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  • Book
  • © 2009

Theory of Adaptive Fiber Composites

From Piezoelectric Material Behavior to Dynamics of Rotating Structures

Authors:

  • Thorough, systematic treatment of theory with several innovations and improvements
  • Detailed examination and extension of applicable variational principles
  • Complete modeling from the continuum via fiber composite, laminated shell, and thin-walled beam to the rotating structure
  • Consistent derivation of analytic as well as numeric solutions for the static respectively dynamic behavior of the non-rotating and rotating structure

Part of the book series: Solid Mechanics and Its Applications (SMIA, volume 161)

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Table of contents (11 chapters)

  1. Front Matter

    Pages i-xviii
  2. Introduction

    • T. H. Brockmann
    Pages 1-3
  3. Helicopter Applications

    • T. H. Brockmann
    Pages 5-18
  4. Fundamental Considerations

    • T. H. Brockmann
    Pages 19-40
  5. Piezoelectric Materials

    • T. H. Brockmann
    Pages 41-67
  6. Piezoelectric Composites

    • T. H. Brockmann
    Pages 69-98
  7. Adaptive Laminated Composite Shells

    • T. H. Brockmann
    Pages 99-113
  8. Adaptive Thin-Walled Beams

    • T. H. Brockmann
    Pages 115-138
  9. Virtual Work Statements

    • T. H. Brockmann
    Pages 139-154
  10. Solution Variants

    • T. H. Brockmann
    Pages 155-168
  11. Demonstration and Validation

    • T. H. Brockmann
    Pages 169-198
  12. Conclusion

    • T. H. Brockmann
    Pages 199-201
  13. Back Matter

    Pages 203-219

About this book

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 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 shall be illuminated in the work at hand from the examination of the material behavior to the simulation of the rotating structure.

Bibliographic Information

Buy it now

Buying options

eBook USD 84.99
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book USD 109.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info
Hardcover Book USD 109.99
Price excludes VAT (USA)
  • Durable hardcover edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info

Tax calculation will be finalised at checkout

Other ways to access