Vortex Shedding and Aerodynamic Performance of Airfoil with Multiscale Trailing-Edge Modifications-Reference-Cited by-同舟云学术

Vortex Shedding and Aerodynamic Performance of Airfoil with Multiscale Trailing-Edge Modifications

Published:2015-11 Issue:11 Volume:53 Page:3240-3250
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Nedić J.¹,Vassilicos J. C.¹

Affiliation:

1. Department of Aeronautics, Imperial College London, London, England SW7 2AZ, United Kingdom

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J053834

Reference25 articles.

1. SmithH. A.SchaeferR. F. “Aerodynamic Characteristics at Reynolds Numbers of 3.0×10(6) and 6.0×10(6) of Three Airfoil Sections Formed by Cutting Off Various Amounts From the Rear Portion of the NACA 0012 Airfoil Section,” NACA TR-TN-2074, 1950.

2. Aerodynamic Analysis of Blunt Trailing Edge Airfoils

3. A Method for Reducing the Base Drag of Wings with Blunt Trailing Edge

4. Base drag reduction by control of the three-dimensional unsteady vortical structures

5. Investigation of the near and far wake of a bluff airfoil model with trailing edge modifications using time-resolved particle image velocimetry

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