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基于多核并行计算的无人机CFD数值模拟

姜悦宁 贾宏光 厉明

计算机工程与应用2018,Vol.54Issue(7):221-225,238,6.
计算机工程与应用2018,Vol.54Issue(7):221-225,238,6.DOI:10.3778/j.issn.1002-8331.1610-0350

基于多核并行计算的无人机CFD数值模拟

CFD numerical simulation of unmanned aerial vehicle based on multi-core parallel computation

姜悦宁 1贾宏光 2厉明3

作者信息

  • 1. 中国科学院 长春光学精密机械与物理研究所,长春130033
  • 2. 中国科学院大学,北京100039
  • 3. 长光卫星技术有限公司,长春130033
  • 折叠

摘要

Abstract

With the computer system developing towards multi-processor and multi-core architecture,a CFD(Computa-tional Fluid Dynamics)numerical simulation method with multi-core CPU has been proposed to solve large-scale aeronautical engineering problems accurately.The serial and parallel solution program is validated using a tested wing. The numerical method based on N-S(Navier-Stokes)equations proves its effective and the parallel efficiency as well as the execute time and speed-up ratio is discussed.An efficient parallel computation method is developed to calculate the longitude aerodynamics for Unmanned Aerial Vehicle(UAV). Script record of FLUENT tool is applied for switching and saving processes automatically.The advantage of parallel method as well as the modular working principle has been introduced.

关键词

计算流体力学(CFD)/并行计算/气动布局/数值模拟/加速比

Key words

Computational Fluid Dynamics(CFD)/parallel computation/aerodynamic configuration/numerical simula-tion/speed-up ratio

分类

航空航天

引用本文复制引用

姜悦宁,贾宏光,厉明..基于多核并行计算的无人机CFD数值模拟[J].计算机工程与应用,2018,54(7):221-225,238,6.

基金项目

中国科学院知识创新工程国防科技创新资金资助项目(No.YYYJ-1122). (No.YYYJ-1122)

计算机工程与应用

OA北大核心CSCDCSTPCD

1002-8331

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