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Analysis and Calibration of Internal Flow Force of Ejector-Powered Engine Simulator System in Wind Tunnels

TANG Wei WU Chaojun HU Buyuan

南京航空航天大学学报(英文版)2019,Vol.36Issue(5):747-759,13.
南京航空航天大学学报(英文版)2019,Vol.36Issue(5):747-759,13.

Analysis and Calibration of Internal Flow Force of Ejector-Powered Engine Simulator System in Wind Tunnels

Analysis and Calibration of Internal Flow Force of Ejector-Powered Engine Simulator System in Wind Tunnels

TANG Wei 1WU Chaojun 2HU Buyuan2

作者信息

  • 1. School of Aeronautics,Northwestern Polytechnical University,Xi'an 710072,P.R. China
  • 2. Low Speed Aerodynamics Research Institute,China Aerodynamic Research and Development Center, Mianyang 621000,P.R. China
  • 折叠

摘要

关键词

low-speed wind tunnel/ejector-powered engine simulator/calibration tank/internal flow force/inlet/jet

Key words

low-speed wind tunnel/ejector-powered engine simulator/calibration tank/internal flow force/inlet/jet

分类

信息技术与安全科学

引用本文复制引用

TANG Wei,WU Chaojun,HU Buyuan..Analysis and Calibration of Internal Flow Force of Ejector-Powered Engine Simulator System in Wind Tunnels[J].南京航空航天大学学报(英文版),2019,36(5):747-759,13.

基金项目

This work was supported by the funda-mental research the Funds of China Aerodynamics Research and Development Center. And the authors would like to ac-knowledge the following people for their assistance:ZHANG Rongping, LI Dong, LIANG Jian, and all with the Low-Speed Aerodynamics Institute of China Aerodynam-ics Research and Development Center. ()

南京航空航天大学学报(英文版)

OACSCDCSTPCD

1005-1120

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