I am a little confused by this range chart. Why does it seem like the fuel burn rate is greater with the 108 gallon belly tank than with two 150 gallon wing tanks? The average fuel efficiency round trip with 413 gallons of fuel is 1.45 mpg, while with 605 gallons it is 1.65 mpg. Wouldn't the two larger wing tanks cause more aerodynamic drag than the single belly tank and thereby decrease fuel efficiency, or am I missing something here?
From what I can gather, with small total fuel capacity, the increased percentage of that fuel was used on high power/high consumption engine settings (take-off, climb, combat), while cruising part was not that long - thus total flight mileage was not that good.
With total fuel capacity greatly increased, a small percentage of fuel was used on high power engine settings, and much greater percentage of fuel was used on cruising - the total flight mileage improved.
Note that required combat time was 5+15min for both cases (108 gal or 300 gal of external fuel), and fuel reserve was the same (30 min). The difference in consumption per hour in hi-power and cruising settings was approx 2:1 up to 4:1.