4.8 Article

Velocity transformation for compressible wall-bounded turbulent flows with and without heat transfer

出版社

NATL ACAD SCIENCES
DOI: 10.1073/pnas.2111144118

关键词

turbulence; wall modeling; law of the wall; mean velocity profile; Mach invariance

资金

  1. National Defense Science and Engineering Graduate Fellowship
  2. Stan-ford Graduate Fellowship
  3. NASA [NNX15AU93A]
  4. Boeing Research Technology

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A transformation method mapping compressible wall-bounded turbulent flows to the incompressible law of the wall has been proposed, successfully collapsing numerical simulation data from various flows without specific tuning. The transformation is successful across the entire inner layer of the boundary layer, verifying its performance for compressible wall-bounded flows.
In this work, a transformation, which maps the mean velocity profiles of compressible wall-bounded turbulent flows to the incompressible law of the wall, is proposed. Unlike existing approaches, the proposed transformation successfully collapses, without specific tuning, numerical simulation data from fully developed channel and pipe flows, and boundary layers with or without heat transfer. In all these cases, the transformation is successful across the entire inner layer of the boundary layer (including the viscous sublayer, buffer layer, and logarithmic layer), recovers the asymptotically exact near-wall behavior in the viscous sublayer, and is consistent with the near balance of turbulence production and dissipation in the logarithmic region of the boundary layer. The performance of the transformation is verified for compressible wall-bounded flows with edge Mach numbers ranging from 0 to 15 and friction Reynolds numbers ranging from 200 to 2,000. Based on physical arguments, we show that such a general transformation exists for compressible wall-bounded turbulence regardless of the wall thermal condition.

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