High-Reynolds number calculations of turbulent heat transfer in FlowVision software
| Autor: | Andrey A. Aksenov, Sergey V. Zhluktov, Dmitriy Vladimirovich Savitskiy |
|---|---|
| Jazyk: | ruština |
| Rok vydání: | 2018 |
| Předmět: |
wall functions
Turbulent heat transfer turbulent boundary layer heat flux 01 natural sciences high-Reynolds number calculations 010305 fluids & plasmas Physics::Fluid Dynamics symbols.namesake Software 0103 physical sciences 0101 mathematics Physics incompressible fluid business.industry lcsh:T57-57.97 lcsh:Mathematics plate Reynolds number compressible gas Mechanics lcsh:QA1-939 non-isothermal flow Computer Science Applications 010101 applied mathematics Computational Theory and Mathematics Modeling and Simulation lcsh:Applied mathematics. Quantitative methods symbols business |
| Zdroj: | Компьютерные исследования и моделирование, Vol 10, Iss 4, Pp 461-481 (2018) |
| ISSN: | 2077-6853 2076-7633 |
| Popis: | This work presents the model of heat wall functions FlowVision (WFFV), which allows simulation of nonisothermal flows of fluid and gas near solid surfaces on relatively coarse grids with use of turbulence models. The work follows the research on the development of wall functions applicable in wide range of the values of quantity y+. Model WFFV assumes smooth profiles of the tangential component of velocity, turbulent viscosity, temperature, and turbulent heat conductivity near a solid surface. Possibility of using a simple algebraic model for calculation of variable turbulent Prandtl number is investigated in this study (the turbulent Prandtl number enters model WFFV as parameter). The results are satisfactory. The details of implementation of model WFFV in the FlowVision software are explained. In particular, the boundary condition for the energy equation used in high-Reynolds number calculations of non-isothermal flows is considered. The boundary condition is deduced for the energy equation written via thermodynamic enthalpy and via full enthalpy. The capability of the model is demonstrated on two test problems: flow of incompressible fluid past a plate and supersonic flow of gas past a plate (M = 3). Analysis of literature shows that there exists essential ambiguity in experimental data and, as a consequence, in empirical correlations for the Stanton number (that being a dimensionless heat flux). The calculations suggest that the default values of the model parameters, automatically specified in the program, allow calculations of heat fluxes at extended solid surfaces with engineering accuracy. At the same time, it is obvious that one cannot invent universal wall functions. For this reason, the controls of model WFFV are made accessible from the FlowVision interface. When it is necessary, a user can tune the model for simulation of the required type of flow. The proposed model of wall functions is compatible with all the turbulence models implemented in the FlowVision software: the algebraic model of Smagorinsky, the Spalart-Allmaras model, the SST $k-\omega$ model, the standard $k-\varepsilon$ model, the $k-\varepsilon$ model of Abe, Kondoh, Nagano, the quadratic $k-\varepsilon$ model, and $k-\varepsilon$ model FlowVision. |
| Databáze: | OpenAIRE |
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