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Development of an active gust generation mechanism on a wind tunnel for wind engineering and industrial aerodynamics applications

  • Haan, Fred L. Jr. (Department of Aerospace Engineering, Iowa State University) ;
  • Sarkar, Partha P. (Department of Aerospace Engineering, Iowa State University) ;
  • Spencer-Berger, Nicholas J. (Dynamic Flight Loads, The Boeing Company)
  • 투고 : 2005.05.30
  • 심사 : 2006.08.17
  • 발행 : 2006.10.25

초록

A combination Aerodynamic/Atmospheric Boundary Layer (AABL) Wind and Gust Tunnel with a unique active gust generation capability has been developed for wind engineering and industrial aerodynamics applications. This facility is a cornerstone component of the Wind Simulation and Testing (WiST) Laboratory of the Department of Aerospace Engineering at Iowa State University (ISU). The AABL Wind and Gust tunnel is primarily a closed-circuit tunnel that can be also operated in open-return mode. It is designed to accommodate two test sections ($2.44m{\times}1.83m$ and $2.44m{\times}2.21m$) with a maximum wind speed capability of 53 m/s. The gust generator is capable of producing non-stationary gust magnitudes around 27% of the mean flow speed. This paper describes the motivation for developing this gust generator and the work related to its design and testing.

키워드

참고문헌

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