Blockage-tolerant wind tunnel measurements for a NACA 0012 at high angles of attack-Reference-Cited by-同舟云学术

Blockage-tolerant wind tunnel measurements for a NACA 0012 at high angles of attack

Published:2015-10 Issue: Volume:145 Page:209-218
ISSN:0167-6105
Container-title:Journal of Wind Engineering and Industrial Aerodynamics
language:en
Short-container-title:Journal of Wind Engineering and Industrial Aerodynamics

Author:

Rainbird J.M.^ORCID,Peiró J.,Graham J.M.R.

Funder

Environmental Services Association Education Trust

Publisher

Elsevier BV

Subject

Mechanical Engineering,Renewable Energy, Sustainability and the Environment,Civil and Structural Engineering

Reference33 articles.

1. Allen, H., Vincenti, W., 1944. Wall Interference in a Two-Dimensional-Flow Wind Tunnel, With Consideration of the Effect of Compressibility. Technical Report TR 782, NACA.

2. Aerodynamic characteristics of NACA 0012 aircraft in relation to wind generators;Bergeles;Wind Eng.,1983

3. Bianchini, A., Ferrari, L., Magnani, S., 2011. Start-up behavior of a three-bladed H-Darrieus VAWT: experimental and numerical analysis. In: Proceedings of the ASME Turbo Expo, pp. 6–10.

4. Critzos, C., Heyson, H., Boswinkle, R., 1955. Aerodynamic Characteristics of NACA 0012 Airfoil Section at Angles of Attack from 0 to 180 Degrees. Technical Report TN 3361, NACA.

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