Data augmented turbulence modeling for three-dimensional separation flows
نویسندگان
چکیده
Field inversion and machine learning are implemented in this study to describe three-dimensional (3D) separation flow around an axisymmetric hill augment the Spalart–Allmaras (SA) model. The discrete adjoint method is used solve field problem, artificial neural network as A validation process for proposed adjust hyperparameters obtain a physically acceptable solution. result shows that non-equilibrium turbulence effects boundary layer upstream of mean line separating shear dominate structure 3D flow, which agrees with prior physical knowledge. However, effect anisotropy on appears be limited. Two approaches stage overcome problem sample imbalance while reducing computational cost during training. results all satisfactory, proves effectiveness approaches.
منابع مشابه
Three-Dimensional Modeling Interface for Augmented Realities
Today’s geometric modeling tools are usually controlled by the mouse and keyboard. 3dmodeling operations are often constrained to planes or lines to make modeling easier. New augmented reality devices promise new classes of applications with natural 3d user interfaces. This paper deals with a new method that enables users to model 3d shapes directly with their fingers. It is implemented in Arti...
متن کامل2DV Nonlinear k-ε Turbulence Modeling of Stratified Flows
The commonly used linear k-ε turbulence model is shown to be incapable of accurate prediction of turbulent flows, where non-isotropy is dominant. Two examples of non-isotropic flows, which have a wide range of applications in marine waters, are saline water flow and the stratified flows due to temperature gradients. These relate to stratification and consequently, variation of density through...
متن کاملTurbulence Modeling Validation for Afterbody Flows
The aerothermodynamics phenomena over space launch vehicles or missiles are a challenging problem on space and aeronautical applications. These physical phenomena can strongly affect the engine's aerodynamic performances. The physical problem met on this geometry is essentially the result of the interaction of two merging flows; one issued from a propulsive jet at high speed and high temperatur...
متن کاملStudy of Parameters Affecting Separation Bubble Size in High Speed Flows using k-ω Turbulence Model
Shock waves generated at different parts of vehicle interact with the boundary layer over the surface at high Mach flows. The adverse pressure gradient across strong shock wave causes the flow to separate and peak loads are generated at separation and reattachment points. The size of separation bubble in the shock boundary layer interaction flows depends on various parameters. Reynolds-averaged...
متن کاملNonextensivity in turbulence in rotating two-dimensional and three-dimensional flows
Our experiments on turbulent flow in a rotating annulus yield probability distribution functions (PDFs) for velocity increments δv( ), where is the separation between points. We fit these PDFs to a form derived for turbulent flows by Beck, who used the Tsallis nonextensive statistical mechanics formalism. For slow rotation rates, we find that the fit parameter q is 1.25 for small . At large , q...
متن کاملذخیره 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: 2022
ISSN: ['1527-2435', '1089-7666', '1070-6631']
DOI: https://doi.org/10.1063/5.0097438