1. Lorber, P. F., Carta, F. O., and Covino, A. F. "An oscillating three-dimensional wing experiment: compressibility, sweep, rate, and geometry effects on unsteady separation and dynamic stall," United Technologies Research Center, Report R92-958325-6,East Hartford, Connecticut,1992. Lorber, P. F., McCormick, D. C., Wake, B., and Florea, R. "Separation Control for Rotorcraft," UTRC Final Progress Report, United Technologies Research Center, Report 2002-5.200.0015-5, EastHartford, Connecticut, 2002. Lorber, P.F., McCormick, D., Anderson, T., Wake, B., MacMartin, D., Pollack, M., Corke, T., and Breuer, K. "Rotorcraft Retreating Blade Stall Control," AIAA Paper, Fluids 2000 ConferenceandExhibit,Denver,CO,2002-2475, 2002. McCroskey, W. J., Carr, L. W., and McAlister, K. W. "Dynamic stall experiments on oscillating airfoils,"AIAA Journal,14,57-63,1976.
2. Dynamic Stall on Advanced Airfoil Sections