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The Development of the UPACS CFD Environment

机译:普遍存存环境的发展

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UPACS (Unified Platform for Aerospace Computational Simulation), a computational environment for CFD (Computational Fluid Dynamic) in the aerospace field, has been in development at NAL (National Aerospace Laboratory of Japan) since 1998, which includes two years of support by the ITBL (IT-Based Laboratory) project. It aims to overcome the increasing programming difficulties with recent CFD codes on parallel computers for aerospace applications. The codes mainly require applicability to complex geometries, higher accuracy, and coupling with heat conduction analysis in materials and structure analysis. UP-ACS successfully developed a general parallelized CFD code for aerospace applications in Japan. This paper describes in detail programming, applications, and parallel performance on the newly installed supercomputer at NAL.
机译:UPACS(航空航天计算模拟统一平台),航空航天领域的CFD(计算流体动力学)的计算环境,自1998年以来一直在NAL(日本国家航空航天实验室)开发,其中包括两年的支持(基于实验室)项目。它旨在克服最近在航空航天应用的平行计算机上的CFD代码增加的编程困难。该代码主要需要适用于复杂的几何形状,更高的精度和与材料和结构分析中的热传导分析的耦合。 UP-ACS成功开发了日本航空航天应用的一般并行CFD代码。本文介绍了NAL上新安装的超级计算机上的详细编程,应用程序和并行性能。

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