Lift improvements using duty-cycled plasma actuation at low Reynolds numbers

[1]  T. Mueller,et al.  Experimental Studies of Separation on a Two-Dimensional Airfoil at Low Reynolds Numbers , 1982 .

[2]  D. J. Mckinzie,et al.  Control of laminar separation over airfoils by acoustic excitation , 1989 .

[3]  John W. Rutherford,et al.  Low-speed wind tunnel test results of the Canard Rotor/Wing concept , 1993 .

[4]  John W. Rutherford,et al.  Sizing Methodology for Reaction-Driven, Stopped-Rotor Vertical Takeoff and Landing Concepts , 1995 .

[5]  Andy P. Broeren,et al.  Summary of Low-Speed Airfoil Data - Vol. 3 , 1996 .

[6]  John W. Rutherford,et al.  Fixed-wing performance predictions of the Canard rotor/wing concept based on wind tunnel test results , 1995 .

[7]  Laura L. Pauley,et al.  Low-Reynolds-number separation on an airfoil , 1996 .

[8]  Clark A. Mitchell,et al.  The Canard Rotor Wing (CRW) Aircraft - A New Way to Fly , 2003 .

[9]  Michael S. Selig,et al.  Surface Oil Flow Measurements on Several Airfoils at Low Reynolds Numbers , 2003 .

[10]  Aerodynamic Characteristics of an Elliptic Airfoil at Low Reynolds Number , 2005 .

[11]  C. Tropea,et al.  Experimental transition delay using glow-discharge plasma actuators , 2007 .

[12]  Eric Moreau,et al.  Airflow control by non-thermal plasma actuators , 2007 .

[13]  Martiqua L. Post,et al.  Scaling Effects of an Aerodynamic Plasma Actuator , 2007 .

[14]  Martiqua L. Post,et al.  Single-Dielectric Barrier Discharge Plasma Enhanced Aerodynamics: Concepts, Optimization, and Applications , 2008 .

[15]  Hui Hu,et al.  An Experimental Study of the Laminar Flow Separation on a Low-Reynolds-Number Airfoil , 2008 .

[16]  Kwing-So Choi,et al.  Flow control around a circular cylinder using pulsed dielectric barrier discharge surface plasma , 2009 .

[17]  M. Samimy,et al.  High-lift airfoil trailing edge separation control using a single dielectric barrier discharge plasma actuator , 2010 .

[18]  R. M. Rennie,et al.  Lift Enhancement by Plasma Actuators at Low Reynolds Numbers , 2010 .

[19]  Jinjun Wang,et al.  Technical Notes Experimental Study of Plasma Flow Control on Highly Swept Delta Wing , 2010 .

[20]  M. Samimy,et al.  High-lift airfoil separation with dielectric barrier discharge plasma actuation , 2010 .

[21]  Fathi Finaish,et al.  Active Flow Control Strategy of Laminar Separation Bubbles Developed over Subsonic Airfoils at Low Reynolds Numbers , 2011 .

[22]  L. Traub Experimental Investigation of the Effect of Trip Strips at Low Reynolds Number , 2011 .

[23]  F. Liu,et al.  PIV Study on Steady and Periodic-Pulsed Dielectric-Barrier-Discharges , 2011 .

[24]  Subrata Roy,et al.  Enhancement of Lift and Drag Characteristics of an Oscillating Airfoil in Deep Dynamic Stall Using Plasma Actuation , 2012 .

[25]  D. Keith Walters,et al.  Prediction of Aerodynamic Characteristics for Elliptic Airfoils in Unmanned Aerial Vehicle Applications , 2012 .

[26]  J. Little,et al.  Mixing Layer Excitation by Dielectric Barrier Discharge Plasma Actuators , 2012 .

[27]  L. Shijun,et al.  PIV study of conical forebody flow control using plasma actuators , 2013 .

[28]  Jeffrey P. Bons,et al.  Active Control of Flow Separation on a Laminar Airfoil , 2013 .

[29]  Jeffrey P. Bons,et al.  Pulsed Jets Laminar Separation Control Using Instability Exploitation , 2014 .

[30]  B. Peng,et al.  Study about the non-linear and unsteady laminar separation phenomena around the airfoil at low reynolds number with low incidence , 2015 .

[31]  Lihao Feng,et al.  Flow control over an airfoil using virtual Gurney flaps , 2015, Journal of Fluid Mechanics.

[32]  Taku Nonomura,et al.  Multifactorial Effects of Operating Conditions of Dielectric-Barrier-Discharge Plasma Actuator on Laminar-Separated-Flow Control , 2015 .

[33]  C. Wen,et al.  Asymmetric Flow Control on a Delta Wing with Dielectric Barrier Discharge Actuators , 2016 .

[34]  C. Wen,et al.  Leading edge vortex control on a delta wing with dielectric barrier discharge plasma actuators , 2017 .

[35]  B. Peng,et al.  Low Reynolds Number Aerodynamic Characteristics of Near Space Solar Unmanned Aerial Vehicle , 2017 .