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Physics · Ch 5 — Gravitation

(C) Variation in g with Latitude and Rotation of the Earth

5.6.3

(C) Variation in g with Latitude and Rotation of the Earth

So far g has been treated as though the Earth were a perfect, non-rotating sphere. In reality the Earth rotates about its polar axis (west to east) with angular velocity ω\omega, and every point on its surface except the two poles themselves is carried along a circular path (parallel to the equator) by this rotation, which requires a centripetal force -- and that force is SUPPLIED by part of the gravitational attraction, reducing the portion of gravity actually felt as weight.

Latitude θ\theta is defined as the angle between the radius vector to a surface point P and the equatorial plane, ranging from 0∘0^\circ at the equator to 90∘90^\circ at the poles. As the Earth spins, point P traces a horizontal circle of radius r=Rcos⁡θr=R\cos\theta about a centre O′O' on the polar axis (Fig. 5.9), with centripetal acceleration a=rω2=Rω2cos⁡θa=r\omega^2=R\omega^2\cos\theta directed along PO′PO'. Only the COMPONENT of this centripetal acceleration directed along PO (i.e. towards the Earth's true centre) actually subtracts from gravity; resolving along PO gives ar=acos⁡θ=Rω2cos⁡2θa_r=a\cos\theta=R\omega^2\cos^2\theta. The effective (measured) acceleration due to gravity at latitude θ\theta is therefore g′=g−Rω2cos⁡2θ.g'=g-R\omega^2\cos^2\theta.

At the EQUATOR (θ=0∘\theta=0^\circ, cos⁡θ=1\cos\theta=1), the reduction is maximum: g′=g−Rω2g'=g-R\omega^2. Using R=6.4×106R=6.4\times10^6 m and ω=2π/T\omega=2\pi/T with T=24T=24 hours (the Earth's rotation period), Rω2≈0.0339R\omega^2\approx0.0339 m/s^2 -- a small but measurable reduction. At the POLES (θ=90∘\theta=90^\circ, cos⁡θ=0\cos\theta=0), there is NO reduction at all (g′=gg'=g), because points exactly on the rotation axis do not move in a circle and feel no centripetal effect whatsoever. Between these extremes, g′g' increases smoothly and monotonically from equator to pole, exactly as tabulated in Table 5.2. …

Figure 5.9Fig. 5.9: Variation of g with latitude

What this figure shows. A circle representing the Earth with its centre O and its polar axis drawn vertically. A point P on the Earth's surface at latitude θ\theta is marked, together with a point E on the equator. The line OP (from the centre to P) makes angle θ\theta with the equatorial plane OE. As the Earth rotates, point P traces a horizontal circle of radius r (smaller than R, except at the equator) about a centre O′O' on the polar axis directly 'below'/'above' P; the segment PO′=r=Rcos⁡θPO'=r=R\cos\theta is drawn, along with the right-angled triangle OPO′OPO' used to derive this relation. The centripetal acceleration a=rω2a=r\omega^2 at P is directed along PO′PO', and its component along PO (i.e. towards the Earth's centre) is what reduces th …

Table T5.2Table 5.2: Variation of acceleration due to gravity g with latitude, measured at sea level, showing g rising steadily from a minimum at the equator to a maximum at the poles

Latitude (deg) | g (m/s^2)

0 | 9.7804

10 | 9.7819

20 | 9.7864

30 | 9.7933

40 | 9.8017

50 | 9.8107

60 | 9.8192

70 | 9.8261 …