Design and analysis of composite structures : with applications to aerospace structures /

"New edition updated with additional exercises and two new chapters. Design and Analysis of Composite Structures: With Applications to Aerospace Structures, 2nd Edition builds on the first edition and includes two new chapters on composite fittings and the design of a composite panel, as well a...

Πλήρης περιγραφή

Λεπτομέρειες βιβλιογραφικής εγγραφής
Κύριος συγγραφέας: Kassapoglou, Christos
Μορφή: Ηλ. βιβλίο
Γλώσσα:English
Έκδοση: Chichester, West Sussex, United Kingdom : John Wiley & Sons Inc., 2013.
Έκδοση:Second edition.
Σειρά:Aerospace series (Chichester, England)
Θέματα:
Διαθέσιμο Online:Full Text via HEAL-Link
Πίνακας περιεχομένων:
  • Aerospace Series List; Title Page; Copyright; About the Author; Series Preface; Preface to First Edition; Preface to Second Edition; Chapter 1: Applications of Advanced Composites in Aircraft Structures; References; Chapter 2: Cost of Composites: a Qualitative Discussion; 2.1 Recurring Cost; 2.2 Nonrecurring Cost; 2.3 Technology Selection; 2.4 Summary and Conclusions; Exercises; References; Chapter 3: Review of Classical Laminated Plate Theory; 3.1 Composite Materials: Definitions, Symbols and Terminology; 3.2 Constitutive Equations in Three Dimensions
  • 3.3 Constitutive Equations in Two Dimensions: Plane StressExercises; References; Chapter 4: Review of Laminate Strength and Failure Criteria; 4.1 Maximum Stress Failure Theory; 4.2 Maximum Strain Failure Theory; 4.3 Tsai-Hill Failure Theory; 4.4 Tsai-Wu Failure Theory; 4.5 Puck Failure Theory; 4.6 Other Failure Theories; References; Chapter 5: Composite Structural Components and Mathematical Formulation; 5.1 Overview of Composite Airframe; 5.2 Governing Equations; 5.3 Reductions of Governing Equations: Applications to Specific Problems; 5.4 Energy Methods; Exercises; References
  • Chapter 6: Buckling of Composite Plates6.1 Buckling of Rectangular Composite Plate under Biaxial Loading; 6.2 Buckling of Rectangular Composite Plate under Uniaxial Compression; 6.3 Buckling of Rectangular Composite Plate under Shear; 6.4 Buckling of Long Rectangular Composite Plates under Shear; 6.5 Buckling of Rectangular Composite Plates under Combined Loads; 6.6 Design Equations for Different Boundary Conditions and Load Combinations; Exercises; References; Chapter 7: Post-Buckling; 7.1 Post-Buckling Analysis of Composite Panels under Compression
  • 7.2 Post-Buckling Analysis of Composite Plates under ShearExercises; References; Chapter 8: Design and Analysis of Composite Beams; 8.1 Cross-Section Definition Based on Design Guidelines; 8.2 Cross-Sectional Properties; 8.3 Column Buckling; 8.4 Beam on an Elastic Foundation under Compression; 8.5 Crippling; 8.6 Importance of Radius Regions at Flange Intersections; 8.7 Inter-Rivet Buckling of Stiffener Flanges; 8.8 Application: Analysis of Stiffeners in a Stiffened Panel under Compression; Exercises; References; Chapter 9: Skin-Stiffened Structure
  • 9.1 Smearing of Stiffness Properties (Equivalent Stiffness)9.2 Failure Modes of a Stiffened Panel; 9.3 Additional Considerations for Stiffened Panels; Exercises; References; Chapter 10: Sandwich Structure; 10.1 Sandwich Bending Stiffnesses; 10.2 Buckling of Sandwich Structure; 10.3 Sandwich Wrinkling; 10.4 Sandwich Crimping; 10.5 Sandwich Intracellular Buckling (Dimpling) under Compression; 10.6 Attaching Sandwich Structures; Exercises; References; Chapter 11: Composite Fittings; 11.1 Challenges in Creating Cost- and Weight-Efficient Composite Fittings; 11.2 Basic Fittings