Paper Title:
Experimental Research on Transition and Flow Separation of Laminar Airfoil
  Abstract

Experimental research on transition and flow separation of laminar airfoil and the influence of transition and flow separation on the performance of laminar airfoil are carried through. The experimental device and instruments used in the research are introduced. It is shown from the experimental results that at certain scope of attack angle, flow transition shifts from 50%c to 30%c on the upper surface of airfoil model along with 1 degree increase of airfoil attack angle; For flow speed of 35m/s and 50m/s with attack angle from 4 degree to 8 degree, flow separation position don’t vary but only separation scope increase; For flow speed of 15m/s laminar flow separation on the upper surface of airfoil take place at attack angle of 4 degree, flow become attaching at attack angle of 6 degree and turbulent flow separation take place at attack angle of 8 degree.

  Info
Periodical
Advanced Materials Research (Volumes 301-303)
Chapter
Chapter 2: Measuring and Testing Techniques
Edited by
Riza Esa and Yanwen Wu
Pages
937-942
DOI
10.4028/www.scientific.net/AMR.301-303.937
Citation
Y. Q. Jiao, Y. Lu, C. S. Xiao, "Experimental Research on Transition and Flow Separation of Laminar Airfoil", Advanced Materials Research, Vols. 301-303, pp. 937-942, 2011
Online since
July 2011
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Price
$32.00
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