# Coriolis Acceleration and Latitude?

We had a lecture on the Coriolis effect today and I am very very confused, this is the first time I've heard of it as such. Anyway, I know that Coriolis acceleration is calculated by $\vec{a} = -2 \vec{\omega} \times \vec{v}$ where $\vert \vec{\omega} \times \vec{v}\vert = \omega v \sin\theta$. This gives $a = -2\omega v \sin \theta$. If I am given a latitude of say, 40°, how do I calculate the Coriolis acceleration of a moving object such as a bus in different directions like due south or due east?

Also, can I use $\omega = \frac{2\pi}{T}$ to calculate $\omega$? Would $T$ be the seconds in a day?

When the Coriolis acceleration is $$\vec{a} = -2 \vec{\omega} \times \vec{v},$$ or $$a =-2\omega v \sin \theta$$ then $\theta$ is the angle between $\vec v$, the vector of velocity and $\vec \omega$, the vector of angular velocity, which always points upwards.

So for example, when you're at the north pole and shoot an arrow horizontally to the earth's surface, $\theta$ is 90 degrees and since $sin(90)=1$, the coriolis acceleration is $a=-2\omega v$.

When you go further in direction of the equator, the angle $\theta$ between the velocity vector and the angular velocity vector increases. At a latitude $\phi$, the angle $\theta$ these two vectors form is $180^\circ-\phi$: Now you have to plug $\theta=180^\circ-\phi$ into the sine in $a = - 2\omega v \sin \theta$. The trigonometric formula gives us

$$sin(180^\circ - \phi)=sin(180^\circ)cos(\phi)-cos(180^\circ)sin(\phi)=sin(\phi)$$ since sin(180°)=0 and cos(180°)=-1.

So at the end you simply have $$a =- 2\omega v \sin \phi$$ which tells you the magnitude of the Coriolis force at a given latitude. When have a bus traveling at 50 km/h at latitude of 40° then this acceleration is a small fraction of the gravitational acceleration.

When you want to know in which direction the force is pointing, you have to consider the cross-product again: when you're traveling from the north to the south (like in the picture), then $\vec \omega \times \vec v$ points into the screen and $-\vec \omega \times \vec v$ out of the screen, so a bus traveling south would be accelerated to the west. When you travel from the east to the west, then the resultant vector points to the north. Or simply put: on the northern hemisphere the Coriolis force deflects always to the right.

For a more intuitive approach why the Coriolis force points to the north when traveling west, see the answer to this question.

(Note that I considered only motion parallel to the earths surface. If you want to drop a ball from a tower it's a bit different.)

Also, can I use $ω=\frac{2π}{T}$ to calculate $ω$? Would T be the seconds in a day?

In principle yes. However, if you do it, then you will get an angular velocity which is slightly lower than the value you get from websites like this. This has to do with the difference between the sidereal and solar day, but I won't go into any details here. (And I think if you only need the first 2 digits it doesn't matter. ^^)

• I'm having trouble understanding how this answer takes the direction of the force into account. Certainly if the velocity is due north-south (with respect to the surface of the earth), then $\varphi = \pi - \theta$. But what if the velocity is due east-west? Isn't $\theta$ (the angle between $\mathbf{v}$ and $\mathbf{\omega}$ always $\pi/2$ in this case? But that would mean that the Coriolis force on an east-west motion is independent of latitude, which is clearly wrong. Can you tell me why I'm confused? Jul 14 '18 at 14:29

Consider the coordinated System $$(\hat{e}_{E}, \hat{e}_{N}, \hat{e}_{r})$$ Where

$$\hat{e}_{E}$$ := unit vector pointing East

$$\hat{e}_{N}$$ := unit vector pointing North

$$\hat{e}_{r}$$ := unit vector normal to the surface of the Earth at the point of longitude

In the inertial reference frame $$\boldsymbol{\omega} = \omega \hspace{1mm} \hat{e}_{N}$$

Then from the plane of the Earth's rotation $$\hat{e}_{N}$$ and $$\hat{e}_{r}$$ are rotated by and angle $$\phi$$

$$\begin{bmatrix}\omega_{r} \\\omega_{N} \end{bmatrix} = \begin{bmatrix}\cos\phi & \sin\phi\\-\sin\phi &\cos\phi \end{bmatrix} \begin{bmatrix} 0 \\ \omega\end{bmatrix}$$

Let $$\overline{v}$$ be the velocity of the mass point in the non-inertial reference frame rotating at the point of longitude. Then $$a_{Coriolis} = -2(\omega\times \overline{v}) = -2(0,\omega\cos\phi, \omega\sin\phi)\times(\overline{v}_{E},\overline{v}_{N},\overline{v}_{r}) =$$

$$-2\omega[(\overline{v}_{r}\cos\phi-\overline{v}_{N}sin\phi)\hat{e}_{E}+\hspace{1mm}\overline{v}_{E}\hspace{1mm}sin\phi\hspace{1mm}\hat{e}_{N}-\cos\phi\hspace{1mm}\overline{v}_{E}\hspace{1mm}\hat{e}_{r}]$$