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Damage Tolerance of Metallic Aircraft Structures [electronic resource] : Materials and Numerical Modelling / by Sérgio M. O. Tavares, Paulo M. S. T. de Castro.

By: Tavares, Sérgio M. O [author.].
Contributor(s): de Castro, Paulo M. S. T [author.] | SpringerLink (Online service).
Material type: materialTypeLabelBookSeries: SpringerBriefs in Computational Mechanics: Publisher: Cham : Springer International Publishing : Imprint: Springer, 2019Edition: 1st ed. 2019.Description: XV, 106 p. 50 illus., 42 illus. in color. online resource.Content type: text Media type: computer Carrier type: online resourceISBN: 9783319701905.Subject(s): Aerospace engineering | Astronautics | Metals | Mechanics, Applied | Solids | Aerospace Technology and Astronautics | Metals and Alloys | Solid MechanicsAdditional physical formats: Printed edition:: No title; Printed edition:: No titleDDC classification: 629.1 Online resources: Click here to access online
Contents:
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.
In: Springer Nature eBookSummary: 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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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.

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