It may be iterative, but you can’t simply slap a fan section onto an old turbojet core that was never developed to be a turbofan. The whole engine works as one integrated component. Treating components as modular when they’re not designed as such is one reason why the WS-10’s development process was such a nightmare. Mix and match isn’t a good way to do jet engine design when your downstream mechanisms have high dependency on your upstream mechanisms, unless you explicitly design such components with such flexibility in mind first.