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Passive Scalar Transport in Turbulent Supersonic Channel Flow

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Part of the book series: Springer Proceedings in Physics ((SPPHY,volume 101))

Summary

Direct numerical simulations (DNS) of turbulent supersonic channel flow of air at Reynolds numbers ranging from Re τ = 180 to 560 and Mach numbers ranging from M = 0.3 to 3.0 have been performed. The DNS data are used to explain the reduction of the pressure-correlation terms due to compressibility, using a Green’s function approach.

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References

  1. G.N. Coleman, J. Kim, and R.D. Moser. Turbulent supersonic isothermal-wall channel flow. J. Fluid Mech., 305:159–183, 1995.

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  3. H. Foysi, S. Sarkar, and R. Friedrich. Compressibility Effects and Turbulence Scalings in Supersonic Channel Flow. submitted to J. Fluid Mech., 2003.

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© 2005 Springer-Verlag Berlin Heidelberg

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Foysi, H., Friedrich, R. (2005). Passive Scalar Transport in Turbulent Supersonic Channel Flow. In: Peinke, J., Kittel, A., Barth, S., Oberlack, M. (eds) Progress in Turbulence. Springer Proceedings in Physics, vol 101. Springer, Berlin, Heidelberg. https://doi.org/10.1007/3-540-27401-4_47

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  • DOI: https://doi.org/10.1007/3-540-27401-4_47

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-540-23216-2

  • Online ISBN: 978-3-540-27401-8

  • eBook Packages: EngineeringEngineering (R0)

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