Experimental investigations of compressible vortex loops

Article English OPEN
Zare-Behtash, H.; Kontis, K.; Gongora-Orozco, N.;
  • Publisher: American Institute of Physics

The present study involves the shock wave and consequent vortex loop generated when a shock tube with various nozzle geometries is employed. It aims to provide quantitative and qualitative insight into the physics of these compressible phenomena. The geometries included... View more
  • References (13)
    13 references, page 1 of 2

    1 Love, E. S., Grigsby, C. E., Lee, L. P., Woodling, M. J., “Experimental and theoretical studies of axisymmetric free jets,” NASA technical report, NASA TR-R-6, (1959).

    2 Kweon, Y. H., Miyazato, Y., Aoki, T., Kim, H. D., “Experimental investigation of nozzle exit reflector effect on supersonic jet,” Shock Waves 15, pp. 229-239, (2006).

    3 Gutmark, E.J., Grinstein, F.F., “Flow control with noncircular jets,” Annual Review of Fluid Mechanics 31, pp. 239-272, (1999).

    4 Grinstein, F. F., Gutmark, E., Parr, T., “Near field dynamics of subsonic free square jets. A computational and experimental study,” Physics of Fluids 7, pp. 1483-1497, (1995).

    5 Saffman, P. G., “Dynamics of vorticity,” Journal of Fluid Mechanics 106, pp. 49-58, (1981).

    6 Shepherd, J. E., Schultz, E., Akbar, R., “Detonation diffraction,” In: Ball, G., Hillier, R., Roberts, G., (eds.) Proceedings of the 22nd International Symposium on Shock Waves 1, pp. 41-48, (2000).

    7 Pantow, E.G., Fischer, M., Kratzel, T., “Decoupling and recoupling of detonation waves associated with sudden expansion,” Shock Waves 6, pp. 131-137, (1996).

    8 Papalexandris, M.V., Thomas, J.F., Jacobs, C., Deledicque, V., “Structural characteristics of detonation expansion from a small channel to a larger one,” Proceedings of the Combustion Institute, pp. 2407-2414, (2007).

    9 Ohyagi, S., Obara, T., Hoshi, S., Cai, P., Yoshihashi, T., “Diffraction and re-initiation of detonations behind a backward-facing step,” Shock Waves 12, pp. 221-226, (2002).

    10 Glaser, A.J., Caldwell, N., Gutmark, E., Hoke, J., Bradley, R., Schauer, F., “Effects of tube and ejector geometry on the performance of pulse detonation engine driven ejectors,” 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, California, AIAA 2006- 4790 (2006).

  • Metrics
Share - Bookmark