The efficiency of an airfoil can be improved by adjusting its surface. CFD software was used to investigate a 2D with and without spanwise semicircular groove on the upper NACA0012 airfoils grooves were analyzed using k-ω turbulence model. lift drag coefficients compared. To effect location efficiency, added in various locations compared smooth airfoil. flow velocity remained constant at 20 m/s...

Regurgitation in the heart diastolic phase represents a critical flow condition associated with many heart valve design considerations. The finite volume method, the Low-Reynolds-Number k-ω turbulent model and sliding mesh model are employed to solve and compare the complex flow field and the torque in each case. The end results expected from a cardiovascular CFD analysis are not limited only t...

We present enhanced physics-based finite element schemes for two families of turbulence models, the NS-ω models and the Stolz-Adams approximate deconvolution models. These schemes are delicate extensions of a method created for the Navier-Stokes equations in Rebholz 2007 , that achieve high physical fidelity by admitting balances of both energy and helicity that match the true physics. The sche...

Abstract In order to study the influence of deformations nozzle’s flexible sections on its inner wall’s heat transfer, this research uses two-dimensional axisymmetric model and k − ω SST turbulence numerically analyze tail flow field flexible-extendible nozzle under multiple working conditions. The transfer with without are simulated analyzed. simulation results show that when deformed, new sho...

This paper presents the comparison of numerical simulation results and wind tunnel experiment for compound WIG's wing. Numerical was performed in ANSYS Fluent software. The choice turbulence model computational mesh parameters, including resolution boundary layer, are substantiated. Comparison showed good convergence middle density about 7 million cells first layer height 0.0001 m. Additional s...

As one of the typical negative factors affecting vortex structure and flow characteristics hydraulic machinery, TLV has a non-negligible impact on energy performance. In order to improve utilization efficiency machinery in marine energy, parallel grooves is proposed applied NACA0009 hydrofoil. Subsequently, an exhaustive numerical analysis carried out adopting SST k-ω turbulence model, effects ...

The present study reported of the numerical investigation of a high-speed wet steam flow through an asymmetric nozzle. The spontaneous non-equilibrium homogeneous condensation of wet steam was numerically modeled based on the classical nucleation theory and droplet growth rate equation combined with the field conservations within the computational fluid dynamics (CFD) code of ANSYS Fluent 13.0....

In this research, a two-dimensional mathematical model using  turbulence model was developed in a rectangular channel with granular permeable bed. Finite volume method was used for numerical solution of governing equations. The equations considered are discretized using Hybrid difference scheme while applying SIMPLE algorithm to correct velocity components in the continuity equation. In the dev...

Combined turbulent wall and offset jets with without the presence of a parallel co-flow stream are investigated using k-ω turbulence model. We focus on effects velocity locations various characteristic points formed owing to interaction in dual jet flow. The inlet Reynolds number is taken as 15,000 ratio varied from 5 11. At low ratios, effect remains almost negligible. With progressive increas...

The mathematical and physical models of the underwater submerged gun are established to study flow field distribution characteristics muzzle at different water depths. Schnerr–Sauer cavitation model realizable k–ω transport turbulence based on Reynolds-averaged Navier–Stokes method employed. for 12.7 mm that is launched numerically simulated by combining user-defined functions overlapping mesh ...