LetAt maximum pressure, the stress is the field from part (c) with and . Under the assumed elastic unloading, previously accumulated plastic strain is frozen. Therefore it is the stress increment, rather than the total stress, that satisfies homogeneous linear elasticity and radial elastic compatibility. Applying the superposition principle, a pressure change produces the elastic incrementsThey have zero far-field stress and change the wall traction from to . These increments are the same in the formerly plastic and formerly elastic regions because their elastic Lamé parameters agree. Adding them to the maximum-load field givesandThese formulae retain : it records the plastic loading history and is not the instantaneous loading-front formula with substituted for . If the entire return is elastic, setting gives the residual stress after removal of the applied pressure.
To check admissibility, examine the signed difference of the principal stresses in the formerly plastic shell:It immediately moves into the interior of the Tresca yield criterion when unloading starts. It can next reach the opposite limit . For fixed , is largest at and stays above . At the wall,There is no earlier violation in the outer region. Indeed,so its magnitude is no larger than , which has already been controlled by the shell calculation. Hence the first reverse yielding occurs at the cavity wall, withIf , the stress stays within the yield surface throughout unloading to zero. If , it reaches reverse yield exactly at ; further unloading would produce reverse plastic deformation. If , reverse plastic deformation starts while the applied pressure is still positive. ThusIf “yield again while unloaded” includes first touching the yield surface at the final endpoint, the corresponding condition is . The displayed elastic unloading fields are physically valid only for ; beyond that interval a new reverse-plastic region must be solved for. Continuing the elastic formula to when would violate the given Tresca yield criterion.
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