Add to ORKGThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1994.Includes bibliographical references (p. 163-168).by James Christopher Garcia.M.S
A comprehensive aeroelastic analytical model of helicopter rotors with trailingedge flaps for primar...
Since the author has always been interested in Aeronautical Engineering, and in particular, rotary-w...
Since the author has always been interested in Aeronautical Engineering, and in particular, rotary-w...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993.In...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1995.In...
Thesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2000.I...
An aeroelastic model of a smart rotor system (which incorporates blade-mounted trailing-edge flap ac...
An actuator using a piezoelectric bender to de ect a trailing edge servo- ap for use on a helicop...
In this thesis, the feasibility of using blade-mounted servoflap actuation or conven-tional root pit...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2001....
In an effort to develop an active control technique for reducing helicopter vibrations stemming from...
AbstractThis paper describes an electronically controlled active force control system developed to t...
Lead-lag dampers are present in most rotor systems to provide the desired level of damping for all f...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1994.In...
A simplified second-order transfer function actuator model used in most flight dynamics applications...
A comprehensive aeroelastic analytical model of helicopter rotors with trailingedge flaps for primar...
Since the author has always been interested in Aeronautical Engineering, and in particular, rotary-w...
Since the author has always been interested in Aeronautical Engineering, and in particular, rotary-w...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993.In...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1995.In...
Thesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2000.I...
An aeroelastic model of a smart rotor system (which incorporates blade-mounted trailing-edge flap ac...
An actuator using a piezoelectric bender to de ect a trailing edge servo- ap for use on a helicop...
In this thesis, the feasibility of using blade-mounted servoflap actuation or conven-tional root pit...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2001....
In an effort to develop an active control technique for reducing helicopter vibrations stemming from...
AbstractThis paper describes an electronically controlled active force control system developed to t...
Lead-lag dampers are present in most rotor systems to provide the desired level of damping for all f...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1994.In...
A simplified second-order transfer function actuator model used in most flight dynamics applications...
A comprehensive aeroelastic analytical model of helicopter rotors with trailingedge flaps for primar...
Since the author has always been interested in Aeronautical Engineering, and in particular, rotary-w...
Since the author has always been interested in Aeronautical Engineering, and in particular, rotary-w...