A discrete-vortex model for the arbitrary motion of a thin airfoil with fluidic control-Reference-Cited by-同舟云学术

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A discrete-vortex model for the arbitrary motion of a thin airfoil with fluidic control

Published:2011-07 Issue:5-6 Volume:27 Page:680-693
ISSN:0889-9746
Container-title:Journal of Fluids and Structures
language:en
Short-container-title:Journal of Fluids and Structures

Author:

Tchieu Andrew A.,Leonard Anthony

Publisher

Elsevier BV

Subject

Mechanical Engineering

Reference32 articles.

1. Theory of Wing Sections;Abbott,1959

2. Aeroelasticity;Bisplinghoff,1955

3. Effect of leading-edge separation on the lift of a delta-wing;Brown;Journal of the Aeronautical Sciences,1954

4. Brzozowski, D., Glezer, A., 2009. Rapid modification of the flow field about a free moving airfoil by controlled, trapped vorticity concentrations. In: 5th AIAA Flow Control Conference.

5. Remarks on nonlinear lift and vortex separation;Cheng;Journal of the Aeronautical Sciences,1954

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