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Titlebook: Structural Integrity of Aging Airplanes; S. N. Atluri (J. C. Hunsaker Visiting Professor),S Conference proceedings 1991 Springer-Verlag Be

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书目名称Structural Integrity of Aging Airplanes
编辑S. N. Atluri (J. C. Hunsaker Visiting Professor),S
视频video
丛书名称Springer Series in Computational Mechanics
图书封面Titlebook: Structural Integrity of Aging Airplanes;  S. N. Atluri (J. C. Hunsaker Visiting Professor),S Conference proceedings 1991 Springer-Verlag Be
描述The emergence of civil aviation as a means of mass transportation is primarily due to the large­ scale construction of jet airplanes in the past 30 years or so. A large number of these jet airplanes is currently operating at or beyond their designed fatigue lives. Thus, the structural integrity of these aging airplanes has become an issue of major concern to all nations of the world. To bring the needed technical and research focus on the issues involved in the life-enhancement and safety-assurance of aging airplanes, the Federal Aviation Administration sponsored a symposium in Atlanta, GA, USA, during 20-22 March 1990. This symposium, under the title "International Symposium on Structural Integrity of Aging Airplanes· was organized jointly be the Georgia Institute of Technology (Center for Computational Mechanics) and the Transportation Systems Center (Cambridge, MA) of the U.S. Department of Transportation. Industrial and academic experts from several countries in North America, Europe and Asia, were invited to discuss their experiences and proposed solutions. This monograph contains the original papers that represent the expanded and edited versions of the talks presented at thi
出版日期Conference proceedings 1991
关键词Alterung; Flugzeugbau; Verschleiß; accident; construction; damage; design; fatigue; fracture; fracture mechan
版次1
doihttps://doi.org/10.1007/978-3-642-84364-8
isbn_softcover978-3-642-84366-2
isbn_ebook978-3-642-84364-8Series ISSN 1431-8547
issn_series 1431-8547
copyrightSpringer-Verlag Berlin, Heidelberg 1991
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Risk Analysis for Aging Aircraft Fleets,luating the durability and damage tolerance characteristics of aircraft which were designed prior to the current requirements of MIL-STD-1530A; and, c) evaluating structural repairs and modifications. These applications have used fracture mechanics principles in a deterministic manner. That is, flaw
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The Civil Damage Tolerance Requirements in Theory and Practice,developed and ageing aircraft. Some improvements to the DTR are suggested. In principle, fracture control of aircraft is ensured by non-destructive inspection, although destructive inspection has been suggested for certain ageing aircraft, as will be discussed briefly as well.
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