Damage Tolerance Of Metallic Structures: Analysis Methods And Applications
Author : J. B. Chang
Publisher : ASTM International
Page : 156 pages
File Size : 12,82 MB
Release : 1984
Category :
ISBN :
Author : J. B. Chang
Publisher : ASTM International
Page : 156 pages
File Size : 12,82 MB
Release : 1984
Category :
ISBN :
Author : Sérgio M. O. Tavares
Publisher : Springer
Page : 117 pages
File Size : 17,88 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.
Author : J. B. Chang
Publisher : ASTM International
Page : 168 pages
File Size : 45,63 MB
Release : 1984
Category : Technology & Engineering
ISBN : 9780803104075
Author : Charles E. Harris
Publisher :
Page : 42 pages
File Size : 27,11 MB
Release : 2003
Category : Airframes
ISBN :
Author : Committee on New Materials for Advanced Civil Aircraft
Publisher : National Academies Press
Page : 99 pages
File Size : 15,93 MB
Release : 1996-03-29
Category : Technology & Engineering
ISBN : 0309588782
The major objective of this book was to identify issues related to the introduction of new materials and the effects that advanced materials will have on the durability and technical risk of future civil aircraft throughout their service life. The committee investigated the new materials and structural concepts that are likely to be incorporated into next generation commercial aircraft and the factors influencing application decisions. Based on these predictions, the committee attempted to identify the design, characterization, monitoring, and maintenance issues that are critical for the introduction of advanced materials and structural concepts into future aircraft.
Author : Taoufik Boukharouba
Publisher : Springer Science & Business Media
Page : 616 pages
File Size : 25,81 MB
Release : 2009-08-09
Category : Science
ISBN : 904812669X
The First African InterQuadrennial ICF Conference “AIQ-ICF2008” on Damage and Fracture Mechanics – Failure Analysis of Engineering Materials and Structures”, Algiers, Algeria, June 1–5, 2008 is the first in the series of InterQuadrennial Conferences on Fracture to be held in the continent of Africa. During the conference, African researchers have shown that they merit a strong reputation in international circles and continue to make substantial contributions to the field of fracture mechanics. As in most countries, the research effort in Africa is und- taken at the industrial, academic, private sector and governmental levels, and covers the whole spectrum of fracture and fatigue. The AIQ-ICF2008 has brought together researchers and engineers to review and discuss advances in the development of methods and approaches on Damage and Fracture Mechanics. By bringing together the leading international experts in the field, AIQ-ICF promotes technology transfer and provides a forum for industry and researchers of the host nation to present their accomplishments and to develop new ideas at the highest level. International Conferences have an important role to play in the technology transfer process, especially in terms of the relationships to be established between the participants and the informal exchange of ideas that this ICF offers.
Author : J. P. Gallagher
Publisher :
Page : 1382 pages
File Size : 45,83 MB
Release : 1984
Category : Airframes
ISBN :
The handbook provides specific background data and justification for the detailed requirements of MIL-A-83444 and provides guidelines and state-of-the-art analysis methods to assist contractor and USAF personnel in complying with the intent of the specification and in solving cracking problems, in general, for metallic aircraft structures. Cf. Report Documentation Page.
Author : A.A. Baker
Publisher : Elsevier
Page : 561 pages
File Size : 16,82 MB
Release : 2003-01-23
Category : Technology & Engineering
ISBN : 0080522955
The availability of efficient and cost-effective technologies to repair or extend the life of aging military airframes is becoming a critical requirement in most countries around the world, as new aircraft becoming prohibitively expensive and defence budgets shrink. To a lesser extent a similar situation is arising with civil aircraft, with falling revenues and the high cost of replacement aircraft.This book looks at repair/reinforcement technology, which is based on the use of adhesively bonded fibre composite patches or doublers and can provide cost-effective life extension in many situations. From the scientific and engineering viewpoint, whilst simple in concept, this technology can be quite challenging particularly when used to repair primary structure. This is due to it being based on interrelated inputs from the fields of aircraft design, solid mechanics, fibre composites, structural adhesive bonding, fracture mechanics and metal fatigue. The technologies of non-destructive inspection (NDI) and, more recently smart materials, are also included. Operational issues are equally critical, including airworthiness certification, application technology (including health and safety issues), and training.Including contributions from leading experts in Canada, UK, USA and Australia, this book discusses most of these issues and the latest developments. Most importantly, it contains real histories of application of this technology to both military and civil aircraft.
Author : Markus G. R. Sause
Publisher : Springer Nature
Page : 292 pages
File Size : 16,22 MB
Release : 2021
Category : Aerospace engineering
ISBN : 3030721922
This open access book presents established methods of structural health monitoring (SHM) and discusses their technological merit in the current aerospace environment. While the aerospace industry aims for weight reduction to improve fuel efficiency, reduce environmental impact, and to decrease maintenance time and operating costs, aircraft structures are often designed and built heavier than required in order to accommodate unpredictable failure. A way to overcome this approach is the use of SHM systems to detect the presence of defects. This book covers all major contemporary aerospace-relevant SHM methods, from the basics of each method to the various defect types that SHM is required to detect to discussion of signal processing developments alongside considerations of aerospace safety requirements. It will be of interest to professionals in industry and academic researchers alike, as well as engineering students. This article/publication is based upon work from COST Action CA18203 (ODIN - http://odin-cost.com/), supported by COST (European Cooperation in Science and Technology). COST (European Cooperation in Science and Technology) is a funding agency for research and innovation networks. Our Actions help connect research initiatives across Europe and enable scientists to grow their ideas by sharing them with their peers. This boosts their research, career and innovation.
Author : Alten F. Grandt, Jr.
Publisher : John Wiley & Sons
Page : 568 pages
File Size : 40,58 MB
Release : 2003-11-03
Category : Technology & Engineering
ISBN : 9780471214595
Discusses applications of failures and evaluation techniques to a variety of industries. * Presents a unified approach using two key elements of structural design.