This is NOT a homework question, there are few informations that I found on the Internet about this specific case of the Coriolis Force
We currently are dealing with the Coriolis Force, and I struggle to understand how to calculate the force when moving east or west ALONG the Equator. I know that the force is zero when moving north or south at the Equator, because the Latitude Angle used to calculate the force is zero.
I know that generally $$F_c = -2m (\Omega \times \overrightarrow{v})$$ where Omega is the Angular Velocity, in the case of Earth it is $\frac{2\pi}{24\cdot 60 \cdot60}$ because we divide the period by the total time in seconds it takes for Earth to go around, so one day. And $\overrightarrow{v}$ is the velocity vector. The resulting force $F_c$ points perpendicular to both velocity and angular velocity
I also know that if moving tangetially along the Surface of earth, the formula is $$F_c = 2\cdot m\cdot v \cdot \omega \cdot \sin{\phi}$$ where $\phi$ is the latitude at which the object lies. So at the Equator, $\phi = 0$ so obvisouly $\sin\phi$ is also zero.
But there is a Coriolis Force when moving East or West along the Equator, I know it is directed inside the Earth when moving West, and directed toward outer space when moving East. But how I am supposed to calculate it in this case ? The latitude angle is zero, so I can't use the formula above even tough we are also moving tangetially along the surfcae of Earth
I would really appreciate any support, because either I didn't find it, or there are only few informations about this specific case of the Coriolis Force on the Internet
Thanks a loot for your help, feel free to comment if anything is unclear