The present work suggests a methodology for construction of stress rupture
ductility diagram using the concept of geometrical factor k that determines
the nature of creep rupture. Large volumes of stress rupture ductility dat
a of a range of engineering materials generated experimentally in the labor
atory and reported in the literature have been used to study the nature of
creep rupture by superimposition of these data on the above diagram.
The rupture ductility of Ni-base superalloy, when superimposed on such diag
ram, indicates that the failure in this alloy could be due to limited amoun
t of localised deformation or cavitation. In case of Zr-Nb alloy, the ruptu
re ductility data lie in the necking regime extending from k=0.9 to 0.4. In
contrast, the data on Cr-Mo steel show a wider variation extending from th
e regime of cavitation to extensive necking.
Reliable prediction of rupture ductility is possible within a narrow range
of k in which the nature of creep rupture remains the same.