000 | 04049nam a22005175i 4500 | ||
---|---|---|---|
001 | 978-0-387-95924-5 | ||
003 | DE-He213 | ||
005 | 20170628033408.0 | ||
007 | cr nn 008mamaa | ||
008 | 100301s2009 xxu| s |||| 0|eng d | ||
020 |
_a9780387959245 _9978-0-387-95924-5 |
||
024 | 7 |
_a10.1007/978-0-387-95924-5 _2doi |
|
050 | 4 | _aTA405-409.3 | |
050 | 4 | _aQA808.2 | |
072 | 7 |
_aTG _2bicssc |
|
072 | 7 |
_aTEC009070 _2bisacsh |
|
072 | 7 |
_aTEC021000 _2bisacsh |
|
082 | 0 | 4 |
_a620.1 _223 |
100 | 1 |
_aFarahmand, Bahram. _eeditor. |
|
245 | 1 | 0 |
_aVirtual Testing and Predictive Modeling _h[electronic resource] : _bFor Fatigue and Fracture Mechanics Allowables / _cedited by Bahram Farahmand. |
264 | 1 |
_aBoston, MA : _bSpringer US, _c2009. |
|
300 |
_aXXIII, 407 p. _bonline resource. |
||
336 |
_atext _btxt _2rdacontent |
||
337 |
_acomputer _bc _2rdamedia |
||
338 |
_aonline resource _bcr _2rdacarrier |
||
347 |
_atext file _bPDF _2rda |
||
505 | 0 | _aVirtual Testing and Its Application in Aerospace Structural Parts -- Tools for Assessing the Damage Tolerance of Primary Structural Components -- Cohesive Technology Applied to the Modeling and Simulation of Fatigue Failure -- Fatigue Damage Map as a Virtual Tool for Fatigue Damage Tolerance -- Predicting Creep and Creep/Fatigue Crack Initiation and Growth for Virtual Testing and Life Assessment of Components -- Computational Approach Toward Advanced Composite Material Qualification and Structural Certification -- Modeling of Multiscale Fatigue Crack Growth: Nano/Micro and Micro/Macro Transitions -- Multiscale Modeling of Nanocomposite Materials -- Predictive Modeling -- Multiscale Approach to Predicting the Mechanical Behavior of Polymeric Melts -- Prediction of Damage Propagation and Failure of Composite Structures (Without Testing) -- Functional Nanostructured Polymer–Metal Interfaces -- Advanced Experimental Techniques for Multiscale Modeling of Materials. | |
520 | _aVirtual Testing and Predictive Modeling: For Fatigue and Fracture Mechanics Allowables provides an overview of cost and time efficient methods in generating the fatigue and fracture data of industrial structural parts. Readers will find a systematic introduction to virtual testing to generate fatigue and fracture allowables through two useful techniques: the conventional continuum mechanics approach, and the utilization of multiscale modeling and simulation techniques to predict materials’ properties. In addition, a chapter devoted to the functionalization process covers the current approach to this technique, which strengthens interface durability through bonding dissimilar materials. Coverage of verification methods, used with devices such as the Transmission Electron Microscope (TEM) and the Atomic Force Microscope (AFM), are also described, which motivate discussion of the fundamental structure and deformation processes of nanoscale materials. The virtual testing continuum approach already plays a crucial role in the life assessment of important manufactured structural parts in the aerospace, automotive, aircraft and defense industries when data is inaccessible to engineers. Virtual Testing and Predictive Modeling: For Fatigue and Fracture Mechanics Allowables provides a unique applications-focus view into these valuable methods, filling a critical void in references currently available. | ||
650 | 0 | _aEngineering. | |
650 | 0 | _aMechanics. | |
650 | 0 | _aMaterials. | |
650 | 0 | _aMechanical engineering. | |
650 | 0 | _aSurfaces (Physics). | |
650 | 1 | 4 | _aEngineering. |
650 | 2 | 4 | _aContinuum Mechanics and Mechanics of Materials. |
650 | 2 | 4 | _aCharacterization and Evaluation of Materials. |
650 | 2 | 4 | _aMechanics. |
650 | 2 | 4 | _aAutomotive Engineering. |
650 | 2 | 4 | _aStructural Mechanics. |
710 | 2 | _aSpringerLink (Online service) | |
773 | 0 | _tSpringer eBooks | |
776 | 0 | 8 |
_iPrinted edition: _z9780387959238 |
856 | 4 | 0 | _uhttp://dx.doi.org/10.1007/978-0-387-95924-5 |
912 | _aZDB-2-ENG | ||
999 |
_c14997 _d14997 |