首页> 外文会议>International Nuclear Atlantic Conference >ARTIFICIAL DISSIPATION MODELS APPLIED TO NAVIER-STOKES EQUATIONS FOR ANALYSIS OF SUPERSONIC FLOW OF HELIUM GAS AROUND A GEOMETRIC CONFIGURATION RAMP TYPE
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ARTIFICIAL DISSIPATION MODELS APPLIED TO NAVIER-STOKES EQUATIONS FOR ANALYSIS OF SUPERSONIC FLOW OF HELIUM GAS AROUND A GEOMETRIC CONFIGURATION RAMP TYPE

机译:应用于Navier-Stokes方程的人工耗散模型,用于分析几何配置斜坡型氦气的超音速流动

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Very High Temperature Gas Cooled Reactors - VHTGRs are studied by several research groups for the development of advanced reactors that can meet the world's growing energy demand. The analysis of the flow of helium coolant around the various geometries at the core of these reactors through computational fluid dynamics techniques is an essential tool in the development of conceptual designs of nuclear power plants that provide added safety. This analysis suggests a close analogy with aeronautical cases widely studied using computational numerical techniques to solve systems of governing equations for the flow involved. The present work consists in solving the Navier-Stokes equations in a conservative form, in two-dimensional space employing a finite difference formulation for spatial discretization using the Euler method for explicit marching in time. The physical problem of supersonic laminar flow of helium gas along a ramp configuration is considered. For this, the Jameson and Mavriplis algorithm and the artificial dissipations models linear and nonlinear of Pulliam was implemented. A spatially variable time step is employed aiming to accelerate the convergence to the steady state solution. The main purpose of this work is to study the cited dissipation models and describe their characteristics in relation to the overall quality of the solution, aiming preliminar results for the development of computational tools of dinamic analysis of helium flow for the VHTGR core.
机译:非常高温气体冷却反应器 - VHTGR是由几个研究组研究的,用于开发先进的反应堆,可以满足世界不断增长的能源需求。通过计算流体动力学技术对这些反应器芯的各种几何形状周围的氦冷却剂流动的分析是开发核电站概念设计的基本工具,提供了增加的安全性。该分析表明,利用计算数值求解所涉及的流程的控制方程系统,与航空病例进行了密切类比。本工作包括以保守形式求解Navier-Stokes方程,在使用有限差异配方的二维空间中,使用欧拉方法进行空间离散化,以便及时明确行进。考虑了沿斜坡构型氦气的超音速层流流动的物理问题。为此,实施了Jameson和Mavriplis算法和人工耗散模型,Lughiam的线性和非线性。采用空间可变的时间步骤,目的是加速稳态解决方案的收敛。这项工作的主要目的是研究引用的耗散模型,并描述了与解决方案的整体质量相关的特征,旨在对VHTGR核心的氦流量分析的计算工具的开发进行预言。

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