There are several problems with gasohol outside the core engine, from compatibility with fuel systems (bladders etc.), to phase separation, to vapor lock, to hygroscopicity. I'm sure that can be designed around, but it's not a drop-in replacement in planes designed for avgas.
If you want an abundant and affordable fuel, in the aviation world that's Jet A(-1). There's some limited success with Jet A burning diesel engines for the GA market (Thielert (or whatever they're called today) and Austro mainly).
Personally I think it would be cool if turbines suitable for GA would be developed. Currently turbines cost an arm and a leg, but I think partially that is an effect of development focused on power/weight and fuel efficiency, cost be damned. That might suit commercial and military use, but not GA. And yes, turbines don't scale down very well either. Still, a turbine that would have an upfront cost competitive with current GA engines would be very attractive, even if it would come at a cost in fuel efficiency. That would be, I think, more than compensated by the power/weight and safety advantages, as well as fuel availability and affordability. I think there are a couple of companies working in this space (TurbAero and Turbotech that I'm aware of, maybe others as well), we'll see if any of them ever come to fruition.