| 000 | 02737nam a22004935i 4500 | ||
|---|---|---|---|
| 001 | 978-94-007-2524-9 | ||
| 003 | DE-He213 | ||
| 005 | 20140220083341.0 | ||
| 007 | cr nn 008mamaa | ||
| 008 | 111027s2012 ne | s |||| 0|eng d | ||
| 020 |
_a9789400725249 _9978-94-007-2524-9 |
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| 024 | 7 |
_a10.1007/978-94-007-2524-9 _2doi |
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| 050 | 4 | _aTA174 | |
| 072 | 7 |
_aTBD _2bicssc |
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| 072 | 7 |
_aTEC016020 _2bisacsh |
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| 072 | 7 |
_aTEC016000 _2bisacsh |
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| 082 | 0 | 4 |
_a620.0042 _223 |
| 100 | 1 |
_aWanhill, Russell. _eauthor. |
|
| 245 | 1 | 0 |
_aFatigue of Beta Processed and Beta Heat-treated Titanium Alloys _h[electronic resource] / _cby Russell Wanhill, Simon Barter. |
| 264 | 1 |
_aDordrecht : _bSpringer Netherlands, _c2012. |
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| 300 |
_aX, 51p. 33 illus., 27 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 |
_aSpringerBriefs in Applied Sciences and Technology, _x2191-530X |
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| 520 | _aThis publication reviews most of the available literature on the fatigue properties of β annealed Ti-6Al-4V and titanium alloys with similar microstructures. The focus is on β processed and β heat-treated alloys because β annealed Ti-6Al-4V has been selected for highly loaded and fatigue-critical structures, including the main wing-carry-through bulkheads and vertical tail stubs, of advanced high-performance military aircraft. An important aspect of the review is a concise survey of fatigue life assessment methods and the required types of fatigue data. This survey provides the background to recommendations for further research, especially on the fatigue behaviour of β annealed Ti-6Al-4V under realistic fatigue load histories, including the essential topic of short/small fatigue crack growth. Such research is required for independent fatigue life assessments that conform to the aircraft manufacturer’s design requirements, and also for life reassessments that most probably will have to be made during the service life of the aircraft. | ||
| 650 | 0 | _aEngineering. | |
| 650 | 0 | _aMechanical engineering. | |
| 650 | 0 | _aEngineering design. | |
| 650 | 0 | _aMaterials. | |
| 650 | 1 | 4 | _aEngineering. |
| 650 | 2 | 4 | _aEngineering Design. |
| 650 | 2 | 4 | _aStructural Materials. |
| 650 | 2 | 4 | _aStructural Mechanics. |
| 700 | 1 |
_aBarter, Simon. _eauthor. |
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| 710 | 2 | _aSpringerLink (Online service) | |
| 773 | 0 | _tSpringer eBooks | |
| 776 | 0 | 8 |
_iPrinted edition: _z9789400725232 |
| 830 | 0 |
_aSpringerBriefs in Applied Sciences and Technology, _x2191-530X |
|
| 856 | 4 | 0 | _uhttp://dx.doi.org/10.1007/978-94-007-2524-9 |
| 912 | _aZDB-2-ENG | ||
| 999 |
_c104502 _d104502 |
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