLR-IB 223-94 A 50, DLR Inst. f. Strömungsmech., Göttingen, Germany, 1994.
11. Hannemann, K., Krek, R., and Eitelberg, G., "Latest calibration results of the HEG contoured nozzle," 20th International Symposium on Shock Waves, edited by H. Hornung, GALCIT, World Scientific Press, Pasadena, CA, 1997.
12. Chue, R. S. M. and Eitelberg, G., "Reflected shock/boundary layer interaction in the reservoir region of the HEG shock tunnel," Symposium on Shock Waves, Tokyo, Japan, 1997.
13. Chue, R. S. M., Eitelberg, G., and Carl, M., "Transient starting process in the HEG nozzle," 21th International Symposium on Shock Waves, Australia, 1997.
14. Chue, R. S. M. and Eitelberg, G., "Studies of the Transient Flows in High Enthalpy Shock Tunnels," Exp. in Fluids, to be published.
15. Hakenesch, P., Carl, M., Kastell, D., and Eitelberg, G., "Cylinder Experiments in the High Enthalpy Tunnel HEG. Part I," DLR-IB 223-96 A 06, DLR Inst. f. Strömungsmech., Göttingen, Germany, 1996.
16. Kastell, D., "Aerodynamik eines stumpfen Kegels in reagierender Überschallströmung," DLR-FB 97-06, DLR Inst, f. Strömungsmech., Göttingen, Germany, 1997.
17. Kastell, D., Carl, M., and Eitelberg, G., "Phase Step Holographic Interferometry applied to Hypervelocity, Nonequilibrium Cylinder Flow," Experiments in Fluids, Vol. 22, 1996, pp. 57-66.
18. Park, C., Nonequilibrium Hypersonic Aerothermodynam-ics, John Wiley and Sons, 1990.
19. Marrone, P. V. and Tveanor, C. E., "Chemical Relaxation with Preferential Dissociation from Excited Vibrational Levels," Physics of Fluids, Vol. 6, No. 9, 1963, pp. 1215-1220.
20. Klomfass, A., Hyperschallströmungen im thermodynamis-chen Nichtgleichgewicht, Ph.D. thesis, RWTH Aachen, Ger-many, 1994.
21. Gupta, Y. and Thomson, L., "A review of reaction rates and thermodynamic and transport properties for an 11-species air model for chemical and thermal nonequilibrium calculations to 30000K," NASA Reference Publications, No. 1232, 1989.
22. Zipperer, L. and Herning, F., "Beitrag zur Berechnung der Zähigkeit technischer Gasgemische aus den Zähigkeitswerten der Einzelbestandteile," Das Gas-und Wasserfach, Vol. 4, 1936, pp. 49-.
23. Klomfaß, A., Müller, S., and Ballmann, J., "Modelling of transport phenomena for the hypersonic stagnation point heat transfer problem." AIAA Paper, No. 93-5047, 1993.
24. Sonar, T., "On the design of an upwind scheme for compressible flow on general triangulations," Numerical Algorithms, Vol. 4, 1993, pp. 135-149.
25. Sonar, T., Hannemann, V., and Hempel, D., "Dynamic adaptivity and residual control in unsteady flow computation." Mathematical and Computer Modelling, Vol. 20, 1994, pp. 201-213.
26. Meister, A., "Zur zeitgenauen numerischen Simulation rei-bungsbehafteter kompŕessibłer turbulenter Strömungsfelder mit einer impliziten Finite-Volumen-Methode vom Box-Typ," DLR-FB 96-08, DLR Inst. f. Strömungsmech., Göttingen, Germany, 1996.
27. Barth, T. J. and Jesperson, D. C., "The design and ap--plication of upwind schemes on unstructured meshes," AIAA Paper, No. 89-0366, 1989.
28. Wada, Y. and Liou, M.-S., "A flux splitting scheme with high-resolution and robustness for discontinuities." ICOMP, No. 93-50, 1993.
29. Fay, J. A. and Riddell, F. R., "Theory of stagnation point heat transfer in dissociated air," J. Aeronautical Sciences, Vol. 25, No. 2, 1958, pp. 73-85.
30. Prabhu, R. K., "An Implementation of a Chemical and Thermal Nonequilibrium Flow Solver on Unstructured Meshes and Application to Blunt Bodies," NASA CR 194967, NASA Langley, 1994.