Aerothermoelastic Analysis of Cylindrical Piezolaminated Shells Based on Multi-field Layerwise Theory |
Oh, Il-Kwon
(LG전자 DA연구소)
Shin, Won-Ho (한국과학기술원 기계공학과 항공우주공학전공) Lee, In (한국과학기술원 기계공학과 항공우주공학전공) |
1 |
Postbuckling and Vibration Characteristics of Piezolaminated Composite Plate Subject to Thermopiezoelectric Loads
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DOI ScienceOn |
2 |
Adaptive Composites Modelling and Applications in Panel Flutter and Noise Suppression
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DOI |
3 |
Enhancement of Pre-buckling Behavior of Composite Beams with Geomatric Imperfections using Piezoelectric Actuators
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DOI ScienceOn |
4 |
Controlling Panel Flutter using Adaptive Materials
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DOI ScienceOn |
5 |
Thermal Snapping and Vibration Characteristics of Cylindrical Composite Panels Using Layerwise Theory
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DOI ScienceOn |
6 |
Buckling Control of a Flexible Bean Using Piezoelectric Actuators
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DOI ScienceOn |
7 |
The Active Buckling Control of Some Composite Columm Strips Using Piezoceramic Actuators
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DOI ScienceOn |
8 |
Thermopiezoelastic Snapping of Piezolaminated Plates Using Layerwise Nonlinear Finite Elements
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DOI ScienceOn |
9 |
Active Control of Panel Flutter with Piezoelectric Transducers
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DOI ScienceOn |
10 |
Layerwise Mechanics and Finite Element Model for Laminated Piezoelectric Shells
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DOI ScienceOn |
11 |
Active Panel Flutter Suppression Using Self-Sensing Piezoactuators
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DOI ScienceOn |
12 |
Suppression of Nonlinear Panel Flutter at Elevated Temperature with Piezoelectric Actuators
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DOI ScienceOn |
13 |
Mixed Laminated Theory and Finite Element for Smart Piezoelectric Composite Shell Structures
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DOI ScienceOn |
14 |
Static Aeroelastic Behavior of an Adaptive Laminated Piezoelectric Composite Wing
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15 |
The Accuracy of Linear Piston Theory When Applied to Cylindrical Shells
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DOI |
16 |
Application of Adaptive Technology to Static Aeroelastic Control of Wing Structures
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DOI |
17 |
Toward Optimal Aeroelastic Control Using Elastic and Induced Strain Anisotropy
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