Effects of Blockage on Airfoils and Wings at High Angles of Attack-Reference-Cited by-同舟云学术

Effects of Blockage on Airfoils and Wings at High Angles of Attack

Published:2015-05 Issue:3 Volume:52 Page:990-993
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Traub Lance W.¹

Affiliation:

1. Aerospace and Mechanical Engineering Department, Embry-Riddle Aeronautical University, Prescott, Arizona 86301

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C033119

Reference15 articles.

1. WenzingerC. J.HarrisT. A. “Wind Tunnel Force Tests in Wing Systems Through Large Angles of Attack,” NACA Rept. 294, Aug. 1928.

2. PopeA. “The Forces and Pressures over an NACA 0015 Airfoil Through 180 Degrees Angle of Attack,” Georgia Inst. of Technology TR-E-102, Atlanta, 1947.

3. WickB. H. “Study of the Subsonic Forces and Moments on an Inclined Plate of Infinite Span,” NACA TN-3221, June 1954.

4. CritzosC. C.HeysonH. H.BoswinkleR. W. “Aerodynamic Characteristics of NACA 0012 Airfoil Section at Angles of Attack from 0 Deg to 180 Deg,” NACA TN-3361, Jan. 1955.

5. RamsayR. R.JaniszewskaJ. M.GregorekG. M. “Wind Tunnel Testing of Three S809 Aileron Configurations for Use on Horizontal Axis Wind Turbines,” Ohio State Univ., Airfoil Performance Rept., Columbus, OH, July 1996.

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