A Comparison Between Boundary Layer Measurements in a Laminar Separation Bubble Flow and Linear Stability Theory Calculations

Author:

LeBlanc P.,Blackwelder R.,Liebeck R.

Publisher

Springer Berlin Heidelberg

Reference14 articles.

1. P. J. LeBlanc, R. H. Liebeck, and R. Blackwelder. Boundary layer and performance characteristics from wind tunnel tests of a low Reynolds number Liebeck airfoil. In Aerodynamics at Low Reynolds Numbers,pages 8.1–8.19, London, Oct. 1986. The Royal Aeronautical Society.

2. K. B. Zaman, A. Bar-Sever, and S. M. Mangalam. Effect of acoustic excitation on the flow over a low-Re airfoil. Journal of Fluid Mechanics, 182: 127–148, 1987.

3. C. F. Liu. Control of Airfoil Performance by Local Excitation. PhD thesis, National Cheng Kung University, Tainan, Taiwan, October 1988.

4. J. L. van Ingen and L. M. M. Boermans. Aerodynamics at low Reynolds numbers: A review of theoretical and experimental research at Delft University of Technology. In Aerodynamics at Low Reynolds Numbers,pages 1.1–1.40, London, Oct. 1986. The Royal Aeronautical Society.

5. D. E. Gault. An experimental investigation of regions of separated laminar flow. Technical report, NACA TN 3505, Sept. 1955.

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