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A METHODOLOGY FOR MODELLING ENCLOSURE RADIATION HEAT TRANSFER UNDER LARGE STRUCTURAL DEFORMATION

机译:大结构变形下壳体辐射传热的建模方法

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Finite element method (FEM) numerical simulations of heat transfer for high-temperature regimes often require modeling of grey-body enclosure radiation where enclosure geometry definitions are obtained as part of the model grid generation process. Owing to the expense of solving the radiation problem, typical FEM approaches loosely couple the radiative transfer solution as boundary conditions to a standard conduction formulation. When the problem at hand is thermal-mechanical and relative motion occurs between enclosure surfaces, the simulation code is tasked with providing a means of updating the original enclosure surface geometry to reflect the deformed configuration. While this scenario is manageable for contiguously meshed discretizations, the difficulty of updating enclosure geometry is greatly increased when the model admits sliding. Here the analysis code must employ both mechanical and thermal contact, relying heavily on geometric search and contact constraints to enforce closure for the conduction formulation.General purpose large-deformation FEM structural codes employ surface contact utilities to provide geometric search and contact constraint definitions. This paper describes an ongoing effort to leverage contact utilities for solving the enclosure radiation problem in deforming and sliding mesh scenarios while having minimal impact to a traditional modeling approach. The current effort is divided into two areas, enclosure definitions and thermal contact, but the primary focus here is on enabling use of contact to provide definition of the enclosure. The proposed methodology is demonstrated on simple enclosure radiation models using SNL Sierra Mechanics Dash contact utilities and the Chaparral enclosure radiation library with Sierra Mechanics Structural and Thermal application codes.Sandia National Laboratories is a multi-program laboratory managed and operated by Sandia Corporation, a wholly owned subsidiary of Lockheed Martin Corporation, for the U.S. Department of Energys National Nuclear Security Administration under contract DE-AC04-94AL85000.
机译:高温状态下热传递的有限元方法(FEM)数值模拟通常需要对灰体外壳辐射进行建模,其中在模型网格生成过程中获得外壳几何形状定义。由于解决辐射问题的代价,典型的有限元方法将辐射传递解作为边界条件松散地耦合到标准传导公式上。当眼前的问题是热机械问题,并且外壳表面之间发生相对运动时,模拟代码的任务是提供一种更新原始外壳表面几何形状的方法,以反映变形的构造。尽管这种情况对于连续网格离散化是可管理的,但是当模型允许滑动时,更新外壳几何形状的难度将大大增加。在这里,分析代码必须同时采用机械接触和热接触,这在很大程度上依赖于几何搜索和接触约束来强制闭合导电配方。通用大变形FEM结构代码使用表面接触实用程序来提供几何搜索和接触约束定义。本文描述了正在进行的一项工作,以利用接触实用程序来解决变形和滑动网格场景中的外壳辐射问题,同时对传统建模方法的影响最小。当前的工作分为两个区域,即外壳定义和热接触,但是这里的主要重点是使能使用接触来提供外壳的定义。使用SNL Sierra Mechanics Dash接触实用程序和具有Sierra Mechanics结构和热学应用代码的Chaparral外壳辐射库在简单的外壳辐射模型上演示了所建议的方法.Sandia国家实验室是由Sandia Corporation管理和运营的多程序实验室是美国洛克希德·马丁公司(Lockheed Martin Corporation)的全资子公司,合同号为DE-AC04-94AL85000。

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