Recently I’ve been trying to make oblique wing aircraft, what inspired me was an artwork of an oblique wing interceptor concept for the U.S. Navy, I tried making one side of the wing smaller than the other so the center of lift would be closer to the middle but even then it would still wanna roll off to the left when the wing was at 70°, my guess to why it’s happening is the airflow starting off strong at one side and becoming weaker the farther it goes down the wing but I’m not sure, does anyone know how to fix this?
The wing area on one side should equal the opposite otherwise a rolling moment is produced. Sweeping the entire wing assembly on a middle pivot point won't adversely affect the CoL location, at least not by a significant margin. That assumes that one side is swept forward and the other sweeps backward