سازه ها و مواد کامپوزيتي در مهندسي هوافضا

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

درباره کتاب:

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.

مدل کردن اثر خرابي در سازه هاي کامپوزيت: روش هاي ساده شده

ويژگي ها:

Comprehensively covers new and existing methods for the design and analysis of composites structures with damage present

  • Provides efficient and accurate approaches for analysing structures with holes and impact damage
  • Introduces a new methodology for fatigue analysis of composites
  • Provides design guidelines, and step by step descriptions of how to apply the methods, along with evaluation of their accuracy and applicability
  • Includes problems and exercises
  • Accompanied by a website hosting lecture slides and solutions

مواد کامپوزيتي پيشرفته براي مهندسي هوافضا: فرآيند (توليد)، خواص و کاربردها

شرح:

Advanced Composite Materials for Aerospace Engineering: Processing, Properties and Applications predominately focuses on the use of advanced composite materials in aerospace engineering. It discusses both the basic and advanced requirements of these materials for various applications in the aerospace sector, and includes discussions on all the main types of commercial composites that are reviewed and compared to those of metals.

Various aspects, including the type of fibre, matrix, structure, properties, modeling, and testing are considered, as well as mechanical and structural behavior, along with recent developments. There are several new types of composite materials that have huge potential for various applications in the aerospace sector, including nanocomposites, multiscale and auxetic composites, and self-sensing and self-healing composites, each of which is discussed in detail.

The book’s main strength is its coverage of all aspects of the topics, including materials, design, processing, properties, modeling and applications for both existing commercial composites and those currently under research or development. Valuable case studies provide relevant examples of various product designs to enhance learning.

سازه هاي هواپيما براي دانشجويان

ويژگي ها:

Aircraft Structures for Engineering Students, Fifth Edition, is the leading self-contained aircraft structures course text. It covers all fundamental subjects, including elasticity, structural analysis, airworthiness, and aeroelasticity.

The author has revised and updated the text throughout and added new examples and exercises using Matlab. Additional worked examples make the text even more accessible by showing the application of concepts to airframe structures.

The text is designed for undergraduate and postgraduate students of aerospace and aeronautical engineering. It is also suitable for professional development and training courses.

  • New worked examples throughout the text aid understanding and relate concepts to real world applications
  • Matlab examples and exercises added throughout to support use of computational tools in analysis and design
  • An extensive aircraft design project case study shows the application of the major techniques in the book

مقدمه اي بر ايروالاستيسيته و بارهاي هواپيما

چکيده

Introduction to Aircraft Aeroelasticity and Loads, Second Edition is an updated new edition offering comprehensive coverage of the main principles of aircraft aeroelasticity and loads. For ease of reference, the book is divided into three parts and begins by reviewing the underlying disciplines of vibrations, aerodynamics, loads and control, and then goes on to describe simplified models to illustrate aeroelastic behaviour and aircraft response and loads for the flexible aircraft before introducing some more advanced methodologies. Finally, it explains how industrial certification requirements for aeroelasticity and loads may be met and relates these to the earlier theoretical approaches used.