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.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
References
G.N. Coleman, J. Kim, and R.D. Moser. Turbulent supersonic isothermal-wall channel flow. J. Fluid Mech., 305:159–183, 1995.
H. Foysi and R. Friedrich. DNS of Passive Scalar Transport in Turbulent Supersonic Channel Flow. Proceedings, Third International Symposium on Turbulence and Shear Flow Phenomena, Sendai, Japan, 2003,, Vol. III:1108–1116, 2003.
H. Foysi, S. Sarkar, and R. Friedrich. Compressibility Effects and Turbulence Scalings in Supersonic Channel Flow. submitted to J. Fluid Mech., 2003.
P.G. Huang, G.N. Coleman, and P. Bradshaw. Compressible turbulent channel flows: DNS results and modelling. J. Fluid Mech., 305:185–218, 1995.
R.D. Moser, J. Kim, and N. N. Mansour. Direct numerical simulation of turbulent channel flow up to Reτ = 590. Phys. Fluids, 9:943–945, 1999.
Author information
Authors and Affiliations
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2005 Springer-Verlag Berlin Heidelberg
About this paper
Cite this paper
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
Download citation
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)