Decomposition of the wall-heat flux of compressible boundary layers
نویسندگان
چکیده
We use the method developed by Elnahhas and Johnson [“On enhancement of boundary layer skin friction turbulence: An angular momentum approach,” J. Fluid Mech. 940, A36 (2022)] Xu et al. [“Decomposition skin-friction coefficient compressible layers,” Phys. Fluids 35, 035107 (2023)] for decomposition to integrate mean temperature equation high-Reynolds-number layers arrive at an identity wall-heat flux. The physical interpretation limitations this approach are discussed. perform integration on obtain that is heat-transfer analog von Kármán integral coefficient. This applied numerical data laminar turbulent layers, revealing mean-flow dissipation production kinetic energy given Favre–Reynolds stresses dominate thermal-energy balance. term related growth opposes wall cooling. Other identities flux, inspired Fukagata [“Contribution Reynolds stress distribution in wall-bounded flows,” 14(11), L73–L76 (2002)], studied numerically asymptotic methods. terms these depend spuriously upper bound because a mathematical quantity used derivation. When asymptotically large, simplify equation. also prove existing multiple-integration reduces definition flux when number integrations large. No information about transfer extracted impact nonphysical.
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ژورنال
عنوان ژورنال: Physics of Fluids
سال: 2023
ISSN: ['1527-2435', '1089-7666', '1070-6631']
DOI: https://doi.org/10.1063/5.0150696