Summary
Supersonic jets emit Mach waves producing noise in their environment. Various experimental techniques have been used in the past for investigating the behaviour of structures present in the supersonic jet boundary layer. These structures are accompanied by long, almost straight and nearly parallel Mach waves. These Mach waves appear both outside and inside the jet. It was experimentally found that these Mach waves move at three preferred speeds: w, w’ and w”. They depend simply and exclusively on the jet Mach number Mi and the speed of sound ratio between inside (ai) and outside (aa) of the jet. Quite simple empiric formulae for w, w’ and w” have been established by Oertel sen. but no satisfying explanation could be found at that time. Recently, however Oertel sen. proposed a new idea based on the growth of long living pairs of vortices formed inside of the jet boundary layer. Vortices move with the velocities w’ and w” respectively, whereas the centre of the pair moves with w. The w’- and w”-vortices move supersonically with respect to aa, therefore produce the so-called w’ -Mach waves outside of the jet. The w” - vortices move with ui – w” > ai , therefore produce the so-called w”-Mach waves inside of the jet. This theory suggests a new method of jet noise reduction.
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References
Oertel, H.: Coherent structures producing Mach waves inside and outside of the supersonic jet. ISL report CO 82/218 (1982)
Ffowcs Williams, J.E., Maidanik, G.: The Mach wave field radiated by supersonic turbulent shear flows. J. Fluid Mech. 21(4), 641–657 (1965)
Tam, C.K.W.: Directional acoustic radiation from a supersonic jet generated by shear layer instability. J. Fluid Mech. 461(4), 757–768 (1971)
Michalke, H.: A note on the spatial jet-instability of the compressible cylindrical vortex sheet, DLR report, DLR-FB-70-51 (1970)
Gropengießer, H.: Beitrag zur Stabilität freier Grenzschichten in kompressiblen Medien, DLR report, DLR-FB-69-25 (1969)
Laufer, J., Schlinker, R., Kaplan, R.E.: Experiments on supersonic jet noise. AIAA J. 14(4), 489–497 (1976)
Oertel, H.: Jet noise research by means of shock tubes. In: Proceedings of the 10th International Shock Tube Symposium, Japan, Kamimoto (1975)
Oertel, H.: Mach wave radiation of hot supersonic jets investigated by means of a shock tube and new optical technics. In: Proceedings of the 12th International Symposium on Shock-Tubes and Waves, Israel, Jerusalem (1980)
Oertel, H.: Measured velocity fluctuations inside the jet boundary layer of a Supersonic jet. In: Recent contributions to fluid mechanics. Springer, Berlin (1982)
Oertel, H.: Coherent structures producing Mach waves inside and outside of the supersonic jet. In: IUTAM Symposium on complex structures in turbulent flow, IMST-Univerity d’Aix-Marseille, France (1982)
Oertel, H.: 33 years of research by means of shock tubes. In: 14th International Symposium on Shock Tubes, Australia, Sydney (1983)
Tam, C.K.W.: Supersonic jet noise. Ann. Rev. Fluid Mech. 27 (1995)
Bailly, C., Candel, S., Lafon, P.: Prediction of supersonic jet noise from a statistical acoustic model and a compressible turbulence closure. Journal of Sound and Vibration 194(2) (1996)
Papamoschou, D., Bunyajitradulya, A.: Evolution of large eddies in compressible shear layers. Phys. Fluids 9(3) (1997)
Papamoschou, D., Debiasi, M.: Noise measurements in supersonic jets treated with the Mach wave elimination method. AIAA J. 37(2) (1999)
Bassetti, A.: A statistical jet-noise model based on the acoustic analogy and a RANS solution, University of Southampton, Institute of Sound and Vibration Research, Doctoral thesis (2009)
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Sen, H.O., Seiler, F., Srulijes, J. (2010). New Explanation of Noise Production by Supersonic Jets with Gas Dredging. In: Dillmann, A., Heller, G., Klaas, M., Kreplin, HP., Nitsche, W., Schröder, W. (eds) New Results in Numerical and Experimental Fluid Mechanics VII. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol 112. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-14243-7_48
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DOI: https://doi.org/10.1007/978-3-642-14243-7_48
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