Add to ORKGThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1994.Includes bibliographical references (p. 119-123).by Eric Frederick Prechtl.M.S
Interest in the use of smart-structure technology for noise and vibration reduction in helicopter ap...
This study investigates the effect of piezoelectric actuator hysteresis on helicopter vibration cont...
This study investigates the effect of piezoelectric actuator hysteresis on helicopter vibration cont...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989.In...
Thesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2000.I...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993.In...
Master of Science in Aeronautics and Astronautics An actuator using a piezoelectric bender to de ect...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1994.Includes...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1995.In...
In this thesis, the feasibility of using blade-mounted servoflap actuation or conven-tional root pit...
An actuator using a piezoelectric bender to de ect a trailing edge servo- ap for use on a helicop...
Thesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1980.M...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1995....
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1967. M.S.Micr...
Thesis (B.S.)--Massachusetts Institute of Technology, Dept. of Aeronautical Engineering, 1954.MIT co...
Interest in the use of smart-structure technology for noise and vibration reduction in helicopter ap...
This study investigates the effect of piezoelectric actuator hysteresis on helicopter vibration cont...
This study investigates the effect of piezoelectric actuator hysteresis on helicopter vibration cont...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989.In...
Thesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2000.I...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993.In...
Master of Science in Aeronautics and Astronautics An actuator using a piezoelectric bender to de ect...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1994.Includes...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1995.In...
In this thesis, the feasibility of using blade-mounted servoflap actuation or conven-tional root pit...
An actuator using a piezoelectric bender to de ect a trailing edge servo- ap for use on a helicop...
Thesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1980.M...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1995....
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1967. M.S.Micr...
Thesis (B.S.)--Massachusetts Institute of Technology, Dept. of Aeronautical Engineering, 1954.MIT co...
Interest in the use of smart-structure technology for noise and vibration reduction in helicopter ap...
This study investigates the effect of piezoelectric actuator hysteresis on helicopter vibration cont...
This study investigates the effect of piezoelectric actuator hysteresis on helicopter vibration cont...