Control Application of Piezoelectric Materials to Aeroelastic Self-Excited Vibrations
A method for application of piezoelectric materials to aeroelasticity of turbomachinery blades is presented. The governing differential equations of an overhung beam are established. The induced voltage in attached piezoelectric sensors due to the strain of the beam is calculated. In aeroelastic sel...
Saved in:
Main Authors: | Mohammad Amin Rashidifar, Darvish Ahmadi |
---|---|
Format: | Article |
Language: | English |
Published: |
Wiley
2014-01-01
|
Series: | Shock and Vibration |
Online Access: | http://dx.doi.org/10.1155/2014/509024 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Aeroelastic Dynamic Response and Control of an Aeroelastic System with Hysteresis Nonlinearities
by: Xingzhi Xu, et al.
Published: (2015-01-01) -
Aeroelastic Vibrations and Stability in Cyclic Symmetric Domains
by: Bernard Lalanne, et al.
Published: (2000-01-01) -
ANALYSIS ON MAGNETO-AEROELASTIC TRANSVERSE VIBRATION OF ROTATING CONDUCTIVE CIRCULAR PLATE
by: HU YuDa, et al.
Published: (2018-01-01) -
Feedforward Control of Gear Mesh Vibration Using Piezoelectric Actuators
by: Gerald T. Montague, et al.
Published: (1994-01-01) -
Aeroelasticity in Turbomachines: Some Aspects of the Effect of Coupling Modeling and Blade Material Changes
by: François Moyroud, et al.
Published: (2000-01-01)