Date post: | 21-Dec-2015 |
Category: |
Documents |
View: | 220 times |
Download: | 3 times |
Chapter 12 Gravitation
C .
apple
mg
earth
m1 m2
F12 F21
r
In chapter 2 we saw that close to the surface of the earth the gravitational force Fg is: a. Constant in magnitude Fg = mg and b. Is directed towards the center of the earth
In this chapter we will give the general form of the gravitational force between two masses m1 and m2 . This force explains in detail the motion of the planets around the sun and of all celestial bodies. This is a law truly at a cosmic level (12-1)
Final Exam:
Friday 5/2/03 8:00-11:00 am Rm. 215 NSC
3 long problems from chapters 9,10,11,12, and 13
6 mini problems from chapters 1-13
Bring with you:
2 pens
1 page with equations (both sides)
Your ID
Celestial objects are divided into two categories:
1. Stars They have fixed positions with respect to each other That is the reason why we can group hem into constellations that maintain the same shape
2. Planets They follow complicated paths among the stars
An example is given in the picture.
Note: All stars rotate around the star polaris every 24 hours
(12-2)
Polaris
Celestial sphere
Rotation Axis of the Celestial sphere
earth
N
S
Star
Geocentric System
1. The earth is at the center of the universe
2. The stars are fixed on a sphere (known as the “celestial sphere”) which rotates about its axis every 24 hours. The axis connects the center of the earth with the star polaris. All stars move on circular paths on the celestial sphere and complete a rotation every 24 hours
(12-3)
Ptolemaic System
Ptolemy in the 2nd century AD used the following geocentric model to describe the complicated motions of the planets. The planets and the sun move on small circular paths called the epicycles. The centers of the epicycles move around the earth on larger circles called deferents
Ptolemy’s system gives a reasonable description of the motion of the planets and it was accepted for 1400 years
(12-4)
The Heliocentric SystemIn 1543 Copernicus introduced the heliocentric system. According to this scheme the sun is at the center of the solar system. The planets and the earth rotate about the sun on circular orbits. The immobility of the stars was ascribed to their great distance. The heliocentric system was not accepted for almost a century
(12-5)
Nicolaus Copernicus
(1473-1543)
He discussed his ideas in the book: De Revolutionibus Orbitum Coelestium published after his death
Thycho Brache in Denmark constructed sophisticated astronomical instruments and studied in detail the motion of the planets with a accuracy of ½ minute (1 minute = 1/60 degree)
Brache died in 1601 before he had a chance to analyze his data. This task was carried out by his assistant Johannes Kepler for the next 20 years. His conclusions are summarized in the form of three laws that bear his name (Kepler’s laws)
(12-6)
Kepler’s first law
Planets move on elliptical paths (orbits) with the sun at one focus
(12-7)
Kepler’s second law
During equal time intervals the vector r that points from the sun to a planet sweeps equal areas
t
t
A
A
constantA
t
Sun
P1
P2
R1
R2
Kepler’s third law
If T is the time that it takes for a planet to complete one revolution around the Sun and R is half the major axis of the ellipse then:
C is constant for all planets of the solar system
If the planet moves on a circular path then R is simply the orbit radius. For the two planets in the figure Kepler’s third law can be written as:
(12-8)
2
3
TC
R
2 21 2
3 31 2
T T
R R
Isaac Newton: Newton had formulated his three laws of mechanics. It was natural to check and see if they apply beyond the earth and be able to explain the motion of the planets around the sun. Newton after studying Kepler’s laws came to the following conclusions:
1. Kepler’s second law implies that the attractive force F exerted by the sun on the planets is a central force
2. If he assumed that the magnitude of the attractive force F has the form:
(k is a constant) and applied Newton’s second law and calculus (which he had also discovered) he got orbits that are conic sections
3. A force gave Kepler’s third law:
(12-9)
2
3
TC
R
2
kF
r
2
kF
r
Conic Section is one of the four possible curves (circle, ellipse, parabola, hyperbola) we get when we cut the surface of a cone with a plane, as shown in the figure below
(12-10)
Kepler’s third law for circular orbits
Sun
P
R
m
v
FM
(12-11)
2 2 22 2
2 2
2 32
2 2
3
2 4 Period
4Substitute v from eqs.3 into the last equation:
4 constant C Note: We know that C
does not depend on m.
(eqs.3)
The answe
mv k k R Rv T T
R mR vR v
R mT
k
T m
kR
r lies in the constant k
2
2 ,
Elimina
(eqs.1)
te F fro
(eqs.2
m eqs.1 and eqs
)
.2
k mvF F
RR
m1 m2
F12 F21
r
Newton’s Law of Gravitational Attraction
(12-12)
1 2
12 21
Two masses m and m placed at a distance r exert an
attractive force on each other. This force is known as the
" " and has the following characteristics:
1. F
gravitational for
and F
e
ac
c
1 2
1 212 21 2
1 22
t along the line that connects m and m
2. G is the gravitational constant
Previously we wrote Thus
Gm mF F
rk
F k Gm mr
1 212 21 2
Gm mF F
r
Revisit Kepler’s third law
Sun
P
R
m
v
FM
(12-13)
2 2
2 2
3
(eqs.1) (eqs.2)
(eqs.3)
4 (eqs.4)
k GmMF F
R R
T mk GmM C
kR
2 2 2
3
2
3
We substitute k from eqs.3 into eqs.4
4 4
Thus C does not contain m. The ratio does not depend
on the planet mass m. Instead it depends on the sun mass M and is
the
T mC
GmM GMR
T
R
same for all the planets of the solar system.
m1 m2
F12 F21
r
The gravitational constant G was measured in 1798 by Henry Cavendish. He used a balance with a quartz fiber. In order to twist a quartz fiber by an angle one has to exert a torque = c (this is very similar to the spring force F = kx). The constant c can be determined easily
1 212 21 2
Gm mF F
r
(12-14)
(12-15)
F
r
F
/2 /2
Cavendish experiment: Two small
masses m are placed on either arm
of a quartz fiber balance. Two
larger masses M are placed at a
distance r from the smaller masses.
The gravitational force F
betw2
2
een M and m is:
The gravitational force on the two
smaller masses create a torque
. This torque
twists the fiber by an angle
given by: = . c
GmMF
r
GmMF
r
2c rG
mM
r
C.
apple
mg
earth
RM
(12-16)
2
2
224
In his experiment Cavendish measured the mass
of the earth! Gravitational force on apple = mg
Gravitational force on apple =
Solve for M
= 5.96 10 kg
mMG
RmMG
mgR
gRM
G
How does one measure the radius of the earth? This was already
done by Cavendish's time by as librarian in Alexandria called
Eratosthenes (around 200 BC). Eratosthenes knew that ot a
particular day every year sunlight reached the bottom of a very
deep well in Syene (modern Aswan). He also knew the distance
between Alexandria and Syene. From this information he was
able to determine R
m
C
RR
Sun’s rays
sAlexandria
Syene
well
h
Ground in Alexandria
Sun’s rays
Erathosthene’s stick
(12-17)
The distance s between Alexandria and Syene . Here
is the angle between the sun's rays and the vertical in Alexandria
at the time when the sun's rays in Syene reach the bottom of the well.
The
s R
angle was determined using Eratosthene's walking stick
and the length of the shadow it cast. tan . He got 7 h
Variation of g with height h
22
2
2
2
( ) ( )
(0) ( )
( )1
(0)
mMG
mg h RR hmMGmg R hR
g h h
g R
CR
A
B
m
mM
(12-18)
2
2
Gravitational force at point A:
( )( )
Gravitational force at point B:
(0)
Divide eqs.1 by eqs.2
(eqs.1)
(eqs.
2)
mMGmg h
R h
mMGmg
R
Note: As h increases, g(h) decreases
A
B
m
mR
C
(12-19)
2
2(1 ) 1
( )1
2 for
1(0)
2 ( ) (0) 1
1x x
g h h h
g R R
hg h g
R
x
Gravitational Potential close to the surface of the earth
In chapter 7 we saw that the potential U of the gravitational force close to the surface of the earth is:
U = mgh
mg
h
m
floor
U = 0
Note 1: Close to the surface of the earth the gravitational force is constant and equal to mg Note 2: The point at which U = 0 can be chosen arbitrarily
we will now remove the restriction that m is close to the surface of the earth and determine U (12-20)
rM m
. . mF
O x-axispath
M
xdx
Gravitational Potential U (12-21)
2
2 22
( ) ( ) ( ) ( ) Take ( ) 0
( )dx 1
1( )
x
r
r r
r
mMGU r U F x dx F x U
x
mMGdx dxU r mMG
x x
mMGU r mM
x
x
Gr
( )mMG
U rr
Escape velocity is the minimum speed with which we must launch an object from the surface of the earth so that it leaves the earth for ever
mM r=
v = 0
RM
m
ve
BeforeAfter
(12-22)
2
2
, 0 , 2
= 2 = 11 km/s The escape velocity2
does not depend on m! All objects large or small must be launched at
the same speed (1
ei f i f
ee
mv mMG mMGE E E E
R r
mv mMGv MGR
R
1 km/s) to escape from the gravitation of the earth
Example (12-2) page 327 An object of mass m moves on a circular orbit of radius r around a planet of mass M. Calculate the energy E = K + U
(12-23)
2
2
22
2
Eliminate F
between eqs.1 and eqs.2.
(eqs.1) (eqs.
2)
mMG mvF F
rr
mv mMG MGv
r rr
2
, 2 2
2
2
mMG mv m MGU K
r rmMG mMG
E U Kr
Er
rmMG
Gravitational force between extended spherical objects
.M mr
R
C
.M'
m
r
C
2
As long as the small sphere
is outside the larger sphere
the force between them is:
GmMF
r
2
If the small sphere is inside
the larger sphere the force
between them is given by:
M is the mass inside the
dotted line. The surrounding
shell sxerts zero force!
GmMF
r
(12-24)
Mm
Mm
r
M
m
r
2
GmMF
r
0F
0F
If m is outside the shell the gravitational force F is as if all the mass M of the shell is concentrated at its center and all the mass m of the sphere is concentrated at it center
If m is anywhere inside the shell then the gravitational force between the shell and the sphere is zero !
Special case: The sphere and the shell are co-centric
(12-25)