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航空CFD高性能计算应用研究

李权 郭兆电 邓一菊 廖振荣

华中科技大学学报(自然科学版)2011,Vol.39Issue(z1):79-82,4.
华中科技大学学报(自然科学版)2011,Vol.39Issue(z1):79-82,4.

航空CFD高性能计算应用研究

CFD high performance computing in aeronautics

李权 1郭兆电 1邓一菊 1廖振荣1

作者信息

  • 1. 中航工业第一飞机设计研究院,陕西西安710089
  • 折叠

摘要

Abstract

Using the large parallelized fluid software CCFD, the drag prediction at high speed and the performance evaluation of high-lift devices in aircraft design were performed on DeepComp 7000 super computer. The effects of different sizes' mesh and different turbulence models to the results were researched, and the efficiency between high performance computing and conventional computing was compared. The two problems' computing results are very close to the test data, which show that CCFD has a good accuracy to conventional aerodynamic problems; high performance computing can enhance the reliability and the efficiency of numerical calculation; increasing the mesh number but not updating the mathematics, the computing accuracy will not always be improved.

关键词

阻力预测;增升装置;网格;计算流体力学;高性能计算机

Key words

drag prediction/ high-lift device/ mesh/ CFD (computational fluid dynamics)/ high performance computer

分类

航空航天

引用本文复制引用

李权,郭兆电,邓一菊,廖振荣..航空CFD高性能计算应用研究[J].华中科技大学学报(自然科学版),2011,39(z1):79-82,4.

基金项目

国家高技术研究发展计划资助项目(2009AA01A130). (2009AA01A130)

华中科技大学学报(自然科学版)

OA北大核心CSCDCSTPCD

1671-4512

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