Acceleration Due to Gravity (g) and its Variations
The acceleration experienced by a freely falling body under the gravitational pull of the Earth is called the acceleration due to gravity, denoted by g. On the surface of the Earth, standard g is approximately 9.8 m/s2. However, g is not a universal constant; it varies systematically with altitude, depth, latitude, and Earth's geometric shape.
1. Relation Between g and Universal Constant G
Consider a body of mass m placed on the surface of the Earth of mass M and radius R. By Newton's law of gravitation, the force acting on the body is:
F = G M m / R2
From Newton's second law of motion, F = m g. Equating the two expressions gives the fundamental relation:
In terms of average density ρ of the Earth (assuming a uniform sphere of volume V = 4/3 π R3):
g = G [4/3 π R3 ρ] / R2 = 4/3 π G ρ R
Anatomy of Variations in Acceleration Due to Gravity
ALTITUDE (HEIGHT h): DEPTH (DEPTH d):
------------------- ----------------
gh = g [R / (R + h)]² gd = g [1 - (d / R)]
If h << R: Linear decrease with depth:
gh ≈ g [1 - (2h / R)] At center of Earth (d = R):
Percentage decrease: (2h / R) * 100% gd = 0 (weightlessness at center)
ROTATION OF EARTH (LATITUDE λ): SHAPE OF EARTH (OBLATE SPHEROID):
------------------------------- ---------------------------------
g' = g - ω² R cos² λ Re > Rp (Equator bulges by ~21 km)
At Equator (λ = 0°): g = GM / R²
geq = g - ω² R (Minimum g) gp > geq
At Poles (λ = 90°): g is MAXIMUM at poles,
gp = g (Maximum g) MINIMUM at equator
2. Analytical Derivations of Variations in g
1. Variation with Altitude (Height h Above Surface)
At a height h above the Earth's surface, the distance from the center is r = R + h:
gh = G M / (R + h)2 = [G M / R2] [1 + h/R]−2 = g (1 + h/R)−2
Using binomial expansion for h ≪ R:
2. Variation with Depth (Depth d Below Surface)
At a depth d below the surface, the distance from the center is r = R − d. By the shell theorem, the outer spherical shell of thickness d exerts zero net force. Only the inner sphere of radius (R − d) contributes:
M' = ρ [4/3 π (R − d)3] = M (R − d)3 / R3
gd = G M' / (R − d)2 = G M (R − d) / R3 = g (1 − d/R)
Note: Unlike the height formula, the depth formula gd = g(1 − d/R) is exact for all depths from surface to center (assuming uniform density). At the center of the Earth (d = R), g = 0.
3. Variation with Latitude (Earth's Rotation)
As the Earth rotates with angular speed ω about its polar axis, a body at latitude λ revolves in a circle of radius r = R cos λ. The centrifugal acceleration acts radially outwards from the axis of rotation:
g' = g − ω2 R cos2 λ
- At the Equator (λ = 0°): cos 0° = 1 ⇒ geq = g − ω2 R (minimum effective gravity).
- At the Poles (λ = 90°): cos 90° = 0 ⇒ gp = g (rotation has zero effect).
3. Comparative Summary of Gravity Variations
| Factor | Mathematical Formula | Nature of Graph | Extreme Values |
|---|---|---|---|
| Altitude (h) | gh = g / (1 + h/R)2 | Inverse-square decay (1/r2) | g → 0 as h → ∞ |
| Depth (d) | gd = g (1 − d/R) | Linear decline (straight line) | g = 0 at center of Earth |
| Latitude (λ) | g' = g − ω2 R cos2 λ | Trigonometric (cos2 λ) | Max at poles; min at equator |
| Shape (Oblateness) | Re − Rp ≈ 21 km | Inverse-square on radius | gp − ge ≈ 0.02 m/s2 |
Weightlessness at equator means geq = 0 ⇒ g − ω2 R = 0 ⇒ ω = √(g / R). Plugging numbers: ω ≈ 1.24 × 10−3 rad/s, which is approximately 17 times the present rotation speed (Earth's day would become 1.4 hours)!
4. Solved High-Yield JEE / NEET Practice Questions
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1. Use the exact altitude formula (since 1/4th is a large change, approximation 1 − 2h/R cannot be used!):
gh = g / (1 + h/R)2.
2. Given gh = g / 4:
g / 4 = g / (1 + h/R)2 ⇒ (1 + h/R)2 = 4.
3. Taking the positive square root:
1 + h/R = 2 ⇒ h/R = 1 ⇒ h = R.
At height equal to Earth's radius (6,400 km), gravity drops to 25% of its surface value.
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1. Change in g at height h: Δgh = g − gh = g − g(1 − 2h/R) = 2g h / R.
2. Change in g at depth d: Δgd = g − gd = g − g(1 − d/R) = g d / R.
3. Equating both changes: 2g h / R = g d / R ⇒ d = 2h.
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1. When rotating, geq = g − ω2 R.
2. If Earth stops rotating (ω = 0), the centrifugal reduction vanishes, so g'eq = g.
3. Hence, the acceleration due to gravity at the equator will increase by ω² R. At the poles, it remains completely unchanged.
5. Frequently Asked Questions (FAQs)
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