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Thin-Walled Composite Beams - Theory and Application

Liviu Librescu and Ohseop Song 
Springer  October 2005  



Hardcover  XXVI, 610 p.,  ISBN 1402034571      £115.50

This is the first monograph devoted to the foundation of the theory of composite anisotropic thin-walled beams and to its applications in various problems involving the aeronautical/aerospace, helicopter, naval and mechanical structures.

Throughout the theoretical part, an effort was made to provide the treatment of the subject by using the equations of the 3-D elasticity theory.

Non-classical effects such as transverse shear, warping constraint, anisotropy of constituent materials yielding the coupling of twist-bending (lateral), bending (transversal)-extension have been included and their implications have been thoroughly analyzed.

Thermal effects have been included and in order to be able to circumvent their deleterious effects, functionally graded materials have been considered in their construction.

Implications of the application of the tailoring technique and of the active feedback control on free vibration, dynamic response, instability and aeroelasticity of such structures have been amply investigated.

Special care was exercised throughout this work to address and validate the adopted solution methodologies and the obtained results against those available in the literature and obtained via numerical or experimental means.

Written for professors and graduate students in mechanical, aeronautical and aerospace engineering, applied mechanics, practicing scientists and engineers working in research in problems involving the modern theory of composite thin-walled structures; aeronautical, naval and mechanical engineers

Contents

  • Preface.
  • Introduction.
  • Kinematics of Thin Walled Beam.
  • The Equations of Motion of Open/Closed Cross-Section Beams.
  • Additional Equations of the Linear Beam Theory.
  • Several Theorems in Linear Thin-Walled Beam Theory.
  • Free Vibration
  • Dynamic Response to Time-Dependent External Excitation.
  • Thin-Walled Beams Carrying Stores.
  • Rotating Thin-Walled Anisotropic Beams.
  • Spinning Thin-Walled Anisotropic Beams.
  • Thermally Induced Vibration and Control of Spacecraft Booms.
  • Aeroelasticity of Thin-Walled Aircraft Wings
  • Open-Section Beams.
  • Appendix.- The Constitutive Equations.
  • References
  • Index
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