Damage Tolerance of Metallic Aircraft Structures (Record no. 75900)
[ view plain ]
| 000 -LEADER | |
|---|---|
| fixed length control field | 03287nam a22005895i 4500 |
| 001 - CONTROL NUMBER | |
| control field | 978-3-319-70190-5 |
| 005 - DATE AND TIME OF LATEST TRANSACTION | |
| control field | 20220801214040.0 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION | |
| fixed length control field | 180806s2019 sz | s |||| 0|eng d |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER | |
| ISBN | 9783319701905 |
| -- | 978-3-319-70190-5 |
| 082 04 - CLASSIFICATION NUMBER | |
| Call Number | 629.1 |
| 100 1# - AUTHOR NAME | |
| Author | Tavares, Sérgio M. O. |
| 245 10 - TITLE STATEMENT | |
| Title | Damage Tolerance of Metallic Aircraft Structures |
| Sub Title | Materials and Numerical Modelling / |
| 250 ## - EDITION STATEMENT | |
| Edition statement | 1st ed. 2019. |
| 300 ## - PHYSICAL DESCRIPTION | |
| Number of Pages | XV, 106 p. 50 illus., 42 illus. in color. |
| 490 1# - SERIES STATEMENT | |
| Series statement | SpringerBriefs in Computational Mechanics, |
| 505 0# - FORMATTED CONTENTS NOTE | |
| Remark 2 | 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. |
| 520 ## - SUMMARY, ETC. | |
| Summary, etc | 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. |
| 700 1# - AUTHOR 2 | |
| Author 2 | de Castro, Paulo M. S. T. |
| 856 40 - ELECTRONIC LOCATION AND ACCESS | |
| Uniform Resource Identifier | https://doi.org/10.1007/978-3-319-70190-5 |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) | |
| Koha item type | eBooks |
| 264 #1 - | |
| -- | Cham : |
| -- | Springer International Publishing : |
| -- | Imprint: Springer, |
| -- | 2019. |
| 336 ## - | |
| -- | text |
| -- | txt |
| -- | rdacontent |
| 337 ## - | |
| -- | computer |
| -- | c |
| -- | rdamedia |
| 338 ## - | |
| -- | online resource |
| -- | cr |
| -- | rdacarrier |
| 347 ## - | |
| -- | text file |
| -- | |
| -- | rda |
| 650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Aerospace engineering. |
| 650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Astronautics. |
| 650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Metals. |
| 650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Mechanics, Applied. |
| 650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Solids. |
| 650 14 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Aerospace Technology and Astronautics. |
| 650 24 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Metals and Alloys. |
| 650 24 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Solid Mechanics. |
| 830 #0 - SERIES ADDED ENTRY--UNIFORM TITLE | |
| -- | 2191-5350 |
| 912 ## - | |
| -- | ZDB-2-ENG |
| 912 ## - | |
| -- | ZDB-2-SXE |
No items available.