Dynamic Deployment of a Minitab for Aerodynamic Load Control
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[1] I. Gursul,et al. An Experimental Study of Mini-Tabs for Aerodynamic Load Control , 2016 .
[2] Li Liu,et al. Computational Study of Microflaps with Application to Vibration Reduction in Helicopter Rotors , 2011 .
[3] R. E. Kalman,et al. A New Approach to Linear Filtering and Prediction Problems , 2002 .
[4] Israel J Wygnanski,et al. Active management of naturally separated flow over a solid surface. Part 1. The forced reattachment process , 2004, Journal of Fluid Mechanics.
[5] L. C. Woods. The theory of subsonic plane flow , 1961 .
[6] I. Gursul,et al. Unsteady Lift and Moment of a Periodically Plunging Airfoil , 2019, AIAA Journal.
[7] D. W. Holder,et al. Wind-tunnel technique : an account of experimental methods in low- and high-speed wind tunnels , 1952 .
[8] Hak-Tae Lee,et al. Computational Investigation of Airfoils with Miniature Trailing Edge Control Surfaces , 2004 .
[9] T. Theodorsen. General Theory of Aerodynamic Instability and the Mechanism of Flutter , 1934 .
[10] Ilan Kroo,et al. Flutter Suppression Using Micro-Trailing Edge Effectors , 2003 .
[11] Earl P. N. Duque,et al. Numerical Investigation on the Aerodynamics of Oscillating Airfoils with Deployable Gurney Flaps , 2010 .
[12] Alan Pope,et al. Wind-tunnel testing , 1947 .
[13] William H. Rae,et al. Low-Speed Wind Tunnel Testing , 1966 .
[14] Earl H. Dowell,et al. Aerodynamic Loading for an Airfoil with an Oscillating Gurney Flap , 2007 .
[15] David G. Wilson,et al. Optimized Active Aerodynamic Blade Control for Load Alleviation on Large Wind Turbines , 2008 .
[16] I. Gursul,et al. Aerodynamic Load Alleviation Using Minitabs , 2018, Journal of Aircraft.
[17] Tianshu Liu,et al. Thin-Airfoil Theoretical Interpretation for Gurney Flap Lift Enhancement , 2007 .
[18] Pavlos P. Vlachos,et al. Estimation of uncertainty bounds for individual particle image velocimetry measurements from cross-correlation peak ratio , 2013 .
[19] Jose Palacios,et al. Active Gurney Flaps: Their Application in a Rotor Blade Centrifugal Field , 2014 .
[20] James G. Coder,et al. CFD Investigation of Unsteady Rotorcraft Airfoil Aerodynamics: MiTEs and Dynamic Stall , 2011 .
[21] Eastman N. Jacobs,et al. Airfoil section characteristics as affected by variations of the Reynolds number , 1939 .
[22] Robert J. Moffat,et al. Describing the Uncertainties in Experimental Results , 1988 .
[23] Mark D. Maughmer,et al. Unsteady Aerodynamic Model for Deployable Gurney Flaps Based on Indicial Concepts , 2017 .
[24] Alena Berit Bach,et al. Gurney flaps and micro-tabs for load control on wind turbines , 2016 .
[25] Lakshmi N. Sankar,et al. Aerodynamic Evaluation of Miniature Trailing-Edge Effectors for Active Rotor Control , 2010 .
[26] Scott J. Johnson,et al. An Innovative Design of a Microtab Deployment Mechanism for Active Aerodynamic Load Control , 2015 .
[27] Nader H. Al-Battal,et al. Lift reduction by counter flowing wall jets , 2018, Aerospace Science and Technology.
[28] Magda Osman,et al. Control Systems Engineering , 2010 .
[29] Jinjun Wang,et al. Influences of Mounting Angles and Locations on the Effects of Gurney Flaps , 2003 .
[30] R. Stengel,et al. CONTROL systems. , 1952, Hospitals.
[31] Israel J Wygnanski,et al. Active management of naturally separated flow over a solid surface. Part 2. The separation process , 2004, Journal of Fluid Mechanics.
[32] Christian Oliver Paschereit,et al. Experimental Investigation of the Aerodynamic Lift Response of an Active Finite Gurney Flap , 2015 .
[33] R. T. Jones. The unsteady lift of a wing of finite aspect ratio , 1940 .
[35] Raymond Chow,et al. Unsteady Computational Investigations of Deploying Load Control Microtabs , 2006 .