Shortround6
Major General
Excellent points on the Hungarian and Rumanian engines. The original GR 14K had some trouble of its own. Especially oil leakages IIRC.
The big problem with GR 14K and ALL of it's derivatives was the two bearing crankshaft. The First G-R 14 cylinder engines were running in 1929 and the fuel available was more like 70-77 octane. Metals available were not what they would be in 5 years let alone 10 years. The two bearing crank on a twin row engine is simply not enough to support either high cylinder pressures or high rpm let alone both. It does allow for a shorter, lighter engine compared to a 3 bearing design. It was a competitive design in the early 30s but the lack of development potential limited it to about 1000-1100hp no matter who made it or what they fed it for fuel. You could put all the fins you want on the cylinders and heads but if the crankshaft failed it was 'game over'.
That also brings me to another point. I said before that the main problem with Italian high-powered aircraft engines was the lack of metal alloys. You seem to steer more in the direction of a lack of high-grade fuel as the main limitation to achieve the necessary boost, like the Allies and Germans could use on their engines.
It may be a bit of both. Power is air flow per minute. High rpm and/or high boost (more air per revolution of the crank) Lack of good alloys may limit the rpm of the engine, Bearing metals or strength of the crankshaft/connecting rods. If you can't use rpm and all you have is 87 octane fuel, which puts a limit on allowable cylinder pressures ( boost and compression ratio) you are about out of options, except to make really large displacement engines ( more air per revolution of the crank and low pressures).