Kabir, M. Rizviul and Shahid, Mubeen and Bartsch, Marion (2013) Microstructure sensitive modeling of deformation behavior of a TiAl alloy with variable lamellae thickness. Gamma TiAl Alloys Technology (GAT 2013), 11-14. Juni, 2013 , Toulouse, Frankreich.
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In TiAl alloys the lamellar spacing influences the elastic, plastic, and creep behavior. To predict the alloy behavior a microstructure-sensitive modeling has to be established that is able to capture local plasticity for variable lamellae thickness. The classical micro-mechanical models (e.g., crystal plasticity model) do not contain any structural size-effect; thus, they are not sensitive to the microstructural variation. To overcome this limitation we have introduced intrinsic (material) length scale, as derived from the Tailor dislocation model, in the crystal plasticity constitute behavior. The model allows us to predict local plasticity and global Hall-petch effects as a contribution of statistically stored and geometrically necessary dislocations in the lamellar structures. Based on this model the size-dependency of the lamellar hardening will be presented.
|Document Type:||Conference or Workshop Item (Speech)|
|Title:||Microstructure sensitive modeling of deformation behavior of a TiAl alloy with variable lamellae thickness|
|Date:||13 June 2013|
|Keywords:||Titanium Aluminide (TiAl), modelling, crystal plasticity, microstructure|
|Event Title:||Gamma TiAl Alloys Technology (GAT 2013)|
|Event Location:||Toulouse, Frankreich|
|Event Type:||international Conference|
|Event Dates:||11-14. Juni, 2013|
|HGF - Research field:||Aeronautics, Space and Transport|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||Propulsion Systems|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L ER - Engine Research|
|DLR - Research theme (Project):||L - Virtual Engine and Validation Methods|
|Institutes and Institutions:||Institute of Materials Research > Experimental and Numerical Methods|
|Deposited By:||Dr. -Ing Mohammad Rizviul Kabir|
|Deposited On:||31 Oct 2013 07:09|
|Last Modified:||31 Oct 2013 07:09|
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