This is equations of motion in $3D:$ How can we numerically solve this system of the equations? (preferably Euler). can you give a sample of $2$ step sizes how is it possible?
$\frac{d^2x}{dt^2} = -vk_d\frac{dx}{dt} + vk_l\frac{dy}{dt}$
$\frac{d^2y}{dt^2} = -vk_d\frac{dy}{dt} - vk_l\frac{dx}{dt}$
$\frac{d^2z}{dt^2} = -vk_d\frac{dz}{dt} - g$
$v = \sqrt{(\frac{dx}{dt})^2 + (\frac{dy}{dt})^2 +(\frac{dz}{dt})^2}$
$g, k_d, k_l$ are constants.
step size = $0.01$ sec = $t$
Intial Conditions:
x,y,z = 0
$\frac{dx}{dt}=10.45$
$\frac{dy}{dt}=5.45$
$\frac{dz}{dt}=33.45$
$v_0=25$
In python (and similar in other languages) you would encode the ODE function of the right side, for the first order system with $v_x=\dot x$ etc., as
and pass it along to any general-purpose solver, which might be one implementing the Euler method, or RK4, or some higher order method with adaptive step size.
If you use implementations similar to those in Does fourth-order Runge-Kutta have an higher accuracy than the second-order one? you need to wrap the result list in a vector type, for instance
numpy.array, either in the return line or in the function call. For further inspiration on getting the trajectories as list see https://stackoverflow.com/questions/61333687/how-do-i-solve-a-2nd-order-differential-equation-for-projectile-motion, https://stackoverflow.com/questions/53645649/cannot-get-rk4-to-solve-for-position-of-orbiting-body.