Recent content by MaceLee

  1. M

    Calculators What Graphing Calculator Should I Buy for Pre-Calc and Physics?

    If you're going to buy a new calculator I would recommend the TI nspire CAS as it does pretty much everything. It's what I use currently to check all my answers.
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    What Does Stationarity Mean in the Context of the Euler-Lagrange Equations?

    I would assume it means that the action s = \int Ldt is a stationary point (i.e. a min most likely as the action is minimised in real systems). You might want to wait for some confirmation however as I haven't studied Lagrangian mechanics in too much depth.
  3. M

    Modelling an Aeroplane - Non-Linear Differential Equation

    Ah, indeed. Prior to being told about using limits, I had no idea that you could do so in separation of variables - so I assumed it would work the same way in all cases. Regardless, the overall result an equation which fits the data well; v_0 ends up as you said, around 140. I've just...
  4. M

    Modelling an Aeroplane - Non-Linear Differential Equation

    Just tried it all in excel. It gives great results :D Thank you very much ehild! Life saver :)
  5. M

    Modelling an Aeroplane - Non-Linear Differential Equation

    Oh yes, 3 \lambda was written incorrectly, it should have been: 3 \lambda = \frac{103.02}{120000} Sorry about that D: The units are standard, v in ms^-1 and t in seconds. The breaking started at t=10 onwards yes. Your attached graph is a really close fit! I'll try out your new function...
  6. M

    Modelling an Aeroplane - Non-Linear Differential Equation

    \mu = \frac{301687.25}{120000} 3 \lambda = 103.02 v_0 was set as to satisfy when t = 10, v = 50
  7. M

    Modelling an Aeroplane - Non-Linear Differential Equation

    Thanks ehild. I tried to use the solution to find predictions for experimental data, but the values are extremely strange. I'm not sure if it's the way I've worked out v_0, but seemingly regardless of the value, the output jumps around really weirdly. The data I'm supposed to be modelling...
  8. M

    Modelling an Aeroplane - Non-Linear Differential Equation

    Ah silly mistake, I took the tan separately. Thanks again ehild.
  9. M

    Modelling an Aeroplane - Non-Linear Differential Equation

    Just one last thing! Taking the tangent of both sides gives: kv(t) = kv_0 - tan(\mu t) Taking the k to the other side gives: v(t) = v_0 - \frac{1}{k} tan(\mu t) Where did the denominator come from in your solution? Was it a mistake? Or did I do something wrong again :/ ? Thanks!
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    Modelling an Aeroplane - Non-Linear Differential Equation

    Thank you so much, ehild & RoyalCat. I had tried by differentiating it and getting a solution from the second order linear - it works for a few values but then suddenly goes wildly astray. :)
  11. M

    Modelling an Aeroplane - Non-Linear Differential Equation

    I've been trying for the past day but still can't solve this equation: \dot{v} = -\gamma v^2 - \lambda Where \gamma and \lambda are known constants Could anyone help me please? Thanks!
  12. M

    Modelling an Aeroplane - Non-Linear Differential Equation

    I've just moved onto the second equation and I'm trying to solve it: \dot{v} = -3\lambda v^2 - \mu Where \lambda and \mu are known constants. I tried to solve it as follows: 3\lambda \int^v_{v_0}v^2 dv = -\mu\int^t_{0}dt Giving: \lambda v^3 - \lambda v_0^3 = -\mu t Resulting...
  13. M

    Modelling an Aeroplane - Non-Linear Differential Equation

    I see; your solution is indeed much neater. Very much appreciated, I'll remember that in future :) Thanks
  14. M

    Modelling an Aeroplane - Non-Linear Differential Equation

    I just tried that out, it would seem that the equation isn't plausible. I'll give it another go with linear drag instead. Thanks!
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