EXPERIMENTS AND ANALYSIS FOR A GUST GENERATOR IN A WIND-TUNNEL

Citation
Dm. Tang et al., EXPERIMENTS AND ANALYSIS FOR A GUST GENERATOR IN A WIND-TUNNEL, Journal of aircraft, 33(1), 1996, pp. 139-148
Citations number
17
Categorie Soggetti
Aerospace Engineering & Tecnology
Journal title
ISSN journal
00218669
Volume
33
Issue
1
Year of publication
1996
Pages
139 - 148
Database
ISI
SICI code
0021-8669(1996)33:1<139:EAAFAG>2.0.ZU;2-I
Abstract
An experimental investigation was made of the gust field generated by a rotating slotted cylinder installed in the Duke University low-speed , closed-circuit wind tunnel. The system has a very simple configurati on with low cost and can produce a controllable single or multiple har monic gust wave in the lateral and longitudinal directions. It require s minimal power and torque input. A simplified theoretical aerodynamic model and a design estimation of the lateral and longitudinal gust fl owfield is also proposed in this article. The design estimate is based on a two-dimensional dynamic lift coefficient that is given by the th eoretical and experimental results. An interfering wake vortex effect is the major disadvantage of this system.