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Composite Materials and Structures in Aerospace Engineering -

Composite Materials and Structures in Aerospace Engineering

Erasmo Carrera (Herausgeber)

Buch | Softcover
248 Seiten
2016
Trans Tech Publications Ltd (Verlag)
978-3-03835-746-9 (ISBN)
CHF 275,80 inkl. MwSt
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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
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.

Preface
Chapter 1
An Introduction to Micromechanics
Chapter 2
Optimisation of Variable Stiffness Plates
Chapter 3
Selected Aspects of Current Challenges in Composite Product Development for Automotive and Aerospace Industry
Chapter 4
Fatigue Properties of Aerospace Z-Pinned Composites
Chapter 5
Some Examples of “Multi-Physical” Fatigue of Organic Matrix Composites for Aircraft Applications
Chapter 6
Post-Buckling Analysis of Damaged Multilayered Composite Stiffened Plates by Rayleigh-Ritz Method
Chapter 7
A Promising Way to Model Damage in Composite and Dry Fabrics Using a Discrete Element Method (DEM)
Chapter 8
A Thermal Stress Analysis of Three-Dimensional Beams by Refined One-Dimensional Models and Strong Form Solutions
Chapter 9
High-Fidelity and Computationally Efficient Component-Wise Structural Models: An Overview of Applications and Perspectives
Chapter 10
Reduced Order Models for Static and Dynamic Analysis of Composite Panels Based on a Perturbation Approach
Chapter 11
Shell Finite Elements for the Analysis of Multifield Problems in Multilayered Composite Structures

Erscheinungsdatum
Reihe/Serie Applied Mechanics and Materials
Zusatzinfo Illustrations
Verlagsort Zurich
Sprache englisch
Maße 170 x 240 mm
Gewicht 560 g
Themenwelt Mathematik / Informatik Informatik Theorie / Studium
Mathematik / Informatik Mathematik Analysis
Technik Fahrzeugbau / Schiffbau
Technik Luft- / Raumfahrttechnik
Technik Maschinenbau
ISBN-10 3-03835-746-4 / 3038357464
ISBN-13 978-3-03835-746-9 / 9783038357469
Zustand Neuware
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