Title:
Composite Materials and Structures in Aerospce Engineering : Selected Plenary Lectures and Key-Note Contributions of the two events FULLCOMP - Meeting FULLy integrated analysis, design, manufacturing and health-monitoring of COMPosite structures and 23rd Congress of AIDAA, Associazione Italiana di Aeronatica ed Astronautica November 17-21, 2015, Torino, Italy
Series:
Applied Mechanics and Materials ; 828
Physical Description:
viii, 236 pages : illustrations ; 23 cm.
ISBN:
9783038357469
Abstract:
Composite structures are massively exploited in many engineering fields. For instance, the state-of-the-art civil aircraft (B787 and A350) are mostly made of composite materials. The design of composites leads to challenging tasks since those competencies that stemmed from the adoption of metallic materials are often inadequate for composites. Insights on many different disciplines and tight academic/industrial cooperation are required to fully exploit composite structure capabilities.
Added Author:
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Library | Item Barcode | Call Number | Material Type | Item Category 1 | Status |
|---|---|---|---|---|---|
Searching... | 30000010343520 | TL698 F85 2016 | Open Access Book | Book | Searching... |
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Summary
Summary
Composite structures are massively exploited in many engineering fields. For instance, the state-of-the-art civil aircraft (B787 and A350) are mostly made of composite materials. The design of composites leads to challenging tasks since those competencies that stemmed from the adoption of metallic materials are often inadequate for composites. Insights on many different disciplines and tight academic/industrial cooperation are required to fully exploit composite structure capabilities.
Table of Contents
| An Introduction to Micromechanics | p. 3 |
| Optimisation of Variable Stiffness Plates | p. 27 |
| Selected Aspects of Current Challenges in Composite Product Development for Automotive and Aerospace Industry | p. 51 |
| Fatigue Properties of Aerospace Z-Pinned Composites | p. 67 |
| Some Examples of "Multi-Physical" Fatigue of Organic Matrix Composites for Aircraft Applications | p. 79 |
| Post-Buckling Analysis of Damaged Multilayered Composite Stiffened Plates by Rayleigh-Ritz Method | p. 99 |
| A Promising Way to Model Damage in Composite and Dry Fabrics Using a Discrete Element Method (DEM) | p. 119 |
| A Thermal Stress Analysis of Three-Dimensional Beams by Refined One-Dimensional Models and Strong Form Solutions | p. 139 |
| High-Fidelity and Computationally Efficient Component-Wise Structural Models: An Overview of Applications and Perspectives | p. 175 |
| Reduced Order Models for Static and Dynamic Analysis of Composite Panels Based on a Perturbation Approach | p. 199 |
| Shell Finite Elements for the Analysis of Multifield Problems in Multilayered Composite Structures | p. 215 |
