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Damage Tolerance of Metallic Aircraf...
~
de Castro, Paulo M. S. T.
Damage Tolerance of Metallic Aircraft Structures = Materials and Numerical Modelling /
Record Type:
Language materials, printed : Monograph/item
Title/Author:
Damage Tolerance of Metallic Aircraft Structures/ by Sérgio M. O. Tavares, Paulo M. S. T. de Castro.
Reminder of title:
Materials and Numerical Modelling /
Author:
Tavares, Sérgio M. O.
other author:
de Castro, Paulo M. S. T.
Description:
XV, 106 p. 50 illus., 42 illus. in color.online resource. :
Contained By:
Springer Nature eBook
Subject:
Aerospace engineering. -
Online resource:
https://doi.org/10.1007/978-3-319-70190-5
ISBN:
9783319701905
Damage Tolerance of Metallic Aircraft Structures = Materials and Numerical Modelling /
Tavares, Sérgio M. O.
Damage Tolerance of Metallic Aircraft Structures
Materials and Numerical Modelling /[electronic resource] :by Sérgio M. O. Tavares, Paulo M. S. T. de Castro. - 1st ed. 2019. - XV, 106 p. 50 illus., 42 illus. in color.online resource. - SpringerBriefs in Computational Mechanics,2191-5342. - SpringerBriefs in Computational Mechanics,.
1 The application of the damage tolerance approach requires extensive -- 2 The engineering practice involving damage tolerance -- 3 The damage tolerance numerical techniques for stress analysis of cracked structures -- 4 The current 3D modeling based on energetic approaches.
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.
ISBN: 9783319701905
Standard No.: 10.1007/978-3-319-70190-5doiSubjects--Topical Terms:
686400
Aerospace engineering.
LC Class. No.: TL787-4050.22
Dewey Class. No.: 629.1
Damage Tolerance of Metallic Aircraft Structures = Materials and Numerical Modelling /
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