I'm unclear on how moving the engine up causes application of power to cause the attitude to tend to go nose up. I would expect the opposite to happen. I think something else must have changed such as the center line of the engine relative to the center line of the plane. Or did moving the engine forward at the same time cause this effect?
I don't think it does. Other sources I've read suggest the larger nacelle introduces a pitch up during certain flap configurations and at a high angle of attack. It's not the engine thrust that's the problem, but the drag due to the large and further forward nacelle. That's the justification for the MCAS software. https://theaircurrent.com/aviation-safety/what-is-the-boeing...
The point about lift from the engine nacelles was that it acts as positive feedback: if you are already pitched too high, it acts to worsen the problem. And, because it is farther forward, it has a greater lever arm to act.