Author : David J. Peery
Publisher : Courier Corporation
Page : 578 pages
File Size : 12,97 MB
Release : 2013-04-29
Category : Science
ISBN : 048626730X
This legendary, still-relevant reference text on aircraft stress analysis discusses basic structural theory and the application of the elementary principles of mechanics to the analysis of aircraft structures. 1950 edition.
Author : Thomas Henry Gordon Megson
Publisher : Hodder Education
Page : 0 pages
File Size : 21,15 MB
Release : 1990
Category : Aeroelasticity
ISBN : 9780713136814
This book provides a self-contained course in aircraft structures which contains not only the fundamentals of elasticity and aircraft structural analysis but also the associated topics of airworthiness and aeroelasticity.
Author : Alan A. Baker
Publisher : AIAA
Page : 626 pages
File Size : 40,43 MB
Release : 2004
Category : Airplanes
ISBN : 9781600860409
Author : John Cutler
Publisher : Grafton Books
Page : 184 pages
File Size : 38,2 MB
Release : 1981
Category : Technology & Engineering
ISBN :
This book explains aircraft structures so as to provide a basic understanding of the subject and the terminology used, as well as illustrating some of the problems.It provides a brief historical background, and covers parts of the aeroplane, loads, structural form, materials, processes, detail design, quality control, stressing, and the documentation associated with modification and repairs.The Fourth Edition takes account of new materials and the new European regulatory system.
Author : Bruce K. Donaldson
Publisher : Cambridge University Press
Page : 15 pages
File Size : 29,51 MB
Release : 2008-03-24
Category : Technology & Engineering
ISBN : 1107394171
As with the first edition, this textbook provides a clear introduction to the fundamental theory of structural analysis as applied to vehicular structures such as aircraft, spacecraft, automobiles and ships. The emphasis is on the application of fundamental concepts of structural analysis that are employed in everyday engineering practice. All approximations are accompanied by a full explanation of their validity. In this new edition, more topics, figures, examples and exercises have been added. There is also a greater emphasis on the finite element method of analysis. Clarity remains the hallmark of this text and it employs three strategies to achieve clarity of presentation: essential introductory topics are covered, all approximations are fully explained and many important concepts are repeated.
Author : Yucheng Liu
Publisher : Bentham Science Publishers
Page : 592 pages
File Size : 30,48 MB
Release : 2016-10-07
Category : Technology & Engineering
ISBN : 1681083051
This comprehensive volume presents a wide spectrum of information about the design, analysis and manufacturing of aerospace structures and materials. Readers will find an interesting compilation of reviews covering several topics such as structural dynamics and impact simulation, acoustic and vibration testing and analysis, fatigue analysis and life optimization, reversing design methodology, non-destructive evaluation, remotely piloted helicopters, surface enhancement of aerospace alloys, manufacturing of metal matrix composites, applications of carbon nanotubes in aircraft material design, carbon fiber reinforcements, variable stiffness composites, aircraft material selection, and much more. This volume is a key reference for graduates undertaking advanced courses in materials science and aeronautical engineering as well as researchers and professional engineers seeking to increase their understanding of aircraft material selection and design.
Author : T.H.G. Megson
Publisher : Butterworth-Heinemann
Page : 645 pages
File Size : 45,23 MB
Release : 2010-01-16
Category : Technology & Engineering
ISBN : 1856179338
Introduction to Aircraft Structural Analysis is an essential resource for learning aircraft structural analysis. Based on the author's best-selling book Aircraft Structures for Engineering Students, this brief text introduces the reader to the basics of structural analysis as applied to aircraft structures. Coverage of elasticity, energy methods and virtual work sets the stage for discussions of airworthiness/airframe loads and stress analysis of aircraft components. Numerous worked examples, illustrations, and sample problems show how to apply the concepts to realistic situations. The book covers the core concepts in about 200 fewer pages by removing some optional topics like structural vibrations and aero elasticity. It consists of 23 chapters covering a variety of topics from basic elasticity to torsion of solid sections; energy methods; matrix methods; bending of thin plates; structural components of aircraft; airworthiness; airframe loads; bending of open, closed, and thin walled beams; combined open and closed section beams; wing spars and box beams; and fuselage frames and wing ribs. This book will appeal to undergraduate and postgraduate students of aerospace and aeronautical engineering, as well as professional development and training courses. Based on the author's best-selling text Aircraft Structures for Engineering Students, this Intro version covers the core concepts in about 200 fewer pages by removing some optional topics like structural vibrations and aeroelasticity Systematic step by step procedures in the worked examples Self-contained, with complete derivations for key equations
Author : Chunyun Niu
Publisher : Adaso Adastra Engineering Center
Page : 612 pages
File Size : 19,35 MB
Release : 1999
Category : Airframes
ISBN : 9789627128090
Author : Adrian P Mouritz
Publisher : Elsevier
Page : 637 pages
File Size : 23,55 MB
Release : 2012-05-23
Category : Technology & Engineering
ISBN : 0857095153
The structural materials used in airframe and propulsion systems influence the cost, performance and safety of aircraft, and an understanding of the wide range of materials used and the issues surrounding them is essential for the student of aerospace engineering.Introduction to aerospace materials reviews the main structural and engine materials used in aircraft, helicopters and spacecraft in terms of their production, properties, performance and applications.The first three chapters of the book introduce the reader to the range of aerospace materials, focusing on recent developments and requirements. Following these introductory chapters, the book moves on to discuss the properties and production of metals for aerospace structures, including chapters covering strengthening of metal alloys, mechanical testing, and casting, processing and machining of aerospace metals. The next ten chapters look in depth at individual metals including aluminium, titanium, magnesium, steel and superalloys, as well as the properties and processing of polymers, composites and wood. Chapters on performance issues such as fracture, fatigue and corrosion precede a chapter focusing on inspection and structural health monitoring of aerospace materials. Disposal/recycling and materials selection are covered in the final two chapters.With its comprehensive coverage of the main issues surrounding structural aerospace materials,Introduction to aerospace materials is essential reading for undergraduate students studying aerospace and aeronautical engineering. It will also be a valuable resource for postgraduate students and practising aerospace engineers. - Reviews the main structural and engine materials used in aircraft, helicopters and space craft in terms of their properties, performance and applications - Introduces the reader to the range of aerospace materials, focusing on recent developments and requirements, and discusses the properties and production of metals for aerospace structures - Chapters look in depth at individual metals including aluminium, titanium, magnesium, steel and superalloys
Author : Sérgio M. O. Tavares
Publisher : Springer
Page : 117 pages
File Size : 27,98 MB
Release : 2018-08-06
Category : Technology & Engineering
ISBN : 3319701908
This book provides a state-of-the-art review of the fail-safe and damage tolerance approaches, allowing weight savings and increasing aircraft reliability and structural integrity. The application of the damage tolerance approach requires extensive know-how of the fatigue and fracture properties, corrosion strength, potential failure modes and non-destructive inspection techniques, particularly minimum detectable defect and inspection intervals. In parallel, engineering practice involving damage tolerance requires numerical techniques for stress analysis of cracked structures. These evolved from basic mode I evaluations using rough finite element approaches, to current 3D modeling based on energetic approaches as the VCCT, or simulation of joining processes. This book provides a concise introduction to this subject.
