Integral Twist Actuation of Helicopter Rotor Blades for Vibration Reduction

Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2001.

[1]  O. Bauchau Computational Schemes for Flexible, Nonlinear Multi-Body Systems , 1998 .

[2]  Robert A. Ormiston,et al.  Hover Testing of a Small-Scale Rotor with On-Blade Elevons , 2001 .

[3]  Paul H. Mirick,et al.  Low-cost piezocomposite actuator for structural control applications , 2000, Smart Structures.

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

[5]  Du Plessis,et al.  Modeling and experimental testing of twist actuated single cell composite beams for helicopter blade control , 1996 .

[6]  William Keats Wilkie Anisotropic piezoelectric twist actuation of helicopter rotor blades: Aeroelastic analysis and design optimization , 1997 .

[7]  Ronald L. Spangler,et al.  Piezoelectric actuators for helicopter rotor control , 1989 .

[8]  Carlos E. S. Cesnik,et al.  Active composite beam cross-sectional modeling - Stiffness and active force constants , 1999 .

[9]  Richard L. Bielawa,et al.  Rotary wing structural dynamics and aeroelasticity , 1992 .

[10]  Robert G. Loewy,et al.  Helicopter Vibrations: A Technological Perspective , 1984 .

[11]  G. A. Pierce,et al.  Helicopter vibration suppression using simple pendulum absorbers on the rotor blade , 1984 .

[12]  Wilkie W. Keats,et al.  Aeroelastic Analysis of the NASA/ARMY/MIT Active Twist Rotor , 1999 .

[13]  Victor Giurgiutiu,et al.  RECENT ADVANCES IN SMART-MATERIAL ROTOR CONTROL ACTUATION. , 2000 .

[14]  Inderjit Chopra,et al.  Feasibility study to build a smart rotor: induced-strain actuation of airfoil twisting using piezoceramic crystals , 1993, Smart Structures.

[15]  Carlos E. S. Cesnik,et al.  On a simplified strain energy function for geometrically nonlinear behaviour of anisotropic beams , 1991 .

[16]  N. Hagood,et al.  Piezoelectric Fiber Composites with Interdigitated Electrodes , 1997 .

[17]  Xiaoyang Shang,et al.  Aeroelastic stability of composite rotor blades in hover , 1995 .

[18]  Bo Ping Wang,et al.  Helicopter Vibration Reduction by Local Structural Modification , 1982 .

[19]  David A. Peters,et al.  Finite state induced flow models. II - Three-dimensional rotor disk , 1995 .