Reynolds Number Effects on Unsteady Boundary Layer of an Oscillating Airfoil-Reference-Cited by-同舟云学术

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Reynolds Number Effects on Unsteady Boundary Layer of an Oscillating Airfoil

Published:2009-06-14 Issue: Volume: Page:
ISSN:
Container-title:27th AIAA Applied Aerodynamics Conference
language:
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Author:

Kim Dong-Ha¹,Chang Jo-Won¹

Affiliation:

1. Korea Aerospace University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-3501

Reference32 articles.

1. The 1976 Freeman Scholar Lecture: Some Current Research in Unsteady Fluid Dynamics

2. Unsteady Airfoils

3. Unsteady Viscous Flow on Oscillating Airfoils

4. 4Pascazio, M., Autric, J.M., Favier, D. and Maresca, C. "Unsteady Boundary-Layer Measurement on Oscillating Airfoils:Transition andSeparation Phenomena inPitchingMotion,"AIAAPaper96-0035.

5. 5Carta, F. O. A. "Comparison of the Pitching and Plunging Response of an Oscillating Airfoil," NACAContractor Report3172,1979.

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Visualization study on vortex structure over an airfoil using planar laser induced fluorescence;Spectroscopy Letters;2018-08-09

2. Experimental study of the boundary layer over an airfoil in plunging motion;Acta Mechanica Sinica;2012-04

3. Unsteady wake measurements behind an airfoil and prediction of dynamic stall from the wake;Aircraft Engineering and Aerospace Technology;2010-07-06

4. Unsteady boundary layer for a pitching airfoil at low Reynolds numbers;Journal of Mechanical Science and Technology;2010-01

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