Add to ORKGInvestigate the feasibility of using piezoelectric sensors/actuators for subscale GEnx composite fan blade damping at target modes
L’objet de cette thèse est d’étudier différents dispositifs d’amortissement de vibrations en basses ...
Vibration control of rotating composite blade beam with piezoelectric patch embedded is investigated...
International audienceDynamics of gas-turbine blades are particularly aero-elastic coupling sensitiv...
Excessive vibration of turbomachinery blades causes high cycle fatigue problems which require dampin...
The NASA Glenn Research Center (GRC) is developing an active damping at blade resonances using piezo...
This thesis concerns the vibration reduction in the low frequency range of a composite fan blade of ...
Cette thèse CIFRE (Conventions Industrielles de Formation par la REcherche), en collaboration avec S...
Vibrations in modern machines such as cars, airplanes and bridges constitute a real issue that can c...
Vibratory loads in helicopters arise from a variety of sources such as the main rotor system, the ae...
Exploiting the properties of piezoelectric materials to minimize vibration in rotor-blade actuators,...
The problem of vibration has limited the use of helicopters in both civil and military applications....
A novel mechanism called the vibration ring is being developed to enable energy conversion elements ...
Vibration of helicopter have different sources, such as the rotor, engine and transmission system. T...
The push for low cost and higher performance/efficient turbine engines have introduced a new demand ...
Gas turbine engines are currently being designed to have increased performance, lower weight and man...
L’objet de cette thèse est d’étudier différents dispositifs d’amortissement de vibrations en basses ...
Vibration control of rotating composite blade beam with piezoelectric patch embedded is investigated...
International audienceDynamics of gas-turbine blades are particularly aero-elastic coupling sensitiv...
Excessive vibration of turbomachinery blades causes high cycle fatigue problems which require dampin...
The NASA Glenn Research Center (GRC) is developing an active damping at blade resonances using piezo...
This thesis concerns the vibration reduction in the low frequency range of a composite fan blade of ...
Cette thèse CIFRE (Conventions Industrielles de Formation par la REcherche), en collaboration avec S...
Vibrations in modern machines such as cars, airplanes and bridges constitute a real issue that can c...
Vibratory loads in helicopters arise from a variety of sources such as the main rotor system, the ae...
Exploiting the properties of piezoelectric materials to minimize vibration in rotor-blade actuators,...
The problem of vibration has limited the use of helicopters in both civil and military applications....
A novel mechanism called the vibration ring is being developed to enable energy conversion elements ...
Vibration of helicopter have different sources, such as the rotor, engine and transmission system. T...
The push for low cost and higher performance/efficient turbine engines have introduced a new demand ...
Gas turbine engines are currently being designed to have increased performance, lower weight and man...
L’objet de cette thèse est d’étudier différents dispositifs d’amortissement de vibrations en basses ...
Vibration control of rotating composite blade beam with piezoelectric patch embedded is investigated...
International audienceDynamics of gas-turbine blades are particularly aero-elastic coupling sensitiv...