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.

برای دانلود رایگان متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

منابع مشابه

Assessment of inflow boundary conditions for compressible turbulent boundary layers

A description of different inflow methodologies for turbulent boundary layers, including validity and limitations, is presented. We show that the use of genuine periodic boundary conditions, in which no alteration of the governing equations is made, results in growing mean flow and decaying turbulence. Premises under which the usage is valid are presented and explained, and comparisons with the...

متن کامل

Boundary Layers for the Navier-Stokes Equations of Compressible Heat-Conducting Flows with Cylindrical Symmetry

We consider the Navier-Stokes equations for viscous compressible heat-conducting fluids with cylindrical symmetry. Our main purpose is to study the boundary layer effect and convergence rates as the shear viscosity μ goes to zero. We show that the boundary layer thickness and a convergence rate are of order O(μ) with 0 < α < 1/2 and O( √ μ) respectively, thus extending the result for isentropic...

متن کامل

Estimating the unknown heat flux on the wall of a heat exchanger internal tube using inverse method

In the design of heat exchangers, it is necessary to determine the heat transfer rate between hot and cold fluids in order to calculate the overall heat transfer coefficient and the heat exchanger efficiency. Heat transfer rate can be determined by inverse methods. In this study, the unknown space-time dependent heat flux imposed on the wall of a heat exchanger internal tube is estimated by app...

متن کامل

A numerical study of compressible turbulent boundary layers

Compressible turbulent boundary layers with free-stream Mach number ranging from 2.5 up to 20 are analyzed by means of direct numerical simulation of the Navier–Stokes equations. The fluid is assumed to be an ideal gas with constant specific heats. The simulation generates its inflow condition using the rescaling-recycling method. The main objective is to study the effect of Mach number on turb...

متن کامل

ذخیره در منابع من


  با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید

ژورنال

عنوان ژورنال: Physics of Fluids

سال: 2023

ISSN: ['1527-2435', '1089-7666', '1070-6631']

DOI: https://doi.org/10.1063/5.0150696