Can anyone verify for me whether the shape of the nose tank is different on the pre-war B model airplanes compared to the post-war B model airplanes?
Could the lower part of the tank have a steeper slope on the later airplanes?
This would explain a LOT about the previous engine issues I've been having. If the pre-war tanks have a shallower slope, then on takeoff acceleration the head pressure would be less than a post-war tank with a steeper slope.
Could the lower part of the tank have a steeper slope on the later airplanes?
This would explain a LOT about the previous engine issues I've been having. If the pre-war tanks have a shallower slope, then on takeoff acceleration the head pressure would be less than a post-war tank with a steeper slope.
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