JEE Main Seat Allotment 2024 - Dates, How to Check

# Acceleration Due To Gravity - Practice Questions & MCQ

Edited By admin | Updated on Sep 18, 2023 18:34 AM | #JEE Main

## Quick Facts

• Variation in 'g' due to height, Variation in 'g' due to Rotation of earth are considered the most difficult concepts.

• Acceleration due to gravity (g) are considered the most asked concepts.

• 75 Questions around this concept.

## Solve by difficulty

The mass of a spaceship is 1000 kg. It is to be launched from the earth's surface out into free space. The values of 'g' and 'R' (radius of the earth) are 10 m/s2 and 6400 km respectively. The required energy for this work will be 6.4 x 10n joules. Then the value of 'n' is :

The spring balance is graduated at sea level. If the body is weighed by this spring scale at gradually increasing heights from the earth's surface, then the weight indicated by the spring scale

Which of the following statements about gravitational acceleration is true?

Which of the following factors affects the value of 'g'?

The variation of acceleration due to gravity g with distance d from centre of the earth is best represented by

Apply to Amity University, Noida B.Tech Admissions 2024

How does the value of 'g' change with increase in altitude?

The height at which the acceleration due to gravity becomes $\dpi{100} g/9$ ( where $g$ = the acceleration due to gravity on the surface of the earth ) in terms of $R$( the radius of the earth) is

##### Amity University, Noida B.Tech Admissions 2024

Asia's Only University with the Highest US & UK Accreditation

Ranked #52 among universities in India by NIRF | Highest CTC 50 LPA | 100% Placements | Last Date to Apply: 27th June

How does the value of 'g' change with increasing depth below the Earth's surface?

How does the value of 'g' change at the equator due to the Earth's rotation?

JEE Main College Predictor
Predict your top engineering college admission chances based on your JEE Main All India Rank & NTA Score.

## Concepts Covered - 5

Acceleration due to gravity (g)

The Gravitational Force exerted by the earth on a body is known as the gravitational pull of gravity. And this force will produce an acceleration in the motion of a body.

And this is known as the acceleration due to gravity.

This is denoted by g.

Let gravitational force exerted by the earth on the body of mass m resting on the surface of the earth is given by

$F=\frac{GMm}{R^2}$ …(1)

Where M = mass of the earth and R = radius of the earth

And If g is the acceleration due to gravity then this F can be written as

F=(mass)*(acceleration)=mg ...(2)

On Comparing

We get

$g=\frac{GM}{R^{2}}$

Now $\rho \rightarrow$ density of earth

Then $M=\rho *(\frac{4}{3})\pi R^3$

So $g=\frac{4}{3}\pi \rho \, GR$

• Its average value is $9.8\: m/s^{2}\; \; or \; \; 981cm/sec^{2}\; or\; 32feet/s^{2}$on the surface of earth.

•  It is a vector quantity and its direction is always towards the center of the earth/Planet.

• Dimension- $LT^{-2}$

•  Its value depends upon the mass, radius, and density of the Earth/Planet.

Means Planet having more value of $\rho R$ than earth will have a greater value of acceleration due to gravity (g)  than the earth

I.e $\\ If \ (\rho R)_P > (\rho R)_E \\ \Rightarrow g_P> g_E$

•  It is independent of mass, shape and density of the body situated on the surface of the Earth/planet.

Value of g will be the same for a  light as well as heavy body if both are situated on the surface of the Earth/planet.

Variation in the value of g due to shape of Earth
• The value of acceleration due to gravity (g) changes its value due to the following factors

1. The shape of the earth

2. Height above the earth's surface

3. Depth below the earth's surface

4.  Axial rotation of the earth.

• Variation of 'g' due to the shape of the earth

Earth has an elliptical shape as shown in fig.

Or $R_e>R_p$

Where $R_{e}\rightarrow$ Radius of the equator

$R_{p}\rightarrow$ Radius of pole

So $g_p > g_e$

In fact $g_{p}=g_{e}+0.018m/s^{2}$

Or we can say Weight increases as the body is taken from equator to pole.

Variation in 'g' due to height

Let's study Variation in 'g' with height

Value of g at the surface of the earth (at distance r=R from earth center)

$g=\frac{GM}{R^2}$

Value of g at height h from the surface of the earth (at a general distance r=R+h from earth center)

$g'\alpha\, \frac{1}{r^{2}}$

Where $r=R+h$

As we go above the surface of the earth, the value of g decreases

So $g'=\frac{GM}{r^2}$

Where $g'\rightarrow$ gravity at a height h from the surface of the earth.

$R\rightarrow$ The radius of earth

$h\rightarrow$ height above the surface

• Value of 'g' at ∞

if   $r=\infty \: \; \; \; \; \; \; g'=0$

No effect of earth gravitational pull at infinite distance.

• Value of g when h < < R

• Formula

1. Value of g

$g'=g(\frac{ R}{R+h})^2=g(1+\frac{h}{R})^{-2}$

So $g'=g\left [ 1-\frac{2h}{R} \right ]$

1.  The absolute decrease in the value of g with height

$\Delta g=g-g'=\frac{2hg}{R}$

1. The fractional decrease in the value of g with height

$\frac{\Delta g}{g}=\frac{g-g'}{g}=\frac{2h}{R}$

1. Percentage decrease in the value of g with height

$\frac{\Delta g}{g}\times 100 \; ^{0}\!\! /\! _{0}=\frac{2h}{R}\times 100 \; ^{0}\!\! /\! _{0}$

Variation in 'g' due to depth

Let's study Variation in 'g' with depth

Value of g at the surface of the earth (at d=0)

$g=\frac{GM}{R^2}=\frac{4}{3}\pi \rho gR$

Value of g at depth d from the surface of the earth (at a general distance r=(R-d) from earth centre)=g'

And $g'\propto (R-d)$

Means Value of g' decreases on going below the surface of the earth.

So $g'=g\left [ 1-\frac{d}{R} \right ]$

• Value of 'g' at the centre of the earth

At the centre

$\text{depth from surface} (d) =R$

So $g'=0$

i.e., Acceleration due to gravity at the centre of the earth becomes zero.

• The absolute decrease in the value of g with depth

$\Delta g=g-g'=\frac{dg}{R}$

• The fractional decrease in the value of g with depth

$\frac{\Delta g}{g}=\frac{g-g'}{g}=\frac{d}{R}$

The value of g decreases with depth.

• Percentage decrease in the value of g with depth

$\frac{\Delta g}{g}\times 100 \ \%=\frac{d}{R}\times 100 \ \%$

Note- Rate of decrease of gravity outside the earth (h<<R) is double that of inside the earth

Variation in 'g' due to Rotation of earth

Let's study Variation in 'g' due to Rotation of earth

As the earth rotates about its axis

Let its angular velocity is $\omega$ about an axis as shown in the figure.

So if a body placed on its surface then it will move along the circular path.

So the apparent weight of the body will decrease as it will experience a centrifugal force due to rotation.

We can calculate this apparent weight of the body using force balance.

Let calculate its value for a body of mass m situated at a point P (having latitude=$\lambda$)

As shown in the figure.

• $\lambda$=The angle between the equatorial plane at that point and line joining that point to the centre of the earth.

• For the poles $\lambda$=90 and for equator $\lambda$=0

$r=RCos \lambda$

$F_c=m\omega ^2r=m\omega ^2Rcos\lambda$

From applying newton's 2nd law along the line joining point P and center.

$mg-F_cCos\lambda =mg'$

Where g' is the value of acceleration due to gravity at point P.

So we get $g'=g-\omega ^{2}R\cos ^{2}\lambda$

• Apparent weight of body decrease with an increase in angular velocity  ($\omega$)

•  Apparent weight of the body varies from point to point because each point has different latitude and magnitude of centrifugal force varies with the latitude of the place.

• For Pole, $\lambda$=90

So $g_{pole}=g$

I.e value of g at the poles is independent of angular velocity of earth.

• For equator,$\lambda$=0

$g_{equator}=g-\omega ^2R$

I.e Decrease in the value of g is maximum at the equator

• Weightlessness due to rotation of the earth-

Weightlessness means g'=0

So $g'=g-\omega ^{2}R\cos ^{2}\lambda$

As $\lambda=0$  (For equator)

$O=g-\omega ^{2}R\cos ^{2}0$

$g-\omega ^{2}R=0$

$\omega =\sqrt{\frac{g}{R}}$

Where $\omega \rightarrow$ Angular velocity for which a body at the equator will become weightless

• The time period of Rotation of earth for which body at the equator will become weightless

$T=\frac{2\pi }{\omega }=2\pi \sqrt{\frac{R}{g}}$

Where $R\rightarrow$ Radius of earth

And using $R=6400\times 10^{3}m$

$g=10\: m/s^{2}$

We get $\omega =\frac{1}{800}\frac{rad}{sec}$

And $T=1.40\; hr$

• Relation of gravity at the poles and equator

After considering the effect of rotation, and elliptical shape of the earth

$g_{p}=g_{e}+0.052\; m/s^{2}$

Where $g_{p}\rightarrow$ gravity at the pole

$g_{e}\rightarrow$ gravity at equator

## Study it with Videos

Acceleration due to gravity (g)
Variation in the value of g due to shape of Earth
Variation in 'g' due to height

"Stay in the loop. Receive exam news, study resources, and expert advice!"