I need to change one thing on my previous post, gravity is a constant, thus, if DRAG ratio, and WEIGHT ratios are the same, the airframes would accelrate at exactly the same rate, reference the experiment done by NASA on the moon, a feather, and a hammer, were both dropped. (In a vacuum with no drag). They both hit the ground at the exact same moment. On earth, the rate of acceleration in descent is goverend by drag, not weight.
Sol
ok but we have not included drag ratio as a constant, or i haven't in this discussion ...
Thorism.
It has become increasingly obvious you have little to no understanding about the subject matter.
Crack a book.
Take a class.
Take the time to better yourself on the subject.
In a few weeks (months/years) when you finally have a basic grasp on it all please post on this subject again.
We will happily accept your apology at that time.
you are once again projecting as i am not anywhere discounting factors brought up by others.
ok so let me see if i can make the bridge here ...
since by the math the planes would perform the same, but also since the engineering problems make the path of least resistance the smaller lighter one, that is why the tendency is to smaller lighter when maneuverability is the key design desire.
the lack of good examples are self explanatory, after some more thought, as why would anyone design a fighter or aerobatic plane larger than it needs to be. so if the fighter is larger there is most likely some other design priority requiring it to be larger, and in that case all the loadings will not match up anyway.
now i take your point about isolating factors.
in-fact i think that is what drags me into these round and round discussions as in the case of this discussion after review as the turn radius caused one to post the preference for the f4u in the "turn fight" however as i and many others expressed when maneuverability is taken in as more than turn radius terms the other factors may make that not the best course of action, and in this case i thought that in most instances the hog had a greater advantage set in a boom and zoom fight vs. the 109.
BnZ mistook my post and the round and round discussion started.
i still have my scaling concerns but i will concede that there are no practical examples, and probably shouldn't be, and that weight and size are well enough represented with the loadings for all but the most theoretical of discussions that as stated have no real world examples for us to examine.
i think that is where i will leave this, if you guys don't mind.
+S+
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