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I Real life application of Euler's method/numerical method

  1. Oct 2, 2017 #1
    Hi! For my math investigation project, I was trying to predict the trajectory of an object in a projectile motion with significant air resistance by using the Euler's Method. But it seems like the differential equation involved there can easily be separated into different variables, and so it seems unnecessary to use the method.
    Can anyone suggest me a real life situation(related to physics) where differential equations can be given in the form: $$\frac{dy}{dx}=f(x,y)$$
    or any worthwhile idea for investigation using the Euler's method??
  2. jcsd
  3. Oct 2, 2017 #2


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    You could choose isolines like isobars or isotherms like those: https://en.wikipedia.org/wiki/Contour_line
    or the ideal gas law: https://en.wikipedia.org/wiki/Equation_of_state#The_ideal_gas_law_.281834.29

    If you like to look out for other examples, then google "implicit function theorem in physics".

    On the other hand, the more general concept of the calculus of variations is spread all over physics. If you search for "Lagrangian" only on PF, you will probably get hundreds of hits. This way you could even choose by forum section, aka physical area.
  4. Oct 2, 2017 #3


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    I'm not sure how this relates to the OP? Yes, we could consider implicit differential equations, but since it was asked
    I think there may be easier ways towards examples.

    Most pieces of text discussing the numerical solution of ODEs will start with Euler. Any such text that includes physics examples (from classical mechanics or circuit theory, for instance) will be worth a look.

    By the way, it is not bad (actually: it is typical) to start with an example that can (also) be solved analytically. This way you can assess the quality of the numerical method.
  5. Oct 3, 2017 #4
    Thanks for your reply!
  6. Oct 3, 2017 #5
    Thank you for your advice! I decided to justify the motive behind the project by saying that I would like to evaluate the usefulness of the Euler's method in real life applications.
  7. Oct 3, 2017 #6

    I like Serena

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    Hi ChanYoung Park! Welcome to PF! :)

    Projectile motion with significant air resistance (##\propto v^2##) seems to be a good example, which is not solvable analytically as far as I know.
  8. Oct 4, 2017 #7
    Euler's method is not stable, and for that reason it is never recommended. It is often discussed because it gives a lot of insight into the nature of numerical solution of ODEs, but something better must always be used to obtain a usable solution.
  9. Oct 5, 2017 #8


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    In chemical reaction kinetics, there can be situations where ##c_1 ,c_2## (the concentrations of substances 1 and 2) develop according to coupled equations

    ##\frac{dc_1}{dt} = f_1 (c_1 ,c_2 )##
    ##\frac{dc_2}{dt} = f_2 (c_1 ,c_2 )##,

    and then you can try a modification of the Euler's method where both ##c_1 (t)## and ##c_2 (t)## are evolved on each timestep. The pair of equations can't be solved analytically in all cases, so a numerical solution is often necessary. The stability problem sometimes causes difficulties and sometimes not.
  10. Oct 6, 2017 #9
    Euler's method is commonly used in projectile motion including drag, especially to compute the drag force (and thus the drag coefficient) as a function of velocity from experimental data. Keep in mind that the drag coefficient (and other aerodynamic coefficients) are seldom really constant. They vary with velocity over the velocity ranges that most projectiles experience in flight. If one has experimental data for position and velocity vs. time from Doppler radar or for position vs. time from sufficiently fast video, Euler's method is common for inferring the drag force and coefficient.

    In real life, one can also use Euler's method to from known aerodynamic coefficients to predicting trajectories. Three degree of freedom (3DOF) models are usually called point mass models, because other than drag acting opposite the velocity vector, they ignore the effects of rigid body motion. These are most amenable to Euler, because computers are fast enough to take small step sizes needed for the method. There are also 4DOF (modified point mass) and 6DOF models for spin stabilized rigid bodies in flight. Knowing the aerodynamic coefficients accurately is actually the harder part of making accurate predictions of the rigid body effects, but better approximations than Euler (such as 4th order Runge-Kutta) are usually used. Computing time can begin to be an issue in 6DOF models, so a method is needed to improve accuracy without just making the time steps smaller and smaller.
  11. Oct 6, 2017 #10
    I have a simulation (7 coupled ODEs in 7 unknowns) that I have run many times using a 5th order Runge-Kutta-Feldberg with variable step size, and it runs in about 2 to 3 seconds. Of course, I have the benefit of an antique Dell Optiplex computer, about 12 years old, so I don't have the additional speed of more recent technology. I really cannot fathom why anyone today is considering actually employing Euler's Method which is known to be unstable.
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