I’d wager that the possibly higher TSFC of ws15 was taken into account for the initial design, as ithas always been the target power plant for J-20. It’d be plain stupid not to design the fuel capacity according to what ws15’s supposed TSFC would be.
Still, if we take tsqzsl’s word and treat the extra space as extra fuel, it might mean that PLAAF when deploying ws10-equipped J-20 has found that they can do with some extra fuel for the ws15
(line of thought: ws15 has higher TSFC, thus higher fuel consumption at same thrust, thus lower range than ws10 if all else equal)