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Modeling Technique of the Aircraft Unsteady Aerodynamics Due to the Travelling Gust

JING Zhiwei TANG Chu

国际设备工程与管理(英文版)2022,Vol.27Issue(2):86-102,17.
国际设备工程与管理(英文版)2022,Vol.27Issue(2):86-102,17.DOI:10.13434/j.cnki.1007-4546.2022.0202

Modeling Technique of the Aircraft Unsteady Aerodynamics Due to the Travelling Gust

Modeling Technique of the Aircraft Unsteady Aerodynamics Due to the Travelling Gust

JING Zhiwei 1TANG Chu2

作者信息

  • 1. General Configuration and Aerodynamics Design Department,Xi'an Aircraft Design Institute,Xi'an 710089,China
  • 2. Unmanned System Research Institute,Northwestern Polytechnical University,Xi'an 710072,China
  • 折叠

摘要

关键词

travelling gust/elastic aircraft/unsteady aerodynamics/doublet lattice method

Key words

travelling gust/elastic aircraft/unsteady aerodynamics/doublet lattice method

引用本文复制引用

JING Zhiwei,TANG Chu..Modeling Technique of the Aircraft Unsteady Aerodynamics Due to the Travelling Gust[J].国际设备工程与管理(英文版),2022,27(2):86-102,17.

国际设备工程与管理(英文版)

1007-4546

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