Wentworth
Institute of Technology
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 additio...
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| Main Author: | |
|---|---|
| Format: | Electronic eBook |
| Language: | English |
| Published: |
New York :
Wiley,
2013.
|
| Edition: | 2nd ed. |
| Series: | Aerospace Series.
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| Subjects: | |
| Online Access: |
Full text (Wentworth users only) |
| Local Note: | ProQuest Ebook Central |
MARC
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| 100 | 1 | |a Kassapoglou, Christos. | |
| 245 | 1 | 0 | |a Design and Analysis of Composite Structures : |b with Applications to Aerospace Structures. |
| 250 | |a 2nd ed. | ||
| 260 | |a New York : |b Wiley, |c 2013. | ||
| 300 | |a 1 online resource (424 pages) | ||
| 336 | |a text |b txt |2 rdacontent | ||
| 337 | |a computer |b c |2 rdamedia | ||
| 338 | |a online resource |b cr |2 rdacarrier | ||
| 490 | 1 | |a Aerospace Series | |
| 500 | |a 7.2.1.1 Application: Post-Buckled Stiffened Fuselage Skin under Shear. | ||
| 505 | 0 | |a DESIGN AND ANALYSIS OF COMPOSITE STRUCTURES : WITH APPLICATIONS TO AEROSPACE STRUCTURES; Contents; About the Author; Series Preface; Preface to First Edition; Preface to Second Edition; 1 Applications of Advanced Composites in Aircraft Structures; References; 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; 3 Review of Classical Laminated Plate Theory; 3.1 Composite Materials: Definitions, Symbols and Terminology; 3.2 Constitutive Equations in Three Dimensions. | |
| 505 | 8 | |a 3.2.1 Tensor Transformations3.3 Constitutive Equations in Two Dimensions: Plane Stress; Exercises; References; 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; 5 Composite Structural Components and Mathematical Formulation; 5.1 Overview of Composite Airframe; 5.1.1 The Structural Design Process: The Analyst's Perspective. | |
| 505 | 8 | |a 5.1.2 Basic Design Concept and Process/Material Considerations for Aircraft Parts5.1.3 Sources of Uncertainty: Applied Loads, Usage and Material Scatter; 5.1.3.1 Knowledge of Applied Loads; 5.1.3.2 Variability in Usage; 5.1.3.3 Material Scatter; 5.1.4 Environmental Effects; 5.1.5 Effect of Damage; 5.1.6 Design Values and Allowables; 5.1.7 Additional Considerations of the Design Process; 5.2 Governing Equations; 5.2.1 Equilibrium Equations; 5.2.2 Stress-Strain Equations; 5.2.3 Strain-Displacement Equations; 5.2.4 von Karman Anisotropic Plate Equations for Large Deflections. | |
| 505 | 8 | |a 5.3 Reductions of Governing Equations: Applications to Specific Problems5.3.1 Composite Plate under Localized In-Plane Load; 5.3.2 Composite Plate under Out-of-Plane Point Load; 5.4 Energy Methods; 5.4.1 Energy Expressions for Composite Plates; 5.4.1.1 Internal Strain Energy U; 5.4.1.2 External Work W; Exercises; References; 6 Buckling of Composite Plates; 6.1 Buckling of Rectangular Composite Plate under Biaxial Loading; 6.2 Buckling of Rectangular Composite Plate under Uniaxial Compression; 6.2.1 Uniaxial Compression, Three Sides Simply Supported, One Side Free. | |
| 505 | 8 | |a 6.3 Buckling of Rectangular Composite Plate under Shear6.4 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; 7 Post-Buckling; 7.1 Post-Buckling Analysis of Composite Panels under Compression; 7.1.1 Application: Post-Buckled Panel under Compression; 7.2 Post-Buckling Analysis of Composite Plates under Shear; 7.2.1 Post-Buckling of Stiffened Composite Panels under Shear. | |
| 520 | |a 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 additional exercises. The book enables graduate students and engineers to generate meaningful and robust designs of complex composite structures. A compilation of analysis and design methods for structural components made of advanced composites, it begins with simple pa. | ||
| 588 | 0 | |a Print version record. | |
| 590 | |a ProQuest Ebook Central |b Ebook Central Academic Complete | ||
| 650 | 0 | |a Airframes |x Materials. | |
| 650 | 0 | |a Composite construction. | |
| 650 | 0 | |a Structural engineering. | |
| 650 | 7 | |a composite construction. |2 aat | |
| 650 | 7 | |a structural engineering. |2 aat | |
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| 776 | 0 | 8 | |i Print version: |a Kassapoglou, Christos. |t Design and Analysis of Composite Structures : with Applications to Aerospace Structures. |d New York : Wiley, ©2013 |z 9781118401606 |
| 830 | 0 | |a Aerospace Series. | |
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