Uploaded by Manoram Subedi

Gravitation

advertisement
Gravitation
Gravitational force
οƒ˜ The force of attraction between any two bodies in the universe is called gravitational force.
οƒ˜ The magnitude of gravitational force is calculated as, F =
πΊπ‘š1 π‘š2
𝑑2
οƒ˜ Example: the force between earth and moon, the force between 1 kg mass in Nepal and 1 kg
mass in India.
οƒ˜ It is always attractive force.
οƒ˜ It doesnot depend upon medium between two bodies.
οƒ˜ The existence of universe is due to gravitational force.
Gravity
οƒ˜ The force with which earth or any other planet attracts an object towards their centre is called
gravity.
οƒ˜ The magnitude of gravity is calculated as, F =
πΊπ‘€π‘š
𝑅2
οƒ˜ Example: A stone is attracted towards the centre of earth.
οƒ˜ It is always attractive force.
οƒ˜ The existence of atmosphere on the surface of earth is due to the gravity.
NewtoN’s law of gravitatioN
It states, “the force of attraction between any two bodies in the universe is directly proportional
to the product of their masses and inversely proportional to the square of distance between their
centres.”
Let us consider two bodies having masses m1 and m2 separated by the distance r as shown in figure.
According to the Newton’s law of gravitation, the force of attraction between them is directly
proportional to the product of their masses and inversely proportional to the square of distance
between their centres.
i.e. F α m1m2 …………….. (i)
1
and, F α π‘Ÿ2 ………………… (ii)
Combining equations (i) and (ii), we get,
Fα
π‘š1 π‘š2
π‘Ÿ2
Or, F =
πΊπ‘š1 π‘š2
𝑑2
Where, G is proportionality constant called universal gravitational constant. Its value is 6.67 x
10-11Nm2/kg2.
Inertial mass and gravitational mass
Inertial mass
1. The mass of a body when it is in
motion is called inertial mass.
2. It is calculated when the body has
some has acceleration.
3. It is calculated by, F = ma
Gravitational mass
1. The mass of a body when it is at rest
is called gravitational mass.
2. It is calculated when the body is at
rest.
πΊπ‘€π‘š
3. It is calculated by, F = 2
𝑅
Mass and Weight
Mass
1. The amount of matter contained in a
body is called mass
2. It is always constant.
3. It is a scalar quantity.
4. Its value cannot be zero.
Weight
1. The force with which earth or any
other planets attract an object
towards their centre is called weight.
2. It varies from place to place.
3. It is a vector quantity.
4. Its value can be zero.
Gravitational field intensity
οƒ˜ The gravitational field intensity at a point in the gravitational field is defined as the force
experienced by unit mass at that point.
𝐹
οƒ˜ It is calculated as, E = π‘š =
πΊπ‘€π‘š
π‘šπ‘… 2
=
𝐺𝑀
𝑅2
οƒ˜ Its unit is N/kg
οƒ˜ It is numerically equal to the acceleration due to gravity.
Acceleration due to gravity
οƒ˜ The acceleration produced on a freely falling body due to gravity is called acceleration
due to gravity.
οƒ˜ Its value changes from place to place. For the earth, acceleration due to gravity is
maximum at pole.
οƒ˜ Its value is calculated as, g =
οƒ˜ It is a vector quantity.
𝐺𝑀
𝑅2
Variation of acceleration due to gravity
(A) Variation of acceleration due to gravity due to height
The acceleration due gravity at the surface of earth is given by,
g=
𝐺𝑀
𝑅2
…………………. (i)
The value of acceleration due to gravity at the height ‘h’ from the surface of earth is,
𝐺𝑀
g’ = (𝑅+β„Ž)2 ……………. (ii)
Dividing equation (ii) by (i), we get,
𝑔′
𝑔
=
𝐺𝑀
(𝑅+β„Ž)2
X
𝑅2
𝐺𝑀
𝑅2
= (𝑅+β„Ž)2
=(
𝑅+ β„Ž −2
𝑅
)
β„Ž −2
= (1 + 𝑅)
Expanding RHS using Binomial expansion, we get,
𝑔′
=1-
𝑔
2β„Ž
𝑅
+ higher power terms of h/R
The value of h/R is very small and its higher power terms can be neglected.
So,
𝑔′
=1-
𝑔
2β„Ž
𝑅
2β„Ž
g’ = g(1 -
𝑅
)
This relation shows that the acceleration due to gravity decreases with increase in height from
the earth surface.
(B) Variation of acceleration due to gravity due to depth
The acceleration due to gravity at the surface of earth is,
𝐺𝑀
g= 2
=
𝑅
𝐺 x 𝑉 x𝜌
=
𝑅2
4
𝐺 x πœ‹π‘… 3 x𝜌
3
𝑅2
4
Or, g = 3πRρG …………. (i)
Similarly, the acceleration due to gravity at a depth x from the surface of earth is,
4
g’ = 3π(R – x)ρG ……………. (ii)
Dividing equation (ii) by equation (i). we get
𝑔′
𝑔
4
=3
=
π(R−x)ρG
4
πRρG
3
𝑅−π‘₯
𝑅
π‘₯
g’ = g (1 - 𝑅)
This relation shows that the acceleration due to gravity decreases with increase in depth from
the earth’s surface.
Q. If a man can lift 60 kg mass on the surface of earth, the mass he can lift on the surface of
moon is ……360kg(For a person, mege = mmgm or, 60 x 6gm = mm gm
or, mm = 360Kg)
Q. If a man can lift 60 N load on the surface of earth, the load he can lift on the surface of moon
is…….60N (For a person, mege = mmgm = 60N )
Q. If the mass of man is 60 kg on the surface of earth, his mass on the surface of moon
is………60Kg
Q. If the weight of a man is 60N on the surface of earth, his weight on the surface of moon
is………….10N ( m = 6 kg, for moon, w = mxgm = 6 x ge/6 = 10N)
Q. If a man can lift 60 N load on the surface of earth, the mass he can lift on the surface of
moon is………36kg
Q. If the potential energy of a man is 60J on the surface of earth, his potential energy on the
surface of moon is…….60J
Q. If a man can jump 1m on the surface of earth, the height he can jump on the surface of
moon is………..6m
Gravitational potential
The amount of work done in bringing a body of unit mass from infinity to a point in the
gravitational field of earth is called gravitational potential.
The gravitational force between the earth and the body of unit mass at point P at a distance x
from the earth is,
F=
πΊπ‘€π‘š
π‘₯2
or, F =
𝐺𝑀
π‘₯2
The small amount of work done in bringing a body from point P to Q through small distance dx
is,
dw = Fdx =
𝐺𝑀
π‘₯2
dx
The total work done in bringing the body from infinity to the point A is,
π‘Ÿ
w = ∫∞ 𝑑𝑀
π‘Ÿ 𝐺𝑀
= ∫∞
=
=
=
dx
π‘₯2
π‘Ÿ
GM∫∞ π‘₯ −2 𝑑π‘₯
π‘₯ −2+1 π‘Ÿ
]
GM [
−2+1 ∞
1 π‘Ÿ
- GM[π‘₯ ] ∞
1
1
= - GM [π‘Ÿ − ∞]
=
−𝐺𝑀
π‘Ÿ
This work done is equal to the gravitational potential at point A.
So, Gravitational potential, V =
−𝐺𝑀
π‘Ÿ
(∫ π‘₯ 𝑛 𝑑π‘₯ = [
π‘₯ 𝑛+1
𝑛+1
])
Gravitational potential energy
The amount of work done in bringing a body of unit mass from infinity to a point in the
gravitational field of earth is called gravitational potential.
The gravitational force between the earth and the body of unit mass at point P at a distance x
from the earth is,
F=
πΊπ‘€π‘š
π‘₯2
or, F =
𝐺𝑀
π‘₯2
The small amount of work done in bringing a body from point P to Q through small distance dx
is,
dw = Fdx =
𝐺𝑀
π‘₯2
dx
The total work done in bringing the body from infinity to the point A is,
π‘Ÿ
w = ∫∞ 𝑑𝑀
π‘Ÿ πΊπ‘€π‘š
= ∫∞
=
=
=
π‘₯2
dx
π‘Ÿ
GMm∫∞ π‘₯ −2 𝑑π‘₯
π‘₯ −2+1 π‘Ÿ
]
GMm [
−2+1 ∞
1 π‘Ÿ
- GMm[π‘₯ ] ∞
1
1
= - GMm [π‘Ÿ − ∞]
(∫ π‘₯ 𝑛 𝑑π‘₯ = [
π‘₯ 𝑛+1
𝑛+1
])
w
=
−πΊπ‘€π‘š
π‘Ÿ
This work done is equal to the gravitational potential energy at point A.
So, Gravitational potential energy, U =
−πΊπ‘€π‘š
π‘Ÿ
Escape velocity
Escape velocity is the minimum velocity required by a body to be projected to overcome the
gravitational pull of the earth.
The gravitational force between the earth and the body of at point P at a distance x from the
earth is,
F=
πΊπ‘€π‘š
π‘₯2
The small amount of work done in moving a body from point P to Q through small distance dx is,
dw = Fdx =
πΊπ‘€π‘š
π‘₯2
dx
The total work done in moving the body from surface of earth (point A) to the infinity is,
∞
w = ∫𝑅 𝑑𝑀
∞ πΊπ‘€π‘š
= ∫𝑅
=
= GMm
π‘₯ −2+1 ∞
[
]
−2+1 𝑅
π‘₯2
dx
∞
GMm∫𝑅 π‘₯ −2 𝑑π‘₯
π‘₯ 𝑛+1
(∫ π‘₯ 𝑛 𝑑π‘₯ = [ 𝑛+1 ])
1
= - GMm[ ] ∞
𝑅
π‘₯
1
1
= - GMm [∞ − 𝑅]
w
=
πΊπ‘€π‘š
𝑅
This work done is equal to the kinetic energy of a moving body.
i.e.
K.E. = w
or,
or,
or,
Since, g =
1
2
π‘šπ‘£π‘’2 =
𝑣𝑒2 =
πΊπ‘€π‘š
2𝐺𝑀
ve = √
𝑅
(ve is escape velocity of earth)
𝑅
2𝐺𝑀
𝑅
…………………… (i)
𝐺𝑀
𝑅2
ve = √
2𝑔𝑅 2
𝑅
So,
ve = √2𝑔𝑅
This is an expression for escape velocity.
For earth,
g = 9.8ms-2
R = 6400000m
Then, ve = √2𝑔𝑅 = √2 x 9.8x 6400000
= 11.2km/s
Satellite
οƒ˜ A satellite is a body that orbits around another body in space.
οƒ˜ Satellites can be natural or artificial.
οƒ˜ The gravitational pull provides necessary centripetal force for the satellite.
οƒ˜ satellites donot require any types of fuel to move in a circular path.
Geostationary satellite
οƒ˜ A satellite which appears stationary above the surface of earth is called geostationary
satellite.
οƒ˜ The time period of geostationary satellite is 24 hrs.
οƒ˜ The height of geostationary satellite is 36000 km from the surface of earth.
οƒ˜ The radius of orbit of geostationary satellite is 42400 km.
Orbital velocity
The velocity which causes the satellite to revolve around the earth (planet) is called orbital
velocity.
Consider a satellite of mass m revolving around the earth at a height h from the surface of earth.
The radius of orbit of satellite is (R+h).
The gravitational pull of earth provides necessary centripetal force for the satellite.
i.e.
π‘šπ‘£ 2
πΊπ‘€π‘š
(𝑅+β„Ž)2
= 𝑅+β„Žπ‘œ
𝐺𝑀
or,
vo2 =
or,
v0 = √𝑅+β„Ž
𝑅+β„Ž
𝐺𝑀
This is an expression of orbital velocity.
If the satellite is close to the surface of earth then, R+h ≈ R
So,
v0 = √
𝐺𝑀
𝑅
v0 = √
𝑔𝑅 2
(g =
𝑅
𝐺𝑀
𝑅2
)
Hence, v0 = √𝑔𝑅
For earth,
g = 9.8ms-2 and R = 6400000m
So, v0 = √9.8 x 6400000
≈ 7.91 km/s
Time period of satellite
The time period of satellite is given by,
Time period, T =
2πœ‹
πœ”
=
=
2πœ‹π‘Ÿ
π‘£π‘œ
2πœ‹(𝑅+β„Ž)
√
(v = ωr)
𝐺𝑀
𝑅+β„Ž
= 2π√
(𝑅+β„Ž)3
𝐺𝑀
Energy of satellite
The satellite moving around the earth possess both potential energy and kinetic energy. So, the
total energy of satellite is equal to the sum of potential energy and kinetic energy.
The potential energy of satellite is given by,
−πΊπ‘€π‘š
P.E. =
𝑅+β„Ž
………………. (i)
The kinetic energy of satellite is given by,
1
K.E. = 2 π‘šπ‘£π‘œ2
2
1
𝐺𝑀
= 2 π‘š (√𝑅+β„Ž )
K.E. =
πΊπ‘€π‘š
2(𝑅+β„Ž)
……………. (ii)
Now, the total energy of satellite is,
E = P.E. + K.E.
=
−πΊπ‘€π‘š
𝑅+β„Ž
− πΊπ‘€π‘š
πΊπ‘€π‘š
+ 2(𝑅+β„Ž)
E = 2(𝑅+β„Ž)
This gives the total energy of satellite.
Download