Low Reynolds number airfoil aerodynamic loads determination via line integral of velocity obtained with particle image velocimetry-Reference-Cited by-同舟云学术

Low Reynolds number airfoil aerodynamic loads determination via line integral of velocity obtained with particle image velocimetry

Published:2012-07-22 Issue:5 Volume:53 Page:1177-1190
ISSN:0723-4864
Container-title:Experiments in Fluids
language:en
Short-container-title:Exp Fluids

Author:

Lee T.,Su Y. Y.

Publisher

Springer Science and Business Media LLC

Subject

Fluid Flow and Transfer Processes,General Physics and Astronomy,Mechanics of Materials,Computational Mechanics

Link

http://link.springer.com/content/pdf/10.1007/s00348-012-1353-x.pdf

Reference25 articles.

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3. Bhagwat MJ, Leishman JG (2000) Measurement of bound and wake circulation on a helicopter rotor. J Aircraft 37:227–234

4. Crabtree LF (1957) Effect of leading edge separation on thin wings in two-dimensional incompressible flow. J Aeronau Sci 24(8):597–604

5. Gerontakos P, Lee T (2008) PIV analysis of flow around unsteady airfoils with dynamically trailing-edge flap deflection. Exp Fluids 45(6):955–972

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