structure troubles.
ranging from flutter to overloaded airframe.
btw, if you increase the every dimension of the size by 1,41, the weight still grows with THIRD ???square??? X*X*X not just X*X second square that the effective area (for lift and drag calculus)
thus while the lift increases 1,41*1,41 the weight increases 1,41*1,41*1,41 for ALL materials. thus you won't double the bomb load, and the structure rigidity goes down the drain, too
>I don't think the weight would increase by x2.8, - don't forget the aircraft skin will stay the same thickness ( and not be made 1.41 times thicker and the fuel load will be double for 4 engines instead of 2 - and not x2.8 )<
no the skin won§t stay the same thickness, it would need to be MORE than 1,41 of original.
you cannot simply inflate the original design to bigger size without resizing the internal structure carrying the load. actually, you need MORE than inflating the structure size by MORE than the inflate ratio of dimensions, to keep the construction corelating with the loads, if not aerodynamic then just the plain mass.
IF you really "understand" the aircraft construction so much that you don't see the calculus above, you should stick to the three present answers "It's not that simple"
in layman terms, inflating the dimensions without changing internal structure = weakening the construction
as demonstrated, not even the strengthening of construction by the ratio equal to the size inflation helps to keep the construction at the same performance.
the rigidity of the beam/spar depends on the length/heigth ratio, influenced by presence or absence of reinforcing elements along the beam.
doubling the length of beam requires (more or less) doubling the height (and the width). hereby, the mass of beam itself increases 2*2*2 eight times, for the doublesized beam, or 1.4*11.4*1.4 in your ratio. the weight need to be carried, so the increase in weight of beam has to be deducted from the total load. hence, the net /transported/ load decreases, and structure is weaker.