xodin
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LastOneStanding said:Actually, I lied: you just have to refer to a table of standard derivatives to see that: [itex]\frac{d}{dx}arctanh(x) = \frac{1}{1 - x^2}[/itex]. You can check this if you like. Your calc textbook should also have a proof of this in it. Now just rescale the variables appropriately and you get the result.
Ah, ok, I think I'm getting close now! Great stuff on the terminal velocity too, that part makes total sense, thanks again!
[itex]\frac {1}{a} \int \frac {dv}{1-\alpha^{2} v^{2}} = t_{0} + t[/itex]
[itex]\frac {tanh^{-1}\left(\alpha v\right)}{a} = t_{0} + t[/itex]
Ignoring [itex]t_{0}[/itex]:
[itex]tanh^{-1}\left(\alpha v\right) =a t[/itex]
[itex]\alpha v = tanh\left(a t\right)[/itex]
[itex]v = \frac {tanh\left(a t\right)}{\alpha}[/itex]
Somewhere I lost an alpha! :P