Skip to main content
Log in

Visualization of shock-vortex interaction radiating acoustic waves

  • Published:
Journal of Visualization Aims and scope Submit manuscript

Abstract

Unsteady compressible flow fields past a wedge and a cone, evolved by propagation and interaction of shock waves, slip lines, and vortices, are studied by shadowgraphs and holographic interferograms taken during the shock tube experiment. The supplementary numerical calculation also presented time-accurate solution of the shock wave physics which was essential to recognize the similarity and dissimilarity between the wedge and the conical flows. The decelerated shock detained by the vortex interacts with the small vortexlets along the slip layer, producing diverging acoustics: this phenomenon is more distinct in the case of wedge flow for a given shock Mach number. The decelerated shock penetrated through the vortex core constitutes a transmitted shock, which eventually merges with the diaphragm shock that bridges the vortex pair/vortex ring. This phenomenon became remarkably salient in the case of conical flow.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Similar content being viewed by others

References

  • Chang, K. S. and Kim, J. K., Numerical Investigation of Inviscid Shock Wave Dynamics in an Expansion Tube, Shock Waves, 5 (1995), 33–45.

    Article  MATH  Google Scholar 

  • Chang, S. M. and Chang, K. S., Shock Wave Scattering Phenomena Behind a Finite Wedge, Proceeding of 5th Asian Symposium of Visualization 1998(Puspiptek Serpong, Indonesia), (1999-3), 47–52.

  • Dosanjh, D. S. and Weeks, T. M., Interaction of a Starting Vortex as well as a Vortex Street with a Travelling Shock Wave, AIAA, 3 (1965), 216–223.

    Article  MATH  Google Scholar 

  • Ellzey, J. L., Henneke, M. R. and Picone, J. M. and Oran, E. S., The Interaction of a Shock with a Vortex: Shock Distortion and the Production of Acoustic Waves, Physics of Fluids, 7 (1995), 172–184.

    Article  MathSciNet  Google Scholar 

  • Hiller, R., Computation of Shock Wave Diffraction at a Ninety Degree Convex Edge, Shock Waves, 1 (1991), 135–144.

    Article  Google Scholar 

  • Mayinger, F., Fundamentals of Holography and Holographic Interferometry in Optical Measurement — Techniques and Applications (Editor: Mayinger, F.), (1994), 51–73, Springer-Verlag.

  • Meadows, K. R., Kumar, A. and Hussaini, M. Y., Computational Study on the Interaction Between a Vortex and a Shock Wave, AIAA, 29 (1991), 174–179.

    Article  Google Scholar 

  • Schardin, H., High Frequency Cinematography in the Shock Tube, Journal of Photo Science, 5 (1957), 19–26; see also Van Dyke, An Album of Fluid Motion, (1982), Parabolic Press, Stanford, California.

    Google Scholar 

  • Sivier, S., Loth, E., Baum, J. and Lohner, R., Vorticity Produced by Shock Wave Diffraction, Shock Waves, 2 (1992), 31–41.

    Article  Google Scholar 

  • Weeks, T. M. and Dosanjh, D. S., Sound Generation by Shock-Vortex Interaction, AIAA, 5 (1967), 660–669.

    Article  Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Additional information

Author Profile Se-Myong Chang: He earned his Ph.D. degree from Korea Advanced Institute of Science and Technology (KAIST) in 2000 under the supervision of Prof. Keun-Shik Chang. He now works as Brain-Korea-21 Post-doctoral Fellow at Seoul National University. His research fields are shock-vortex interaction, computational aero-acoustics and experiment of high-speed flow.

Keun-Shik Chang: He finished his academic discipline of Ph.D. at the University of California, Berkeley in 1977, and NRC Research Associateship at NASA-Ames Research Center in 1978. He has since served as a professor of Department of Aerospace Engineering in Korea Advanced Institute of Science and Technology (KAIST). He is the founder of Korean Society of Computational Fluids Engineering (KSCFE). His research interests are in engineering flow computation and shock wave experiment. He has published hundredsome international journal and conference papers.

Rights and permissions

Reprints and permissions

About this article

Cite this article

Chang, S.M., Chang, K.S. Visualization of shock-vortex interaction radiating acoustic waves. J Vis 3, 221–228 (2000). https://doi.org/10.1007/BF03181844

Download citation

  • Received:

  • Revised:

  • Issue Date:

  • DOI: https://doi.org/10.1007/BF03181844

Keywords

Navigation