Computational aeroelastic analysis of a hovering W3 Sokol blade with gurney flap
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George N. Barakos | Vasileios Pastrikakis | Rene Steijl | J. Małecki | G. Barakos | R. Steijl | J. Małecki | V. Pastrikakis
[1] Sudhir L. Gai,et al. Influence of Trailing-Edge Flow Control on Airfoil Performance , 2003 .
[2] F. Dehaeze,et al. Hovering rotor computations using an aeroelastic blade model , 2012 .
[3] Mark D. Maughmer,et al. Experimental Investigation of Gurney Flaps , 2008 .
[4] Lakshmi N. Sankar,et al. Computational Investigation of Gurney Flap Effects on Rotors in Forward Flight , 2009 .
[5] Tim Lee,et al. Lift enhancement and flow structure of airfoil with joint trailing-edge flap and Gurney flap , 2011 .
[6] Hyeonsoo Yeo,et al. Assessment of Active Controls for Rotor Performance Enhancement , 2008 .
[7] Stanley Osher,et al. Upwind schemes and boundary conditions with applications to Euler equations in general geometries , 1983 .
[8] Earl P. N. Duque,et al. Numerical Investigation on the Aerodynamics of Oscillating Airfoils with Deployable Gurney Flaps , 2010 .
[9] Farhan Gandhi,et al. Upstream Active Gurney Flap for Rotorcraft Vibration Reduction , 2012 .
[10] Jinjun Wang,et al. Gurney flap—Lift enhancement, mechanisms and applications , 2008 .
[11] George N. Barakos,et al. CFD Method for Efficient Analysis of Flapped Rotors , 2010 .
[12] David W. Hurst,et al. Aerodynamics of Gurney Flaps on a Single-Element High-Lift Wing , 2000 .
[13] George N. Barakos,et al. Aeroelastic CFD computations for rotor flows , 2011 .
[14] C. Keys,et al. Effect of twist on helicopter performance and vibratory loads , 1987 .
[15] Sikorsky Aircraft Corp.,et al. Rotor Aeromechanics Results from the Sikorsky Active Flap Demonstration Rotor , 2012 .
[16] Ranjan Ganguli,et al. An optimization approach to vibration reduction in helicopter rotors with multiple active trailing edge flaps , 2004 .
[17] George N. Barakos,et al. Rotor Computations with Active Gurney Flaps , 2016 .
[18] Peretz P. Friedmann,et al. Numerical Evaluation of Microflaps for On Blade Control of Noise and Vibration , 2011 .
[19] G. Barakos,et al. Sliding mesh algorithm for CFD analysis of helicopter rotor–fuselage aerodynamics , 2008 .
[20] Ken Badcock,et al. Development of CFD Capability for Full Helicopter Engineering Analysis , 2005 .
[21] George N. Barakos,et al. Mesh Deformation Method for Rotor Flows , 2012 .
[22] Kevin Standish,et al. Two-Dimensional Wind Tunnel and Computational Investigation of a Microtab Modified Airfoil , 2005 .
[23] Ken Badcock,et al. Computational study of the advancing-side lift-phase problem , 2008 .
[24] George N. Barakos,et al. Analysis and design of a Flap-Equipped Low-Twist Rotor for Hover , 2009 .
[25] Raymond Chow,et al. Unsteady Computational Investigations of Deploying Load Control Microtabs , 2006 .
[26] Roberto Celi,et al. Optimum Two-Per-Revolution Inputs for Improved Rotor Performance , 2005 .
[27] Friedrich K. Straub,et al. Rotors with Trailing Edge Flaps: Analysis and Comparison with Experimental Data , 1998 .
[28] Raymond Chow,et al. Unsteady Computational Investigations of Deploying Load Control Microtabs , 2006 .
[29] George N. Barakos,et al. A framework for CFD analysis of helicopter rotors in hover and forward flight , 2006 .
[30] C. J. Simao Ferreira,et al. Assessment of PIV-based unsteady load determination of an airfoil with actuated flap , 2014 .
[31] A. Jameson. Time dependent calculations using multigrid, with applications to unsteady flows past airfoils and wings , 1991 .
[32] Earl H. Dowell,et al. Aerodynamic Loading for an Airfoil with an Oscillating Gurney Flap , 2007 .
[33] R. Liebeck. Design of Subsonic Airfoils for High Lift , 1976 .
[34] Dong-Ho Lee,et al. Aerodynamic Performance Analysis of a Gurney Flap for Rotorcraft Application , 2007 .
[35] James D. Baeder,et al. Evaluation of a Navier-Stokes Analysis Method for Hover Performance Prediction , 1996 .
[36] P. S. Heyns. An Optimization Approach to Vibration Isolation of Rigid Bodies , 1997 .
[37] Li Liu,et al. Computational Study of Microflaps with Application to Vibration Reduction in Helicopter Rotors , 2011 .
[38] G. D. van Albada,et al. A comparative study of computational methods in cosmic gas dynamics , 1982 .
[39] Ellen K. Longmire,et al. Time resolved PIV analysis of flow over a NACA 0015 airfoil with Gurney flap , 2006 .