The problem is with any external tank, because there is a reason why miliatary airplanes in particular are made aerodynamic. The slipper tank, particularly the big one, decidedly isn't.
The rear fuselage tank would be Ok except that it causes severe stability issues in the Spitfire (and in a P-51)
What they really needed was a wing tank, a real one not that tiny one they used, but that would have required a new wing.
Which is where we started.
Again you are arguing for the sake of arguing, who cares where the fuel is, there is plenty of room in the rear fuselage and by the time you are at 25,000ft and set up for cruise it's down around 30G so instability is a mute point. You seem determined to make a non issue a major one.