A Parametric Design Study for a Swashplateless Helicopter Rotor with Trailing-Edge Flaps

[1]  Robert A. Ormiston,et al.  Aeroelastic Considerations For Rotorcraft Primary Control with On-Blade Elevons , 2001 .

[2]  Fu-Shang Wei,et al.  Correlation and analysis for SH-2F 101 rotor , 1988 .

[3]  Inderjit Chopra,et al.  Wind tunnel testing of a Mach-scaled rotor model with trailing-edge flaps , 2000 .

[4]  Theodore Theodorsen,et al.  Nonstationary flow about a wing-aileron-tab combination including aerodynamic balance , 1942 .

[5]  S. Hoerner.  Fluid-Dynamic Lift , 1985 .

[6]  Inderjit Chopra,et al.  Wind Tunnel Testing of a Smart Rotor Model with Trailing-Edge Flaps , 2002 .

[7]  Fu-Shang Wei,et al.  Servo-Flap Rotor Performance Flight Testing And Data Identification , 2001 .

[8]  Friedrich K. Straub,et al.  Rotors with Trailing Edge Flaps: Analysis and Comparison with Experimental Data , 1998 .

[9]  Peretz P. Friedmann,et al.  Vibration reduction in helicopter rotors using an actively controlled partial span trailing edge flap located on the blade , 1994 .

[10]  Jinwei Shen,et al.  AEROELASTIC STABILITY OF SMART TRAILING-EDGE FLAP HELICOPTER ROTORS , 2001 .

[11]  Inderjit Chopra,et al.  Aeroelastic modeling of trailing-edge flaps with smart material actuators , 2000 .

[12]  Friedrich K. Straub,et al.  Aeroelastic Analysis of Rotors with Trailing Edge Flaps Using Comprehensive Codes , 2001 .

[13]  J. Gordon Leishman,et al.  Principles of Helicopter Aerodynamics , 2000 .

[14]  Inderjit Chopra,et al.  Actuation Requirements for a Swashplateless Helicopter Control System , 2002 .

[15]  Inderjit Chopra,et al.  Status of Application of Smart Structures Technology to Rotorcraft Systems , 2000 .