A Numerical Simulation Method for Plate Impingement Jet Heat Transfer Problem

A numerical simulation and impingement jet technology, applied in the field of fluids, can solve the problems of the hard-to-get Nusselt number distribution of flat-plate impingement jets and the inability to accurately predict the distribution of Nusselt number on the impact plate surface, and achieve the effect of improving accuracy

Active Publication Date: 2020-09-29
DALIAN UNIV OF TECH
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Problems solved by technology

Early numerical calculations of impinging jets found that the traditional model and the standard model cannot accurately predict the Nusselt number distribution on the impinging plate surface when calculating the plate impinging jet heat transfer problem
With the development of computer computing power, methods such as v2-f turbulence model, large eddy simulation turbulence model (LES), direct numerical simulation (DNS) and other methods have been widely used, but it is still difficult to obtain accurate nuceration in flat plate impingement jet flow. Algorithm distribution

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  • A Numerical Simulation Method for Plate Impingement Jet Heat Transfer Problem
  • A Numerical Simulation Method for Plate Impingement Jet Heat Transfer Problem
  • A Numerical Simulation Method for Plate Impingement Jet Heat Transfer Problem

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specific Embodiment approach

[0049] (1) Establish a calculation model

[0050] According to the experimental data, a flat impact jet model including the adiabatic impact surface and the closed plate is established; the experimental model is selected as an example to verify, the nozzle width is 0.04m, the impact height is 4 times and 9.2 times the nozzle width, and the length of the impact plate is taken 50 times the nozzle width.

[0051] (2) Verification of model meshing and mesh independence

[0052] The grid is divided in ICEM, and the grid type adopts structural grid, such as figure 2 Shown. According to the selected SSTk-ω turbulence model, select a set of y arranged from large to small + Perform grid independence verification and use ICEM for grid division. Import the divided mesh into ANSYS-FLUENT for trial operation until y is adjacent twice + The calculated results of the local Nusselt number of the impact plate are similar, so choose the smaller y + As the optimal grid for the next calculation, the ...

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Abstract

The invention discloses a numerical simulation method for a plate impact jet flow heat transfer problem. The method comprises the following steps that: S1: establishing a calculation model, and according to experimental data, establishing a plate impact jet model which contains a thermal insulation impact face and a sealed plate; S2: carrying out grid division and grid independence verification onthe model; S3: setting a turbulence model, and selecting an SSTk-[Omega] model to be coupled with an intermittent transition model, a cross flow transition model and a Kato-Launder model; S4: according to a practical situation, setting a boundary condition and an initial value; S5: setting the solving way of ANSYS-FLUENT software; and S6: operating the ANSYS-FLUENT, obtaining the heat transfer distribution rule of the plate impact jet flow under different heights, and expressing the heat transfer rule by a dimensionless Nusselt number Nu. By use of the method, the influence of transition on the impact jet flow heat transfer is considered so as to better conform to the physical phenomenon of the impact jet flow heat transfer, and therefore, calculation accuracy is improved.

Description

Technical field [0001] The invention relates to the technical field of fluids, in particular to a numerical simulation method for the heat transfer problem of a flat plate impinging jet. Background technique [0002] The heat transfer phenomenon of impinging jets is widespread and widely used in civil and military fields. Because it has a very thin boundary layer in the stagnation zone, which can greatly improve the heat transfer efficiency, it is widely used in such as paper and textile drying, gas turbine blade cooling, rapid cooling of high-speed aircraft, and cooling of electronic components. And wing deicing. In the military field, the launch of unmanned aircraft, the launch of weapons, and the take-off of vertical take-off and landing aircraft are all closely related to the impact jet phenomenon. Accurate numerical simulation of the impinging jet phenomenon is of great significance for optimizing the design based on an in-depth understanding of the problem mechanism. [00...

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F17/11G06F30/20G06F111/10G06F119/08
CPCG06F17/11G06F30/20G06F2111/10G06F2119/08
Inventor 张桂勇黄华坤孙铁志回达姜宜辰孙雷孙哲宗智
Owner DALIAN UNIV OF TECH
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