| 000 | 03287nam a22005895i 4500 | ||
|---|---|---|---|
| 001 | 978-3-319-70190-5 | ||
| 003 | DE-He213 | ||
| 005 | 20220801214040.0 | ||
| 007 | cr nn 008mamaa | ||
| 008 | 180806s2019 sz | s |||| 0|eng d | ||
| 020 |
_a9783319701905 _9978-3-319-70190-5 |
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| 024 | 7 |
_a10.1007/978-3-319-70190-5 _2doi |
|
| 050 | 4 | _aTL1-4050 | |
| 072 | 7 |
_aTRP _2bicssc |
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_aTTDS _2bicssc |
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_aTTDS _2thema |
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| 082 | 0 | 4 |
_a629.1 _223 |
| 100 | 1 |
_aTavares, Sérgio M. O. _eauthor. _4aut _4http://id.loc.gov/vocabulary/relators/aut _935992 |
|
| 245 | 1 | 0 |
_aDamage Tolerance of Metallic Aircraft Structures _h[electronic resource] : _bMaterials and Numerical Modelling / _cby Sérgio M. O. Tavares, Paulo M. S. T. de Castro. |
| 250 | _a1st ed. 2019. | ||
| 264 | 1 |
_aCham : _bSpringer International Publishing : _bImprint: Springer, _c2019. |
|
| 300 |
_aXV, 106 p. 50 illus., 42 illus. in color. _bonline resource. |
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| 336 |
_atext _btxt _2rdacontent |
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| 337 |
_acomputer _bc _2rdamedia |
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| 338 |
_aonline resource _bcr _2rdacarrier |
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| 347 |
_atext file _bPDF _2rda |
||
| 490 | 1 |
_aSpringerBriefs in Computational Mechanics, _x2191-5350 |
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| 505 | 0 | _a1 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 | _aThis 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. | ||
| 650 | 0 |
_aAerospace engineering. _96033 |
|
| 650 | 0 |
_aAstronautics. _935993 |
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| 650 | 0 |
_aMetals. _911824 |
|
| 650 | 0 |
_aMechanics, Applied. _93253 |
|
| 650 | 0 |
_aSolids. _93750 |
|
| 650 | 1 | 4 |
_aAerospace Technology and Astronautics. _935994 |
| 650 | 2 | 4 |
_aMetals and Alloys. _931871 |
| 650 | 2 | 4 |
_aSolid Mechanics. _931612 |
| 700 | 1 |
_ade Castro, Paulo M. S. T. _eauthor. _4aut _4http://id.loc.gov/vocabulary/relators/aut _935995 |
|
| 710 | 2 |
_aSpringerLink (Online service) _935996 |
|
| 773 | 0 | _tSpringer Nature eBook | |
| 776 | 0 | 8 |
_iPrinted edition: _z9783319701899 |
| 776 | 0 | 8 |
_iPrinted edition: _z9783319701912 |
| 830 | 0 |
_aSpringerBriefs in Computational Mechanics, _x2191-5350 _935997 |
|
| 856 | 4 | 0 | _uhttps://doi.org/10.1007/978-3-319-70190-5 |
| 912 | _aZDB-2-ENG | ||
| 912 | _aZDB-2-SXE | ||
| 942 | _cEBK | ||
| 999 |
_c75900 _d75900 |
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