Advanced topics of thin-walled structures /

Bibliographic Details
Main Author:	Abramovits, Ḥayim, Dr (Author)
Corporate Author:	World Scientific (Firm)
Format:	eBook
Language:	English
Published:	Singapore ; Hackensack, NJ : World Scientific Publishing Co. Pte. Ltd., [2021]
Subjects:	Thin-walled structures. Composite materials. Airframes. Electronic books.
Online Access:	Connect to the full text of this electronic book

Table of Contents:

2.2. Unidirectional Composites
2.3. Properties of a Single Ply
2.4. Transformation of Stresses and Strains
2.5. Classical Lamination Theory
2.6. First-Order Shear Deformation Theory
2.7. Higher Order Theories
References
3. Buckling of Thin-Walled Structures
3.1. Introduction
3.2. Buckling of Columns
3.2.1. Euler buckling
3.2.2. Rankin-Gordon formula
3.2.3. Composite columns
CLT approach
3.2.3.1. Symmetric laminate (B11 = 0)
3.2.4. Non-symmetric laminate (B11 = 0)
3.4. Buckling of Columns: FSDT Approach
3.5. Buckling of Plates
3.5.1. Buckling of isotropic plates
3.5.2. Buckling of orthotropic plates
3.6. Buckling of Shells
3.6.1. Introduction to shells
3.6.2. Buckling of isotropic cylindrical shells
3.6.2.1. Axial compression
3.6.2.2. External pressure
3.6.2.3. Torsion
3.6.2.4. Combined loadings
3.6.2.5. Buckling of orthotropic cylindrical shells under axial compression
3.6.2.6. Buckling of orthotropic cylindrical shells under external pressure
3.6.2.7. Buckling of orthotropic cylindrical shells under torsion
3.6.2.8. Combined bending and axial compression of orthotropic cylindrical shells
References
Appendix A: Non-symmetric Laminated Composite Beam
CLT Approach
Appendix B: Energy Methods
References
4. Vibrations of Thin-Walled Structures
4.1. Introduction
4.2. CLPT Approach
4.3. FSDPT Approach
4.4. Vibrations of Columns
CLT Approach
4.4.1. Symmetric laminate (B11 = 0, I1 = 0)
4.4.2. Non-symmetric laminate (B11 = 0, I1 = 0)
4.5. Vibrations of Columns
FSDT Approach
4.5.1. Symmetric laminate (B11 = 0, I1 = 0)
4.5.2. Non-symmetric laminate (B11 = 0, I1 = 0)Following the derivation performed by Abramovich and Livshits
4.5.2. Non-symmetric laminate (B11 = 0, I1 = 0)
4.6. Vibrations of Plates
CLT Approach
4.6.1. Simply supported special orthotropic plates
4.6.2. Simply supported on two opposite edges of special orthotropic plates
4.7. Vibration of Cylindrical Shells
4.7.1. Isotropic shells
4.7.2. Soedel theory
4.8. Laminated Composite Shells
CLT Approach
References
Appendix A: General Solution for a Nonsymmetrical Beam Resting on any Boundary Conditions