Electronic Resource

Damage Tolerance of Metallic Aircraft Structures

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Penilaian

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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.

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Availability

Inventory Code	Barcode	Call Number	Location	Status
1908002038	EB0002727	629.134 31 Tav d	Central Library (OPAC)	Available

Detail Information

Series Title

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Call Number

629.134 31 Tav d

Publisher

Switzerland : Springer Cham., 2018

Collation

xv, 106p.:Ill

Language

English

ISBN/ISSN

978-3-319-70190-5

Classification

629.134 31

Content Type

Ebook

Media Type

-

Carrier Type

online resource

Edition

1

Subject(s)

Metals--Fatigue

Specific Detail Info

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Statement of Responsibility

BRF

Other version/related

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