Experimental study of the boundary layer over an airfoil in plunging motion
Author:
Publisher
Springer Science and Business Media LLC
Subject
Mechanical Engineering,Computational Mechanics
Link
http://link.springer.com/content/pdf/10.1007/s10409-012-0039-1.pdf
Reference18 articles.
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2. Pascazio, M., Autric, J.M., Favier, D., et al.: Unsteady boundary-layer measurement on oscillating airfoils, transition and separation phenomena in pitching motion. AIAA-96-0035, 34th Aerospace Sciences Meeting and Exhibit, Reno, NV (1996)
3. Schreck, S., Faller, W.E., Helin, H.E.: Pitch rate and Reynolds number effects on unsteady boundary-layer transition and separation. Journal of Aircraft, 35, 46–52 (1998)
4. Lee, T., Basu, S.: Measurement of unsteady boundary layer developed on an oscillating airfoil using multiple hot-film sensors. Experiments in Fluids, 25, 108–117 (1998)
5. Brodeur, R., van Dam, C.P.: Transition prediction for a twodimensional Navier-Stokes solver applied to wind-turbine airfoils. AIAA-2000-0047 (2000)
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