Theory of Adaptive Fiber Composites [electronic resource] :From Piezoelectric Material Behavior to Dynamics of Rotating Structures / by T. H. Brockmann.
by Brockmann, T. H [author.]; SpringerLink (Online service).
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BookSeries: Solid Mechanics and Its Applications: 161Publisher: Dordrecht : Springer Netherlands, 2009.Description: online resource.ISBN: 9789048124350.Subject(s): Materials | Mechanics | Engineering | Vibration | Material Science | Ceramics, Glass, Composites, Natural Methods | Continuum Mechanics and Mechanics of Materials | Vibration, Dynamical Systems, Control | Computational Intelligence | MechanicsDDC classification: 620.14 Online resources: Click here to access online | Item type | Current location | Call number | Status | Date due | Barcode |
|---|---|---|---|---|---|
| TA418.9.C6 (Browse shelf) | Available | ||||
| Long Loan | MAIN LIBRARY | TP807-823 (Browse shelf) | Available |
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| GF1-900 Enhancing the City | LC8-6691 Progressing Science Education | TA357-359 Convection in Fluids | TP807-823 Theory of Adaptive Fiber Composites | B1-5802 Plural Action | RM1-950 Drug-related problems in the elderly | RM1-950 Pharmacology and Abuse of Cocaine, Amphetamines, Ecstasy and Related Designer Drugs |
Helicopter Applications -- Fundamental Considerations -- Piezoelectric Materials -- Piezoelectric Composites -- Adaptive Laminated Composite Shells -- Adaptive Thin-Walled Beams -- Virtual Work Statements -- Solution Variants -- Demonstration and Validation -- Conclusion.
Adaptive structural systems in conjunction with multifunctional materials facilitate technical solutions with a wide spectrum of applications and a high degree of integration. By virtue of combining the actuation and sensing capabilities of piezoelectric materials with the advantages of fiber composites, the anisotropic constitutive properties may be tailored according to requirements and the failure behavior can be improved. Such adaptive fiber composites are very well-suited for the task of noise and vibration reduction. In this respect, the helicopter rotor system represents a very interesting and widely perceptible field of application. The occurring oscillations can be reduced with the aid of aerodynamic couplings via fast manipulation of the angle of attack, being induced by twist actuation of the rotor blade. On the one hand, the sensing properties may be used to determine the current state of deformation, while, on the other hand, the actuation properties may be used to attain the required state of deformation. The implementation of such concepts requires comprehensive knowledge of the theoretical context, which is illuminated in this work from the examination of the material behavior to the simulation of the rotating structure.
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