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      https://www.ias.ac.in/article/fulltext/sadh/036/02/0223-0249

    • Keywords

       

      Nimonic C-263 alloy sheets; microstructure; texture; tensile deformation; in-plane anisotropy; yield loci; work hardening; deep drawability.

    • Abstract

       

      An effort has been made to comprehensively evaluate and rationalize the in-plane anisotropy in tensile properties and the effect of aging on the nature of deformation (strain hardening behaviour) and formability characteristics, especially the limit drawing ratio and forming limit diagram. Despite weak crystallographic texture and excellent ductility and high work hardening exponents, the alloy sheets of C-263 exhibit significant extent of in-plane anisotropy in its tensile properties and yield loci. The absolute magnitudes of yield stress and the exact nature of anisotropy that can be predicted from the tensile part of the yield locus need to be employed with caution. This is because when the magnitudes of the yield stresses, obtained from yield locus are more than 5 times higher as compared to the yield and ultimate tensile strength values and the nature and degree of in-plane anisotropy under tensile loading matches with that of only the compressive yield stresses of yield locus. The alloy sheet, due to weak crystallographic texture and relatively high strengths, is found to be far more suitable for structural applications, rather than for deep drawing applications, which was reflected in low limit drawing ratio values (1.34 for CR+ST and 1.23 for peak aged conditions). Further, the study conducted reveals that the safer forming limits in strain space is higher for CR+ST condition; while, the safer forming limits in stress space are higher for peak aged (CR+ST+1073 K/8 h) condition. Finally, detailed studies are outlined to arrive at suitable microstructural and textural characteristics that provide significantly enhanced drawability in the Nimonic C-263 alloy sheets.

    • Author Affiliations

       

      K Ankamma1 D V V Satyanarayana2 G Chandramohan Reddy1 M Komaraiah3 N Eswara Prasad4

      1. Mechanical Engineering Department, Mahatma Gandhi Institute of Technology, Hyderabad 500 075, India
      2. Defence Metallurgical Research Laboratory, DRDO, PO Kanchanbagh, Hyderabad 500 058, India
      3. Malla Reddy College of Engineering and Technology, Hakimpet Post, Secunderabad 500 014, India
      4. Regional Centre for Military Airworthiness (Materials), CEMILAC, DRDO, PO Kanchanbagh, Hyderabad 500 058, India
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