Quote:
Originally Posted by InfiniteStates
These equations must apply to a specific plane, rather than general equations. Hence the constants, which are probably the result of wing equations for this specific plane. Otherwise, you mean to tell me that a plane's wingspan and surface area have no effect on it's ability to turn?
LOL thank you. You just disproved your statement ("Actually.. both turn radius and rate of turn have nothing to do with lift, but a lot with speed."), and reinforced my argument that the 153 can turn tighter because it has more lift due to having 2 wings instead of 1.
EDIT: thus, making it a cheap plane to whore in online matches. I rest my case 
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Agreed, that statement was incorrect in retrospect. Again, the general rule to aviation forces is: everything affects everything. Conclusion: you, Soviet and me were all right: you need low speed for the best turn, and high lift to maintain it.
P.S.: The formula goes for every plane, you'll just have to check if the airspeed and bank angle used can actually be maintained in a constant non-accelerated flight. E.g. you can't say 'A Spitfire has a turn radius of 14 ft if you fill in v = 30kt and bank angle = 80 degrees', because the Spit can't fly 30 kts with a bank angle of 80 degrees while maintaining altitude and a coordinated turn.
The constant was for conversion so the answers would be in knots and feet.