It is certain that the designer had that in mind when they designed it. The core stage has 7 (odd number) engines, with one in the center. Considering YF-100's current throttle range is down to 65%. VTVL capability is just a matter of priority.
This is probably also why the design from 8th Academy failed. It has 4 engines in a 3.8m core. This is also why I said in an earlier post that I don't want and I don't believe this new rocket from 8th is going to go beyond the brochure.
Yes the configuration of the cores certainly seem like they were designed with VTVL in mind.
Though I think they could go a bit further with CZ-5DY's potential for reusability -- specifically, I think if all three cores were "identical" in terms of their fuel tanks and their external shaping that would allow all of the cores to be used individually as standalone rockets (like the Falcon 9 to Falcon Heavy relationship). In fact I'm not sure if the asymmetrical tip of the CZ-5DY's two booster cores would allow for a reliable VTVL to be carried out for the booster cores.
Personally I'm of the opinion that in the medium to long term, prioritization and standardization on reusable capable CZ-5DY (in triple and single booster form) and reusable capable CZ-9 (with the sixteen YF135s) should be the optimal family for state rocket types (outside of rapid response and solid fuel rockets).
Having too many different rocket types is a waste of money, and consolidating the product line to 3-4 main reusable rockets capable of deploying larger single payloads per launch (or multiple smaller payloads per launch) is the way forwards.
I would even say that from a technological point of view, it is more important to achieve reliable large payload orbital launches at fast pace (i.e.: reusability) rather than pursuing lunar+interplanetary ambitions, if they were forced to choose between them.