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飞机发动机短舱外形设计及数值仿真

单文娟 闻捷

航空科学技术Issue(2):16-19,4.
航空科学技术Issue(2):16-19,4.

飞机发动机短舱外形设计及数值仿真

Design and Numerical Simulation of Aircraft Engine Nacelle’s Shape

单文娟 1闻捷1

作者信息

  • 1. 上海飞机设计研究院,上海 200232
  • 折叠

摘要

Abstract

An engine nacelle has significant influence on the aircraft’s performance. In this paper, the parameters were selected and the aerodynamic shape was designed for a commercial aircraft’s engine nacelle. The numerical simulation results indicate that the aerodynamic shape of the nacelle designed in this paper meets the design requirements, and the total pressure recovery coefifcient becomes larger with the length of the inlet decreasing.

关键词

发动机短舱/外形设计/数值仿真/进气道/流动特性

Key words

engine nacelle/shape design/numerical simulation/air inlet/lfow qualities

分类

航空航天

引用本文复制引用

单文娟,闻捷..飞机发动机短舱外形设计及数值仿真[J].航空科学技术,2016,(2):16-19,4.

航空科学技术

1007-5453

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