000 03578nam a22004455i 4500
001 978-1-4020-8520-8
003 DE-He213
005 20161121230536.0
007 cr nn 008mamaa
008 100301s2008 ne | s |||| 0|eng d
020 _a9781402085208
_9978-1-4020-8520-8
024 7 _a10.1007/978-1-4020-8520-8
_2doi
050 4 _aTA401-492
072 7 _aTGM
_2bicssc
072 7 _aTEC021000
_2bisacsh
082 0 4 _a620.11
_223
245 1 0 _aMultiscale Fatigue Crack Initiation and Propagation of Engineering Materials: Structural Integrity and Microstructural Worthiness
_h[electronic resource] :
_bFatigue Crack Growth Behaviour of Small and Large Bodies /
_cedited by G. C. Sih.
264 1 _aDordrecht :
_bSpringer Netherlands,
_c2008.
300 _aXIV, 380 p.
_bonline resource.
336 _atext
_btxt
_2rdacontent
337 _acomputer
_bc
_2rdamedia
338 _aonline resource
_bcr
_2rdacarrier
347 _atext file
_bPDF
_2rda
490 1 _aSolid Mechanics and its Applications,
_x0925-0042 ;
_v152
505 0 _aApplication of Virtual Testing for Obtaining Fracture Allowable of Aerospace and Aircraft Materials -- An Equivalent Block Approach to Crack Growth -- Prediction of Fatigue Crack Growth Rates in Ti-6Al-4V Alloy -- Some Practical Implications of Exponential Crack Growth -- Fatigue Behaviour of FS, LB and MIG Welds of AA6061-T6 and AA6082-T6 -- Fatigue Damage from Surface to Bulk -- Microcracking in High Temperature Low Cycle Fatigue -- Invariant Form of Micro-/Macro-Cracking in Fatigue -- Fatigue Crack Growth Rate of Cable-Stayed Portion of Runyang Bridge: Part I – Cable Crack Growth Due to Disproportionate Cable Tightening/Loosening and Traffic Loading -- Fatigue Crack Growth Rate of Cable-Stayed Portion of Runyang Bridge: Part II – Steel Wire Crack Growth Due to Disproportionate Cable Tightening/Loosening and Traffic Loading -- Fatigue of Small-Scale Metal Materials: From Micro- to Nano-Scale -- Assessment of Fatigue Damage in Heterogeneous Materials by Application of a Novel Compliance Technique -- Fatigue Crack Growth of Aircraft Aluminum Alloys.
520 _aThis book elucidates the correlation of fatigue crack growth data to multiscale cracking, particularly to the understanding of micrographs influenced by mechanical disturbance and thermodynamic variables. Attention is given to the interpretation of test data by fatigue crack growth rate using two empirical parameters in consistence with the fracture control methodology currently used by industry. Micrograph and crack growth rate data are presented for a host of metals used by the aerospace and nuclear industry. Furthermore, these data can be shown to lie on a straight line for the two parameter model that traditionally refers to regions I, II, and III. Results for small and large cracks can thus be connected to provide fatigue life prediction with data from the microscopic scale level such that the interactive effects of loading, geometry and material by mechanical tests are accounted for.
650 0 _aMaterials science.
650 0 _aStructural mechanics.
650 1 4 _aMaterials Science.
650 2 4 _aMaterials Science, general.
650 2 4 _aStructural Mechanics.
700 1 _aSih, G. C.
_eeditor.
710 2 _aSpringerLink (Online service)
773 0 _tSpringer eBooks
776 0 8 _iPrinted edition:
_z9781402085192
830 0 _aSolid Mechanics and its Applications,
_x0925-0042 ;
_v152
856 4 0 _uhttp://dx.doi.org/10.1007/978-1-4020-8520-8
912 _aZDB-2-ENG
950 _aEngineering (Springer-11647)
999 _c500315
_d500315