Skip to main content
Log in

Mach waves produced in the supersonic jet mixing layer by shock/vortex interaction

  • Original Article
  • Published:
Shock Waves Aims and scope Submit manuscript

Abstract

The noise emission of free jets has been extensively investigated for many decades. At subsonic jet velocities, coherent structures of the mixing layer move at subsonic speed and emit sound waves. Free jets blowing at supersonic speeds, however, can emit weak shock waves, called Mach waves. At supersonic speeds, two cases must be distinguished: the structures move either subsonically or supersonically relative to the inside and/or outside speed of sound. In the case of supersonic movement, the Mach waves exist inside as well as outside the jet. At subsonic speeds, no Mach waves appear. Although numerous theories have been established to find the origin of the Mach waves, to the authors’ best knowledge, the mechanism of the Mach wave formation has not yet been clearly explained. Recently another theory of Mach waves in supersonic jets was developed, as described herein, which outlines the causes for the Mach wave production and stability as well as their dynamics. The theory’s principle is that the Mach waves are initiated by vortices which move downstream at three speeds w, \({w}'\) and \({w}''\) inside of the mixing layer. These three types of vortices and Mach waves are described in a comprehensive manner by the theory and are called the “w-, \({w}'\)- and \({w}''\)-vortices” and “w-, \({w}'\)- and \({w}''\)-Mach waves,” respectively.

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.

Fig. 1
Fig. 2
Fig. 3
Fig. 4
Fig. 5
Fig. 6
Fig. 7
Fig. 8
Fig. 9
Fig. 10
Fig. 11
Fig. 12
Fig. 13
Fig. 14
Fig. 15
Fig. 16
Fig. 17
Fig. 18

Similar content being viewed by others

References

  1. Oertel, H.: Kinematik der Machwellen in Überschallstrahlen (kinematics of Mach waves in supersonic jets). ISL-Report R 112/78 (1978)

  2. Oertel, H.: Mach wave radiation of hot supersonic jets investigated by means of a shock tube and new optical techniques. In: Proceedings of the 12th International Symposium on Shock-Tubes and Waves, Jerusalem (1980)

  3. Oertel, H.: 33 years of research by means of shock tubes at the French-German Research Institute of Saint-Louis. In: Proceedings of the 14th International Symposium on Shock Tubes and Waves, Sydney, pp. 3–13 (1983)

  4. Tam, C.K.W.: Directional acoustic radiation from a supersonic jet generated by shear layer instability. J. Fluid Mech. 46, 757–768 (1971)

    Article  MATH  Google Scholar 

  5. Tam, C.K.W.: Supersonic jet noise generated by large scale disturbances. J. Sound Vib. 38(1), 51–79 (1975)

    Article  MATH  Google Scholar 

  6. Tam, C.K.W.: Supersonic jet noise. Annu. Rev. Fluid Mech. 27, 17–43 (1995)

    Article  Google Scholar 

  7. Tam, C.K.W.: Mach wave radiation from high-speed jets. AIAA J. 47(10), 2440–2448 (2009)

    Article  Google Scholar 

  8. Tam, C.K.W., Morris, P.J.: The radiation of sound by the instability waves of a compressible plane turbulent shear layer. J. Fluid Mech. 98(Part 2), 349–381 (1980)

    Article  MathSciNet  MATH  Google Scholar 

  9. Tam, C.K.W., Hu, F.Q.: On the three families of instability waves of high-speed jets. J. Fluid Mech. 201, 447–484 (1989)

    Article  MathSciNet  MATH  Google Scholar 

  10. Papamoschou, D.: Structure of the compressible turbulent shear layer. AIAA J. 29(5), 680–681 (1991)

    Article  Google Scholar 

  11. Papamoschou, D.: Mach wave elimination in supersonic jets. AIAA-97-0147 (1997)

  12. Papamoschou, D., Bunyajitradulya, A.: Evolution of large eddies in compressible shear layers. Phys. Fluids 9(3), 756–764 (1997)

    Article  Google Scholar 

  13. Papamoschou, D., Debiasi, M.: Noise measurements in supersonic jets treated with the Mach wave elimination method. AIAA J. 37(2), 154–160 (1999)

    Article  Google Scholar 

  14. Colonius, T., Lele, S.K., Moin, P.: Sound generation in a mixing layer. J. Fluid Mech. 330, 375–409 (1997)

    Article  MATH  Google Scholar 

  15. Lele, S.K., Mendez, S., Ryu, J., Nichols, J., Shoeybi, M., Moin, P.: Sources of high-speed jet noise: analysis of LES data and modeling. Procedia Eng. 6, 84–93 (2010)

    Article  Google Scholar 

  16. Freund, J.B., Lele, S.K., Moin, P.: Numerical simulation of a Mach 1.92 turbulent jet and its sound field. AIAA J. 38(11), 2023–2031 (2000)

    Article  Google Scholar 

  17. Rossmann, T., Mungal, M.G., Hanson, R.K.: Character of Mach wave radiation and convection velocity estimation in supersonic shear layers. AIAA 2002–2571 (2002)

  18. Prasun, K.R., Lele, S.K.: Sound generated by instability wave/shock-cell interaction in supersonic jets. J. Fluid Mech. 587, 173–215 (2007)

    MathSciNet  MATH  Google Scholar 

  19. Mendez, S., Shoeybi, M., Sharma, A., Ham, F.E., Lele, S.K., Moin, P.: Large-eddy simulation of perfectly expanded supersonic jets using an unstructured solver. AIAA J. 50(5), 1103–1118 (2012)

    Article  Google Scholar 

  20. de Cacqueray, N., Bogey, C., Bailly, C.: Investigation of a high-Mach-number overexpanded jet using large-eddy simulation. AIAA J. 49(10), 2171–2182 (2011)

    Article  Google Scholar 

  21. Murakami, E., Papamoschou, D.: Mean Flow development in dual-strem compressible jets. AIAA J. 40(6), 1131–1138 (2002)

    Article  Google Scholar 

  22. Lowson, M.V., Ollerhead, J.B.: Visualization of noise from cold supersonic jets. J. Aeronaut. Soc. Am. 44(2), 624–630 (1968)

  23. Elliot, G.S., Samimy, Mo, Arnette, S.A.: The characteristics and evolution of large-scale structures in compressible mixing layers. Phys. Fluids 7(4), 864–876 (1995)

    Article  Google Scholar 

  24. Lau, J.C., Fisher, M.J.: The vortex-street structure of ‘turbulent’ jets. Part 1. J. Fluid Mech. 67, 299–337 (1975)

    Article  Google Scholar 

  25. Oertel Sen., H., Seiler, F., Srulijes, J.: New explanation of noise production by supersonic jets with gas dredging. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol. 112, pp. 389–397. New Results in Numerical and Experimental Fluid Mechanics VII. Springer, Berlin (2010)

  26. Oertel Sen., H., Seiler, F., Srulijes, J.: Vortex induced Mach waves in supersonic jets. In: Proceedings of the 28th International Symposium on Shock Waves, Manchester (2011)

  27. Oertel Sen., H., Seiler, F., Srulijes, J.: Visualization of Mach waves produced by a supersonic jet and theoretical explanations. J. Vis. 16(4), 303–312 (2013)

    Article  Google Scholar 

  28. Oertel Sen., H., Seiler, F., Srulijes, J., Hruschka, R.: Vortical structures as Mach wave sources in the mixing layer of supersonic jets. In: Proceedings of the 29th International Symposium on Shock Waves, Madison (2013)

  29. Shapiro, A.H.: The Dynamics and Thermodynamics of Compressible Fluid Flow, vol. I. The Ronald Press Company, New York (1953)

    Google Scholar 

  30. Oertel, H.: Dynamik der Machwellen in der Umgebung von Überschallstrahlen (dynamics of Mach waves near supersonic jets). ISL-Report R 124/81 (1981)

  31. Chien, K.-Y., Ferguson, R.E., Kuhl, A.L., Glaz, H.M., Colella, P.: Inviscid dynamics of two-dimensional shear layers. AIAA-91-1978 (1999)

  32. Mitchell, B.E., Lele, S.K., Moin, P.: Direct computation of the sound generated by vortex pairing in an axisymmetric jet. J. Fluid Mech. 383, 113–142 (1999)

    Article  MATH  Google Scholar 

  33. Bühler, S.: Numerical simulation of laminar and turbulent nozzle-jet flows and their sound. Dissertation at ETH Zürich No. 21483 (2013)

  34. Oertel Sen., H., Seiler, F., Srulijes, J.: The limits of Mach wave emission from supersonic jets. In: Proceedings of the 30th International Symposium on Shock Waves, Tel Aviv (2015)

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to F. Seiler.

Additional information

Communicated by M. Brouillette and A. Podlaskin.

H. Oertel Sen., F. Seiler and J. Srulijes: retired from the ISL.

This paper is based on work that was presented at the 21st International Symposium on Shock Interaction, Riga, Latvia, August 3–8, 2014.

Rights and permissions

Reprints and permissions

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Oertel Sen, H., Seiler, F., Srulijes, J. et al. Mach waves produced in the supersonic jet mixing layer by shock/vortex interaction. Shock Waves 26, 231–240 (2016). https://doi.org/10.1007/s00193-015-0612-1

Download citation

  • Received:

  • Revised:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s00193-015-0612-1

Keywords

Navigation