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6 Results and Discussion   177


























                  FIGURE 7.14
                  True stress versus true plastic strain of Zircaloy-4 fuel-clad tube at room temperature.

                     The load-displacement response of the specimen in the conical mandrel test setup
                  (as calculated from FE analysis) is shown in Figure 7.17. This behavior is similar to
                  the experimental data. Initially, the load is very small for an applied mandrel dis-
                  placement of  23 mm due to limited contact of the mandrel with the specimen
                  crack-tip. When the crack-tip is in full contact with the conical loading mandrel,
                  the load rises sharply and hence, there is large-scale plastic deformation at the
                  crack-tip as can be seen from the large values of von Mises stress and plastic strain
                  near the crack-tip in Figures 7.15 and 7.16, respectively. The extent of frictional dis-
                  sipation can be computed through FE analysis from the difference of area under load-
                  displacement curves (i.e., FE analysis with and without friction) as shown in
                  Figure 7.18. It can be observed from Figure 7.18 that the extent of frictional in
                  the test setup with conical mandrel is large and it is of the order of 40% of the total
                  energy used (in the experiment) by the specimen for ductile crack growth.
                     Thefractureresistancebehavior(intermsofJ-Rcurve)isevaluatedforthetwotypes
                  of axially cracked fuel-clad specimens, that is, specimens with total length of 50 and
                  100 mm, respectively, and these are shown in Figure 7.19. It can be observed that J-
                  R curve is almost independent of the total length (W) of the specimen as the effective
                  remaining ligament length is small compared to the actual remaining ligament length.



                  6.3 RESULTS OF TEST SETUP WITH PAIR OF SPLIT
                  SEMI-CYLINDRICAL LOADING MANDRELS
                  The load-displacement curves as obtained from the tests with semi-cylindrical load-
                  ing mandrels (Figure 7.8) are presented in Figure 7.20. The displacement is measured
                  through a COD gauge mounted at the right-end opening of mandrels as shown in
                  Figure 7.8b and the measurement of load is taken directly from the load cells. As the
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