Large-Eddy Simulation of Heat Transfer from a Single Cube Mounted on a Very Rough Wall

The Wall-modeled Large-eddy Simulation (WMLES) methods are commonly accompanied with an underprediction of the skin friction and a deviation of the velocity profile. The widely-used Improved Delayed Detached Eddy Simulation (IDDES) method is suggested to improve the prediction of the mean skin friction when it acts as WMLES, as claimed by the original authors. However, the model tested only on flow configurations with no heat transfer. This study takes a systematic approach to assess the performance of the IDDES model for separated flows with heat transfer. Separated flows on an isothermal wall and walls with mild and intense heat fluxes are considered. For the case of the wall with heat flux, the skin friction and Stanton number are underpredicted by the IDDES model however, the underprediction is less significant for the isothermal wall case. The simulations of the cases with intense wall heat transfer reveal an interesting dependence on the heat flux level supplied; as the heat flux increases, the IDDES model declines to predict the accurate skin friction.

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Wall-modeled large eddy simulation of turbulent heat transfer by the lattice Boltzmann method

Journal of Computational Physics ◽

10.1016/j.jcp.2021.110186 ◽

2021 ◽

Vol 433 ◽

pp. 110186

Author(s):

Y. Kuwata ◽

K. Suga

Keyword(s):

Heat Transfer ◽

Large Eddy Simulation ◽

Lattice Boltzmann Method ◽

Lattice Boltzmann ◽

Turbulent Heat Transfer ◽

Turbulent Heat ◽

Eddy Simulation ◽

Large Eddy ◽

Boltzmann Method

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Large-Eddy Simulation Study of Flow and Heat Transfer in Swirling and Non-Swirling Impinging Jets on a Semi-Cylinder Concave Target

Applied Sciences ◽

10.3390/app11157167 ◽

2021 ◽

Vol 11 (15) ◽

pp. 7167

Author(s):

Liang Xu ◽

Xu Zhao ◽

Lei Xi ◽

Yonghao Ma ◽

Jianmin Gao ◽

...

Keyword(s):

Heat Transfer ◽

Large Eddy Simulation ◽

Wall Temperature ◽

Target Surface ◽

Impinging Jets ◽

Small Scale ◽

Complex Flow ◽

Eddy Simulation ◽

Flow And Heat Transfer ◽

Large Eddy

Swirling impinging jet (SIJ) is considered as an effective means to achieve uniform cooling at high heat transfer rates, and the complex flow structure and its mechanism of enhancing heat transfer have attracted much attention in recent years. The large eddy simulation (LES) technique is employed to analyze the flow fields of swirling and non-swirling impinging jet emanating from a hole with four spiral and straight grooves, respectively, at a relatively high Reynolds number (Re) of 16,000 and a small jet spacing of H/D = 2 on a concave surface with uniform heat flux. Firstly, this work analyzes two different sub-grid stress models, and LES with the wall-adapting local eddy-viscosity model (WALEM) is established for accurately predicting flow and heat transfer performance of SIJ on a flat surface. The complex flow field structures, spectral characteristics, time-averaged flow characteristics and heat transfer on the target surface for the swirling and non-swirling impinging jets are compared in detail using the established method. The results show that small-scale recirculation vortices near the wall change the nearby flow into an unstable microwave state, resulting in small-scale fluctuation of the local Nusselt number (Nu) of the wall. There is a stable recirculation vortex at the stagnation point of the target surface, and the axial and radial fluctuating speeds are consistent with the fluctuating wall temperature. With the increase in the radial radius away from the stagnation point, the main frequency of the fluctuation of wall temperature coincides with the main frequency of the fluctuation of radial fluctuating velocity at x/D = 0.5. Compared with 0° straight hole, 45° spiral hole has a larger fluctuating speed because of speed deflection, resulting in a larger turbulence intensity and a stronger air transport capacity. The heat transfer intensity of the 45° spiral hole on the target surface is slightly improved within 5–10%.

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Towards High-Order Large Eddy Simulation of Aero-Thermal Flows for Turbomachinery Applications

Volume 2B: Turbomachinery ◽

10.1115/gt2017-63358 ◽

2017 ◽

Cited By ~ 2

Author(s):

R. Bhaskaran ◽

Feilin Jia ◽

Gregory M. Laskowski ◽

Z. J. Wang ◽

Umesh Paliath

Keyword(s):

Heat Transfer ◽

Large Eddy Simulation ◽

Numerical Algorithms ◽

High Order ◽

Sixth Order ◽

Computational Grids ◽

Variable Order ◽

Free Stream Turbulence ◽

Eddy Simulation ◽

Large Eddy

The solution accuracy and computational efficiency of high order Large Eddy Simulation (LES) solvers are evaluated on two benchmark open literature blade cascade problems. The first problem concerns wake development in the T106A low pressure turbine cascade [1]. The second problem examines the effect of free-stream turbulence on heat transfer from the VKI first stage high pressure turbine vane [2]. The calculations are performed with two independently developed high order LES solvers using completely different numerical algorithms. The first solver FDL3Di [3] was originally developed at the Airforce Research Laboratory (AFRL) and employs structured overset grids. It uses a sixth order compact finite difference scheme in space along with an implicit Beam-Warming scheme for time marching. The second solver, hpMusic, is developed at the University of Kansas [4]. This is a variable order (up to sixth order) unstructured grid solver employing a discontinuous formulation known as flux reconstruction (FR) / correction procedure via reconstruction (CPR) [5]. The computational grids used are independently tuned for each application. The solvers are benchmarked against experimental data for wake development and blade heat transfer coefficient. Further physical insights in to the test cases are also obtained, filling gaps in experimental results, especially for the VKI problem.

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