Please use this identifier to cite or link to this item: http://dspace.iitrpr.ac.in:8080/xmlui/handle/123456789/4960
Full metadata record
DC FieldValueLanguage
dc.contributor.authorMishra, A. K.-
dc.date.accessioned2025-10-26T12:36:56Z-
dc.date.available2025-10-26T12:36:56Z-
dc.date.issued2025-06-27-
dc.identifier.urihttp://dspace.iitrpr.ac.in:8080/xmlui/handle/123456789/4960-
dc.description.abstractAustenitic stainless steel is the preferred material for permanent components of sodium-cooled fast breeder reactors due to its high-temperature tensile and creep strength, compatibility with liquid sodium, ease of fabrication, and weldability. Type SS316LN containing 0.02–0.03 wt.% carbon and 0.06–0.08 wt.% nitrogen is designated as SS316LN. The metallic materials exhibit time-dependent deformation in high-temperature applications of fast breeder reactors (FBR), such as primary and secondary piping, heat exchangers, and the main vessel. To ensure the structural integrity of these components, it is important to understand the crack behavior and the resistance offered by the materials used in these components. In creep conditions, conventionally, C* and Ct parameter are used for characterizing the crack tip. However, the true crack driving force or its rate cannot be described by any of the conventional parameters. The theoretical validity of conventional crack tip-characterizing parameters like Ct and J is also restricted, making it hard to anticipate underlying cracks driving forces. To investigate the creep crack growth behavior of this material, an experimental and numerical analysis of SS316LN is performed with different constraint conditions. This study explores the influence of in-plane constraint on the creep crack behavior of a SS316LN with 0.07% nitrogen under stationary and growing cracks through experimental and numerical approaches. To examine constraint Q parameter is calculated to characterize the in-plane constraint, while the C∗ parameter is used to analyze creep deformation and fracture behavior. Comprehensive experimental tests and finite element simulations provide insights into the interaction between in-plane constraints and crack-tip stress fields. The results enhance the understanding of constraint effects in stationary crack scenarios, contributing to the development of improved methodologies for high-temperature failure assessments and life prediction of structural components made of SS316LN.en_US
dc.language.isoen_USen_US
dc.subjectCreep Crack Growth (CCG)en_US
dc.subjectConfigurational forcesen_US
dc.subjectDriving forceen_US
dc.subjectConstrainten_US
dc.subjectSS316LNen_US
dc.titleCharacterizing crack using configurational forces and assessment of constraint in SS316LN (0.07)en_US
dc.typeThesisen_US
Appears in Collections:Year- 2025

Files in This Item:
File Description SizeFormat 
Full_text.pdf.pdf5.61 MBAdobe PDFView/Open    Request a copy


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.