Multiscale Fatigue Crack Initiation and Propagation of Engineering Materials: Structural Integrity and Microstructural Worthiness Fatigue Crack Growth Behaviour of Small and Large Bodies /

Detalles Bibliográficos
Autor Corporativo: SpringerLink (Online service)
Otros Autores: Sih, George C. (Editor )
Formato: eBook
Lenguaje:English
Publicado: Dordrecht : Springer Netherlands : Imprint: Springer, 2008.
Edición:1st ed. 2008.
Colección:Solid Mechanics and Its Applications, 152
Materias:
Acceso en línea:https://doi.org/10.1007/978-1-4020-8520-8
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245 1 0 |a Multiscale Fatigue Crack Initiation and Propagation of Engineering Materials: Structural Integrity and Microstructural Worthiness  |b Fatigue Crack Growth Behaviour of Small and Large Bodies /  |c edited by George C. Sih. 
250 |a 1st ed. 2008. 
260 # # |a Dordrecht :  |b Springer Netherlands :  |b Imprint: Springer,  |c 2008. 
300 |a XIV, 380 p.  |b online resource. 
336 |a text  |b txt  |2 rdacontent 
337 |a computer  |b c  |2 rdamedia 
338 |a online resource  |b cr  |2 rdacarrier 
490 1 |a Solid Mechanics and Its Applications,  |v 152 
505 0 |a Application 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. 
650 0 |a Materials science. 
650 0 |a Mechanics. 
650 0 |a Mechanics, Applied. 
650 1 4 |a Materials Science, general. 
650 2 4 |a Solid Mechanics. 
700 1 |a Sih, George C.  |e editor. 
710 2 |a SpringerLink (Online service) 
773 0 |t Springer eBooks 
856 4 0 |u https://doi.org/10.1007/978-1-4020-8520-8