Wake of a Lifting Wing with Cut-In Sinusoidal Trailing Edges-Reference-Cited by-同舟云学术

Wake of a Lifting Wing with Cut-In Sinusoidal Trailing Edges

Published:2017-05 Issue:5 Volume:55 Page:1590-1601
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Prigent S. L.¹,Buxton O. R. H.¹,Bruce P. J. K.¹

Affiliation:

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

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J055068

Reference20 articles.

1. SmithH. A.SchaeferR. F. “Aerodynamic Characteristics at Reynolds Numbers of 3.0×106 and 6.0×106 of Three Airfoil Sections Formed by Cutting Off Various Amounts from the Rear Portion of the NACA 0012 Airfoil Section,” NACA TN-2074, 1950.

2. HoernerS. F.BorstH. V. “Fluid-Dynamic Lift: Practical Information on Aerodynamic and Hydrodynamic Lift,” NASA Scientific and Technical Information/Recon TR A 76, 1975, p. 32,167.

3. Experimental research on blunt trailing-edge airfoil sections at low Reynolds numbers

4. Aerodynamic Analysis of Blunt Trailing Edge Airfoils

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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