| 000 | 03473nam a22005535i 4500 | ||
|---|---|---|---|
| 001 | 978-3-319-56227-8 | ||
| 003 | DE-He213 | ||
| 005 | 20220801214127.0 | ||
| 007 | cr nn 008mamaa | ||
| 008 | 170420s2017 sz | s |||| 0|eng d | ||
| 020 |
_a9783319562278 _9978-3-319-56227-8 |
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| 024 | 7 |
_a10.1007/978-3-319-56227-8 _2doi |
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| 050 | 4 | _aTA349-359 | |
| 072 | 7 |
_aTGB _2bicssc |
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| 072 | 7 |
_aTEC009070 _2bisacsh |
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| 072 | 7 |
_aTGB _2thema |
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| 082 | 0 | 4 |
_a620.1 _223 |
| 100 | 1 |
_aAlderliesten, René. _eauthor. _4aut _4http://id.loc.gov/vocabulary/relators/aut _936478 |
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| 245 | 1 | 0 |
_aFatigue and Fracture of Fibre Metal Laminates _h[electronic resource] / _cby René Alderliesten. |
| 250 | _a1st ed. 2017. | ||
| 264 | 1 |
_aCham : _bSpringer International Publishing : _bImprint: Springer, _c2017. |
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| 300 |
_aXII, 300 p. 189 illus., 116 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 |
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| 490 | 1 |
_aSolid Mechanics and Its Applications, _x2214-7764 ; _v236 |
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| 505 | 0 | _aI Laminate concepts and properties -- 1 Introduction -- 2 Intellectual property and patents -- 3 Laminate concepts and typical properties -- II Prediction & analysis methods -- 1 Stress-train -- 2 Blunt notch strength -- 3 Bearing strength -- 4 Fatigue initiation -- 5 Static and fatigue delamination -- 6 Fatigue crack propagation -- 7 Residual strength -- III Environmental aspects -- 1 Temperature -- 2 Effect of frequency (wave form, hold time) -- 3 Acoustic fatigue. | |
| 520 | _aThis book contributes to the field of hybrid technology, describing the current state of knowledge concerning the hybrid material concept of laminated metallic and composite sheets for primary aeronautical structural applications. It is the only book to date on fatigue and fracture of fibre metal laminates (FMLs). The first section of the book provides a general background of the FML technology, highlighting the major FML types developed and studied over the past decades in conjunction with an overview of industrial developments based on filed patents. In turn, the second section discusses the mechanical response to quasi-static loading, together with the fracture phenomena during quasi-static and cyclic loading. To consider the durability aspects related to strength justification and certification of primary aircraft structures, the third section discusses thermal aspects related to FMLs and their mechanical response to various environmental and acoustic conditions. | ||
| 650 | 0 |
_aMechanics, Applied. _93253 |
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| 650 | 0 |
_aMaterials—Analysis. _936479 |
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| 650 | 0 |
_aAerospace engineering. _96033 |
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| 650 | 0 |
_aAstronautics. _936480 |
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| 650 | 1 | 4 |
_aEngineering Mechanics. _931830 |
| 650 | 2 | 4 |
_aCharacterization and Analytical Technique. _936481 |
| 650 | 2 | 4 |
_aAerospace Technology and Astronautics. _936482 |
| 710 | 2 |
_aSpringerLink (Online service) _936483 |
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| 773 | 0 | _tSpringer Nature eBook | |
| 776 | 0 | 8 |
_iPrinted edition: _z9783319562261 |
| 776 | 0 | 8 |
_iPrinted edition: _z9783319562285 |
| 776 | 0 | 8 |
_iPrinted edition: _z9783319858593 |
| 830 | 0 |
_aSolid Mechanics and Its Applications, _x2214-7764 ; _v236 _936484 |
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| 856 | 4 | 0 | _uhttps://doi.org/10.1007/978-3-319-56227-8 |
| 912 | _aZDB-2-ENG | ||
| 912 | _aZDB-2-SXE | ||
| 942 | _cEBK | ||
| 999 |
_c75986 _d75986 |
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