Numerical Study of Compressible Wall-Bounded Turbulence – the Effect of Thermal Wall Conditions on the Turbulent Prandtl Number in the Low-Supersonic Regime
Author:
Affiliation:
1. Aerospace Center, Japan Aerospace Exploration Agency, Chofu, Tokyo, Japan
2. NASA Langley Research Center, Hampton, VA, USA
Funder
NASA Langley Research Center
Japan Society for the Promotion of Science
Transformational Tools and Technologies
EPSRC
Publisher
Informa UK Limited
Subject
Mechanical Engineering,Mechanics of Materials,Energy Engineering and Power Technology,Condensed Matter Physics,Aerospace Engineering,Computational Mechanics
Link
https://www.tandfonline.com/doi/pdf/10.1080/10618562.2023.2189247
Reference66 articles.
1. Mean temperature calculations in a turbulent channel flow for air and mercury
2. Turbulent Prandtl number in the near-wall region of a turbulent channel flow
3. Measurements of turbulent boundary layer Prandtl numbers and space-time temperature correlations
4. Asymptotic behaviour at the wall in compressible turbulent channels
5. Turbulent heat flux in supersonic flows for different thermal boundary conditions
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