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The Earth Presses Every Train Sideways

Irodov 1.116DifficultyDifficulty 3 of 5UniquenessUniqueness 3 of 5

Problem Irodov 1.116

A train of mass mm travels at northern latitude φ\varphi, in the reference frame that rotates with the Earth (angular velocity ω\omega, radius RR).

  1. If the train runs along a meridian at speed vv, find the magnitude and direction of the sideways force it presses on the rails with.

  2. Find the compass direction and the speed at which the train would have to travel so that the vector sum of the centrifugal and Coriolis forces on it, in the Earth-fixed frame, vanishes completely.

A meridian section of the Earth (center O, radius R), turning at ω about the dashed polar axis. The train sits at latitude φ, running along the meridian, so its velocity v (charcoal) lies in the plane of the page.

A meridian section of the Earth (center OO, radius RR), turning at ω\vect\omega about the dashed polar axis. The train sits at latitude φ\varphi, running along the meridian, so its velocity v\vect v (charcoal) lies in the plane of the page.

Given
  • m=2000m = 2000 t =2.0×106= 2.0\times10^6 kg
  • φ=60∘\varphi = 60^\circ
  • v=54v = 54 km/h =15= 15 m/s (part a)
  • ω,R\omega, R: Earth’s rotation
Find
(a) The lateral force on the rails; (b) the direction and speed that zeroes the inertial forces

Solution

Step 1Reference: the equation of motion in a rotating frame

In a reference frame rotating with constant angular velocity ω\vect\omega relative to an inertial frame, a particle of mass mm obeys

mw′=F+mω2ρ+2m (v′×ω)m\vect w' = \vect F + m\omega^{2}\vect\rho + 2m\,(\vect v'\times\vect\omega)
(1)

where w′\vect w' and v′\vect v' are the particle’s acceleration and velocity measured in the rotating frame, F\vect F is the resultant of the real (interaction) forces, and ρ\vect\rho is the position vector drawn perpendicularly from the rotation axis to the particle. The term mω2ρm\omega^{2}\vect\rho is the centrifugal force: it depends only on where the particle is and points away from the axis. The term 2m(v′×ω)2m(\vect v'\times\vect\omega) is the Coriolis force: it depends only on how the particle moves, is perpendicular to both v′\vect v' and ω\vect\omega, and has magnitude 2mv′ωsin⁡θ2mv'\omega\sin\theta, where θ\theta is the angle between v′\vect v' and ω\vect\omega. Both vanish in an inertial frame (ω=0\omega=0), and the Coriolis force does no work, since it is always perpendicular to v′\vect v'.

In this problem the rotating frame is the Earth, so ω\vect\omega is the Earth’s rotation along the polar axis; ρ\vect\rho is the perpendicular from that axis to the train, of magnitude Rcos⁡φR\cos\varphi and not along the local vertical; and v′\vect v', written simply v\vect v from here on since no other velocity appears, is the train’s velocity relative to the ground, horizontal. Both fictitious terms are wanted, and each is needed as a vector rather than a magnitude, so the work below resolves them in a local east-north-up frame. Part (a) asks only for the sideways (east-west) part of the Coriolis term, for which the surviving factor is the vertical component ωsin⁡φ\omega\sin\varphi crossed with a meridional v′\vect v'; part (b) asks for the velocity that makes the two fictitious terms of (1) cancel as vectors.

Step 2The local compass frame, and the Earth’s spin vector resolved in it

At latitude φ\varphi, set up local unit vectors east e\vect e, north n\vect n and up u\vect u (radially outward), a right-handed set with e×n=u\vect e\times\vect n=\vect u. The angle φ\varphi in the figure is exactly the tilt between this local frame and the equatorial one, so the Earth’s own spin vector, purely along the polar axis, splits into a horizontal (northward) and a vertical (upward) part.

ω=ωcos⁡φ n+ωsin⁡φ u\vect\omega = \omega\cos\varphi\,\vect n+\omega\sin\varphi\,\vect u
Step 3The Coriolis force on a horizontal velocity, in components

The Coriolis term of (1), written with the cross product the other way round, is FCor=−2mω×v\vect F_{Cor}=-2m\vect\omega\times\vect v. The right-handed frame’s three cyclic products give every cross product the expansion below needs.

e×n=u,n×u=e,u×e=n\vect e\times\vect n=\vect u, \qquad \vect n\times\vect u=\vect e, \qquad \vect u\times\vect e=\vect n
ω×v=ωcos⁡φ ve(n×e)+ωsin⁡φ ve(u×e)+ωsin⁡φ vn(u×n)=−ωcos⁡φ ve u+ωsin⁡φ ve n−ωsin⁡φ vn e.\begin{align*}\vect\omega\times\vect v &= \omega\cos\varphi\,v_e(\vect n\times\vect e)+\omega\sin\varphi\,v_e(\vect u\times\vect e)+\omega\sin\varphi\,v_n(\vect u\times\vect n) \\ &= -\omega\cos\varphi\,v_e\,\vect u+\omega\sin\varphi\,v_e\,\vect n-\omega\sin\varphi\,v_n\,\vect e.\end{align*}
FCor=2mωsin⁡φ vn e−2mωsin⁡φ ve n+2mωcos⁡φ ve u\begin{aligned}\vect F_{Cor} &= 2m\omega\sin\varphi\,v_n\,\vect e-2m\omega\sin\varphi\,v_e\,\vect n\\ &\quad+2m\omega\cos\varphi\,v_e\,\vect u\end{aligned}
(2)
Step 4Part (a): motion along the meridian

For a train on the meridian, ve=0v_e=0 and vn=±vv_n=\pm v. Equation (2) then leaves only the east component, evaluated with the Earth’s mean solar angular velocity ω=2π/86400 s≈7.27×10−5\omega=2\pi/86400\text{ s}\approx7.27\times10^{-5} rad/s (the sidereal value changes this by under half a percent, immaterial at this precision). Numerically,

F=2×2.0×106×15×7.27×10−5×sin⁡60∘ NF = 2\times2.0\times10^6\times15\times7.27\times10^{-5}\times\sin60^\circ\text{ N}
F=2mvωsin⁡φ≈3.8 kNF = 2mv\omega\sin\varphi \approx 3.8\text{ kN}
(3)

Whether vnv_n is positive (heading north) or negative (heading south), the deflection is to the right of the direction of travel: east of a train heading north is to its right, and west of a train heading south is to its right too, so the Earth’s reaction always presses the same rail. By Newton’s third law the train presses on that rail with the force above.

Step 5The centrifugal force, in the same local components
The same meridian section with the centrifugal force added: F_cf (gold) points away from the spin axis, perpendicular to it and not along the radius from O.

The same meridian section with the centrifugal force added: Fcf\vect F_{cf} (gold) points away from the spin axis, perpendicular to it and not along the radius from OO.

Writing X\vect X for the fixed global direction perpendicular to the spin axis (through the train’s own meridian), ρ=Rcos⁡φ X\vect\rho=R\cos\varphi\,\vect X and the centrifugal term of (1) is Fcf=mω2Rcos⁡φ X\vect F_{cf}=m\omega^2R\cos\varphi\,\vect X. The same rotation that resolved ω\vect\omega in Step 2 resolves X\vect X into the local frame, X=cos⁡φ u−sin⁡φ n\vect X=\cos\varphi\,\vect u-\sin\varphi\,\vect n.

Fcf=mω2Rcos⁡2φ u−mω2Rsin⁡φcos⁡φ n\vect F_{cf} = m\omega^2R\cos^2\varphi\,\vect u-m\omega^2R\sin\varphi\cos\varphi\,\vect n
(4)
Step 6Part (b): the velocity that cancels every inertial force

Adding (2) and (4) and setting each of the three components to zero,

east:2mωsin⁡φ vn=0north:−2mωsin⁡φ ve−mω2Rsin⁡φcos⁡φ=0up:2mωcos⁡φ ve+mω2Rcos⁡2φ=0\begin{aligned} \text{east:}&\quad 2m\omega\sin\varphi\,v_n = 0 \\ \text{north:}&\quad -2m\omega\sin\varphi\,v_e-m\omega^2R\sin\varphi\cos\varphi = 0 \\ \text{up:}&\quad 2m\omega\cos\varphi\,v_e+m\omega^2R\cos^2\varphi = 0 \end{aligned}

The east equation forces vn=0v_n=0 (a due east-west train), and the up equation then gives vev_e directly.

ve=−ωRcos⁡φ2v_e = -\frac{\omega R\cos\varphi}{2}

Substituting that value back into the north equation confirms it is satisfied automatically, so this single velocity kills all three components at once and not merely the vertical one that fixed it.

−2mωsin⁡φ(−ωRcos⁡φ2)−mω2Rsin⁡φcos⁡φ=mω2Rsin⁡φcos⁡φ−mω2Rsin⁡φcos⁡φ=0(5)-2m\omega\sin\varphi\left(-\frac{\omega R\cos\varphi}{2}\right)-m\omega^2R\sin\varphi\cos\varphi = m\omega^2R\sin\varphi\cos\varphi-m\omega^2R\sin\varphi\cos\varphi = 0 \tag{5}

The negative sign means westward; evaluating the constants fixes the numerical value.

ωRcos⁡φ=7.27×10−5×6.37×106×cos⁡60∘ m/s≈2.32×102 m/sv=2.32×1022 m/s\begin{align*}\omega R\cos\varphi &= 7.27\times10^{-5}\times6.37\times10^6\times\cos60^\circ\text{ m/s} \approx 2.32\times10^2\text{ m/s}\\ v &= \dfrac{2.32\times10^2}{2}\text{ m/s}\end{align*}
v=ωRcos⁡φ2≈116 m/s≈4.2×102 km/hv = \dfrac{\omega R\cos\varphi}{2} \approx 116\text{ m/s} \approx 4.2\times10^2\text{ km/h}
(6)

The train must head due west, at half the ground’s own rotation speed at that latitude.

Check

Part (a)’s force is linear in vv and vanishes at the equator (sin⁡φ=0\sin\varphi=0), growing to its largest value at the poles, a textbook feature of the Coriolis effect. Equation (5) confirms that part (b)’s single velocity cancels both horizontal components at once, not only the vertical one that fixed its value.

Remark

Part (b)’s train travels westward, against the Earth’s own eastward spin, but not fast enough to stand still in the truly inertial frame: its ground speed relative to the stars is ωRcos⁡φ−ωRcos⁡φ/2=ωRcos⁡φ/2\omega R\cos\varphi-\omega R\cos\varphi/2=\omega R\cos\varphi/2 eastward, not zero, so this is not simply “cancel the Earth’s rotation.” What it does cancel is the Earth’s surface velocity at half strength: that factor of 1/21/2 is the Coriolis term’s own factor of 22 set against the single power of ω\omega carried by the centrifugal term, not an accident of the particular numbers here.