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    Chapter 13 Gravitation

    In this chapter we will explore the following topics:

    -Newtons law of gravitation that describes the attractive force between

    two point masses and its application to extended objects

    -The acceleration of gravity on the surface of the earth, above it,

    as well as below it.

    -Gravitational potential energy

    -Keplers three laws on planetary motion

    -Satellites (orbits, energy , escape velocity)

    (13-1)

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    Claudius Ptolomeu

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    In contrast, planets follow complicated paths

    in the sky. An example of such motion is

    given in the figure. Tycho Brahe made

    very careful measurementsof planetary

    motions but he died before he had

    the chance to analyze his data.

    (13-12)

    This task was carried out by his assistant Johannes Kepler who summarized

    the results into three empirical laws known by his name.

    Later, Newton used his second law of motion with his gravitational law

    and the newly developed methods of calculus and derived Kepler's laws

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    Nicolau Coprnico

    Giordano Bruno

    Galileu Galilei

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    The square of the period of any planet is proportional to

    the cube of the semimajor For the sake

    of simplicity we will consider

    Keple

    the c

    r's Third

    irculr orb

    axis

    it sh

    la

    ow

    of

    n i

    its

    n

    t

    or

    he

    w

    bit.

    figure.

    ( ) ( )2 2 22 3

    A planet of mass moves on a circular orbit of radius around a star of mass .

    We apply Newton's second law to the motion:

    (eqs.1) The period can be expressed

    in

    g

    m r M

    GMm GM F ma m r m r T

    r r

    = = = = =

    22

    2

    2

    2

    3

    2 2

    3

    2 4terms of the angular speed . = (eqs.2)

    If we substitute form eqs.1 into eqs.2 we get:

    : The ratio does

    4

    not deNote pend on the mass of the1

    p

    T

    r M

    T

    m

    G

    T

    T

    r

    =

    =

    2

    3Note 2:

    lanet but only on the mass of the central star.

    For elliptical orbits the ratio remains cons at nt

    M

    T

    a (13-14)

    2 2

    3

    4

    T

    r MG

    =

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    m1

    m2

    1 2

    2m mF G

    r=

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    m1

    m2

    F12

    F21

    r

    m1

    m2r

    F1

    m2

    m1

    1 2

    2

    m mF G

    r=

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    (13-4)

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    1. A Terra no uniformemente distribuda2. A Terra no esfrica

    3. A Terra est girando

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    y-axis

    3. Terra est girando

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    m1m2

    r

    F1

    m2

    m1

    Newton proved that the net gravitational force on a particle by a shell depends

    on the postion of the particle with respect to the shell

    If the pa

    Gravitation

    rticle is i

    insid

    nside

    e the ear

    the s

    th

    hell,

    1 21 2

    the net force is zero

    If the particle is outside the shell the force is given by:

    Consider a mass inside the earth at a distance from the center of the earth

    If we divide the earth in a

    m r

    m mF G

    r=

    2

    series of concentric shells, only the shells with

    radius less than exert a force on . The net force on is:

    Here is the mass of the part of the earth inside a sphere os radius

    ins

    ins

    i

    GmMr m m F r

    M r

    M

    =

    34 4is linear with r

    3 3ns ins

    r GmV F r F

    = = =

    (13-7)

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    (13-9)

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    r

    m

    In chapter 8 we derived the potential energy of a mass

    near the surface of the earth. We will remove this restriction

    and assume that t

    Gravitational P

    he mass can

    otential E

    move away

    ne

    fr

    rgy

    om th

    U m

    m e surfaceof the earth, at a distance from the center of the earth as shown

    in the figure. In this case the gravitational potential energy is:

    The negative sign of expresses the fact thGmM

    Ur

    r

    U= at

    the corresponding gravitational force is

    The gravitational potential energy is not only associated

    with the mass but with as well i.e. w

    att

    ith

    N

    ot

    bo

    rac

    th

    tiv

    o

    e

    b

    :

    s

    e

    jectm M

    1 2 3

    1 3 2 31 2

    12 13 23

    If we have three masses , , and positi oned as shown in the figure

    the potential energy due to the gravitational forces among the objects is:

    We take into

    m m m

    U

    Gm m Gm mGm mU

    r r r

    = + +

    account each paironce

    (13-8)

    GmM

    Ur

    =

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    m

    r =

    B

    v = 0

    m

    v

    A

    If a projectile of mass is fired upward

    at point A as shown in the figure, the projectile

    will stop momentarily and return t

    Escape

    o the e

    Spe

    .

    ed

    arth

    m

    There is however a minimum initial speed for which the projectile

    will escape from the gravitational pull of the earth and will stop

    at infinity (point B in the figure). This minimum speed is known as

    es

    2

    2

    We can determine the escape velocity using

    energy conservation between point A and point B.

    cape velo

    02

    02

    The escape speed form the earth

    2

    city.

    is

    A B

    A B

    mv GMmE K U E K U

    R

    mv GMmE ER

    GMvR

    = + = = + =

    = = =

    11.2 km/s

    The escape speed does depeNote: ndnot on m

    (13-10)

    2

    GMv

    R=

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    Stars follow regular paths in the evening sky.

    They rotate once every 24 hours about

    an axis that passes through the

    star polari

    Planets and Satellites: Kepler'

    s. Polaris is the only star

    th

    s Laws

    at does not move in the sky.

    The stars have fixed spatial relationships

    among them. Humans have

    classified them in groups

    known as "constellations"

    Polaris

    Celestial

    sphere

    Rotation Axis

    of the

    Celestial

    sphere

    earth

    N

    S

    Star

    (13-11)

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    22

    2

    Consider a satellite that follows a circular orbit of radius

    around a planet of mass . We apply Newton's second

    law and hav

    Sate

    e:

    llites: Orbits and Ener

    The kinetic ene

    gy

    rgy

    r

    M

    GMm v GM

    ma m vr r r= = =2

    (eqs.1)2 2

    The potential energy (eqs.2)

    If we compare eqs.1 with eqs.2 we have: (eqs.3)2

    The total energy2 2

    The energies ,

    mv GMmK

    r

    GMmU

    r

    UK

    GMm GMm GMmE K U K

    r r r

    E K

    = =

    =

    =

    = + = = =

    , and are plotted as function of rin the figure to the left.

    For elliptical orbits2

    Note:

    U

    GMmE

    a=

    (13-15)

    2

    GMmE

    r=