Dynamic stall experiments on the NACA 23012 aerofoil

Author:

Leishman J. G.

Publisher

Springer Science and Business Media LLC

Subject

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

Reference21 articles.

1. Abbott, I. H.; Doenhoff, A. E. von 1959: Theory of wing sections including a summary of airfoil data. New York: Dover

2. Abbott, I. H.; Doenhoff, A. E. von; Stivers, L. S. 1945: A summary of airfoil data. NACA Report No. 824

3. Althaus, D.; Wortmann, F. X. 1981: Stuttgarter Profilkatalog 1. Experimental results from the laminar wind tunnel of the Institut für Aero und Gasdynamik der Universität Stuttgart. Braunschweig: Vieweg

4. Bisplinghoff, R. L.; Ashley, H.; Halfman, R. L. 1955: Aeroelasticity. Addison-Wesley, Cambridge/MA

5. Carr, L. W.; McAlister, K. W.; McCroskey, W. J. 1977: Analysis of the development of dynamic stall based on oscillating airfoil experiments. NASA TN D-8382

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