Right. So with the surrounding engines of a Saturn V pressing in on the exhaust from the center engine, that exhaust should be contained for a longer time. Hence, higher ISP. That's what an aerospike does. The concentric rings of the Starship booster (and the Starship itself, for that matter) should function collectively like an aerospike. My comment on the bell size is almost an aside. The bell is, in theory, oversized for the environment. I would think that the bells of the innermost engines could just be eliminated (except that they are fired independently during landing).Less expansion is less isp (less efficiency).
The fact that SpaceX has never mentioned the effect tells me that I'm wrong, but the basic rocketry stuff that you've described hasn't convinced me why that is.
I need to sit down with a SpaceX engines guy over a few drinks.
I suspect that they are recessed for reentry more than anything else. Those walls could be constructed as a framework, as with certain Russian rockets that hot fire stages. But SpaceX would have to figure out how to thermally protect the framework, so they just went with solid walls and will use some other technique to vent engine exhaust during hot firing.The ship's engines are recessed because the ship stacks on the booster and test stands so it needs the walls there