27 Open Query

#$&*

course PHY 201

11/23/2011 9:48 PM

027. `query 27

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Question: `qQuery intro probs set 7, 1-7

Knowing the 9.8 m/s^2 gravitational field

strength of the Earth's field at the surface of

the Earth, and knowing the radius of the Earth,

how do we find the gravitational field strength

at a given distance 'above' the surface of the

Earth?

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Your solution:

The force at the surface is 9.8m/s^2. If an

object is above the surface the distance from

the center of the Earth has increased. Say the

radius of the Earth is 4000 km. If the object

is at 8000 km the ratio is 2 to 1. This will

be inverted and squared to obtain 1/4 then

multiplied by the original 9.8m/s^2 to obtain

the new force.

(r_earth/radius_2)^2 * 9.8m/s^2

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Given Solution:

`a** You have an inverse square force. Square

the ratio of Earth radius to orbital radius and

multiply by 9.8 m/s^2:

Field strength=(Re/r)^2*9.8m/s^2 **

STUDENT COMMENT

I used G M_earth / r^2. Wonder if they get the

same result.

INSTRUCTOR RESPONSE

For r > Re, the expressions G M_earth / r^2 and

(Re/r)^2*9.8m/s^2 give the same results, to the

number of significant figures dictated by the

known quantities.

The first formula is inherently more accurate,

because the radius of the Earth is not the same

at the poles as at the equator, with the result

that Re is not known as precisely as G and the

mass of the Earth.

STUDENT QUESTION:

???? I don't think I understand the answer. Is

mine correct? ?????

INSTRUCTOR RESPONSE:

Your method is completely equivalent to this

one, though you didn't actually show the

expressions you would get:

a_grav = k / r^2, and a_grav = g =9.8 m/s^2

when R = R_e, the radius of the Earth.

Thus

9.8 m/s^2 = k / R_e^2 and

k = 9.8 m/s^2 * R_e^2.

The proportionality becomes

a_grav = 9.8 m/s^2 * R_e^2 / r^2 = 9.8 m/s^2 *

(R_e / r)^2.

Any proportionality of the form

y = k x^p

implies that if y1 = k x1^p and y2 = k x2^p, we

have

y2 / y1 = k x1^p / (k x2^p) = (x1 / x2)^p.

In the current case p = -2, the y quantity

would be the acceleration of gravity and the x

quantity would be the distance

from the center of the Earth. Using y1 = g and

x1 = R_e, with y2 = a_grav and x2 = r, we have

a_grav / g = (r / R_e)^(-2) so that

a_grav = g * (R_e / r)^2.

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Question: `qIf we double our distance from the

center of the Earth, what happens to the

gravitational field strength we experience?

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Your solution:

The field strength will be quartered.

(1/2)^2 = 1/4

confidence rating #$&*:

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Given Solution:

`a** We have an inverse square force so if r2 =

2 * r1 the ratio of the gravitational field

will be

g2 / g1 = (1 / r2^2) / (1 / r1^2) = r1^2 / r2^2

= (r1 / r2)^2 = (r1 / (2 * r1))^2 = r1^2 / 4

r1^2 = 1/4.

In a nutshell double the radius gives us 1 /

2^2 = 1/4 the gravitational field. **

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Question: `qHow do we approximate the energy

required to move a given mass from the surface

of the Earth to a given height 'above' the

Earth, where the field strength at the given

height differ significantly from that at the

surface?

STUDENT QUESTION (applicable to University

Physics Students; others may ignore):

I'm not quite sure how this would be found.

Looking at the given solution, it looks like

you could integrate the function F =

G*m1*m2 / r^2 over the period from r1 to r2

with respect to r. What this would do would

give you the area under the

curve for a graph of F vs r (distance). That

means the area would be f*d. We know that work

= f*d, and we know that

total work = KE. So integrating will give you

the energy.

INSTRUCTOR RESPONSE

That's a very good synopsis. That would give

you an exact result. The present problem asks

for an approximation.

For your course, the integral results when you

partition the interval between r1 and r2,

approximating the work on each interval of the

partition. When you let the number of intervals

approach infinity, the approximation errors

approach zero and the resulting integral gives

you the exact work.

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Your solution:

Wouldn't you try to find an average of the

field strengths for the two distances or a mean

of several different field strengths between

the two desired points?

I don't know.

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Given Solution:

`a STUDENT SOLUTION AND INSTRUCTOR RESPONSE:

mass*[(Re + distance)/Re]^2=force

Force*distance=KE

INSTRUCTOR RESPONSE:

The first approximation would be to average the

force at the surface and the force at the

maximum altitude, then multiply by the

distance. The result would give you the work

necessary to 'raise' the object against a

conservative force, which would be equal to the

change in PE.

ADDENDUM FOR UNIVERSITY PHYSICS STUDENTS

ONLY:The exact work is obtained by integrating

the force with respect to position. You can

integrate either G M m / r^2 or m g * (RE / r)

^2 from r = RE to rMax.

Integrating G M m / r^2 from r = r1 to r = r2

you get G M m / r1 - G M m / r2, which is the

change between r = r1 and r = r2 of the

potential energy function -G M m / r (note that

this function is an antiderivative with respect

to r of G M m / r^2).**

STUDENT COMMENT

OK. `dPE = F_net * `ds

INSTRUCTOR RESPONSE

PE = F_cons_BY * `ds, where F_cons_BY is the

force exerted BY the system against

conservative forces.

There could be nonconservative forces present;

they would have no effect on the PE change but

would have to be included in F_net, so F_net *

`ds wouldn't be correct.

STUDENT COMMENT:

im not sure i understand this answer I know I

need to find KE and then the different PE from

the min and max altitudes

but I dont know if my equation represents the

same one shown here

INSTRUCTOR RESPONSE

No KE difference is assumed. We are looking

only at the work required to 'lift' the object

without speeding it up.

Energy is required because, in order to 'lift'

a mass, a force is required to counter the

gravitational pull of the Earth. If we can find

the average force required, we need only

multiply by the distance. This only gives an

approximation (see more about this below). The

work done against gravity is done against a

conservative force, and is therefore equal to

the change in gravitational PE.

You can't use the book's m g y formula because

in this case the acceleration of gravity

changes significantly from the initial point to

the final point.

The work required is equal to the area beneath

the graph of F vs. r. The graph is decreasing

at a decreasing rate (i.e., decreasing and

concave up), and is asymptotic to the positive

r axis.

See the Introductory Problem Sets for worked

problems of this nature. The approach used

there is to approximate the force at the two

distances from the center of the Earth, average

the two and use this as an approximation to the

average force. This approximation is accurate

only to the extent that the slope of the F vs.

r graph is constant.

For a given mass m we have

F = m * (r_earth / r)^2 * 9.8 m/s^2; simce m *

9.8 m/s^2 is the weight at the surface of the

earth we could write this as

F = weight_surface * (r_earth / r)^2, where

weight_surface is the weight of the mass at the

surface of the Earth..

Either way, this expression gives the force at

distance r from the center of the Earth.

So you would plug in the initial distance from

the center of the Earth, and the final

distance, obtaining two values for the force.

Averaging these two values you would have an

approximate value for the average force, which

would then be multiplied by the distance to get

the approximate work.

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Question: `qQuery class notes #24

Describe the paths of various particles 'shot'

parallel to the surface of the Earth from the

top of a very high tower, starting with a very

small velocity and gradually increasing to a

velocity sufficient to completely escape the

gravitational field of the Earth.

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Your solution:

The paths should follow a parabolic path toward

the center of the Earth. As the velocity

increases the distance the object travels

before falling back to the Earth increases.

Eventually, as the velocity of the object

increases, the path of the object will be an

elipse with the Earth at the center of one end.

If the velocity of the object is increased

even more it will escape the gravitational

force of the Earth and continue to travel away

from the Earth indefinitely.

confidence rating #$&*:

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Given Solution:

`aGOOD STUDENT ANSWER:

Each particle sets out to follow an orbit

around the center of mass of the earth. But for

particles shot at slower speeds, this path is

interupted by the surface of the eath and

simply stops there. The faster it is shot, the

further x distance becomes before the particle

lands. However, if it given a great enough

velocity, it will fall around the curviture of

the earth. If is shot even faster than that, it

will follow an eliptical oribit with varying

speeds and distances from center of earth.

GOOD STUDENT ANSWER:

With a very low velocity the projectile will

not traveled as far. It will fall to earth in a

nearly parabolic fashion since it gains

vertical velocity as it travels horizontally at

a steady pace.

If the projectile is fired at a very strong

velocity it will leave the earths vacinity but

will still be pulled by the forces acting on it

from the earths center. This will cause it to

go only so far at which point it has slowed

down considerabley, since it has lost most of

its kinetic energy. It turns and begins to gain

energy as it approaches the earths area, using

the potential energy it gained on the trip out.

(Causing it to speed up). The path that this

projectile will take will be eliptical, and it

will continue to loop around the earth.

If the projectile is fired at the correct

velocity to form a circular orbit, it will also

fall at a parabolic fashion, although the

earth's surface will also be descending at the

same rate so that the object will appear to be

'not falling'. It is falling but at the same

rate the earth is 'falling' under it. It will

circle the earth until something causes it to

stop.

INSTRUCTOR RESPONSE:

The path of the projectile will always be an

ellipse with the center of the Earth at one

focus. For low velocities and low altitude this

path is very nearly parabolic before being

interrupted by the surface of the Earth.

One of these ellipses is a perfect circle and

gives us the circular orbit we use frequently

in this section. **

STUDENT COMMENT:

I thought this object left the earths

force...if not i understand it will fall back

to earth as a normal projectile because of a

small velocity and have a parabolic path

because gravity will take over

The gravitational field of the Earth

extends forever, but as distance from the Earth

increases the strength of the field decreases

as 1 / r^2. For example at the distance of the

Moon the earth's field is only about 1/3600

times as great as at the surface of the Earth.

This is still plenty to hold the Moon in its

orbit about the Earth. The Earth's

gravitational field also affects the orbits of

other planets, even though only one planet ever

gets close enough to experience a field which

is even one-millionth as great as the field we

feel at the surface of the Earth (the other

planets are affected chiefly by the

gravitational field of the Sun).

The further a projectile or a satellite gets

from the Earth, the less gravitational force it

experiences, and if it's moving fast enough it

will keep going and never come back; but all

the while it will experience some force from

the Earth, just not enough to ever stop

it.

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Question: `qHow many of the velocities in the

preceding question would result in a perfectly

circular orbit about the Earth?

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Your solution:

One

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Given Solution:

`a** For a given distance from the center of

the Earth, there is only one velocity for which

centripetal acceleration is equal to

gravitational acceleration, so there is only

one possible velocity for a circular orbit of

given orbital radius. The orbital radius is

determined by the height of the 'tower', so for

a given tower there is only one velocity which

will achieve a circular orbit. **

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Question: `qIs it necessary in order to achieve

a circular orbit to start the object out in a

direction parallel to the surface of the Earth?

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Your solution:

The path would have to be horizontal with the

surface of the Earth. The velocity would also

have to be exact in order to maintain the

parallel path. The force of the initial launch

would have to be equal to the force of the

""pull"" from the center of the Earth for the

object to maintain the parallel trajectory.

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Given Solution:

`a** If you have just one 'shot' then you must

start out parallel to the surface of the Earth.

The reason is that any circle about the center

must be perpendicular at every point to a

radial line--a line drawn from the center to

the circle. Any radial line will intercept the

surface of the Earth and must be perpendicular

to it, and the circular orbit must also be

perpendicular to this line. Therefore the orbit

and the surface are perpendicular to the same

line and are therefore parallel. **

STUDENT COMMENT: im now seeing the idea of a

launch paralell to earth. the tower needs to be

pretty tall then.

the velocity needs to be headed in the

direction of the orbit it will take.

INSTRUCTOR REPSONSE: The main reason it has to

be very tall is because of the atmosphere. If

you shoot the projectile with sufficient speed

while it's in the atmosphere, it will quickly

lose most of its kinetic energy to air

resistance; the energy goes mostly into heating

the object, which as a result proceeds to melt

as its orbit decays. Whether it melts before

hitting the ground or not depends on how

quickly the orbit decays and how high it was in

the first place.

If there was no atmosphere, you still would

need to be careful about the flattening of the

Earth at the equator (the radius at the equator

is about 20 km greater than the radius at the

poles, which means that if you wanted an orbit

that took you over the equator, then even in

the absence of atmosphere a tower at the pole

would have to be at least 20 km high.

STUDENT QUESTION

When a rocket is launched why is it pointed

straight up, isnt this perpendicular to the

earth surface, would it be more effective to

have it pointed at an angle to be shot parallel

with the orbit and the surface of the earth?

INSTRUCTOR RESPONSE

Excellent question.

You want to get out of the atmosphere as

quickly as possible, to minimize the work you

need to do against air resistance.

A vertical launch position is much more stable

than one at an angle away from vertical. Same

reason we build towers vertical rather than

leaning.

The launch starts out vertical, and gradually

curves toward the tangential direction.

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Question: `qPrinciples of Physics and General

College Physics Problem 5.2: A jet traveling at

525 m/s moves in an arc of radius 6.00 km. What

is the acceleration of the jet?

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Your solution:

a=v^2/r,

a= (525m/s)^2/6000m,

a=46m/s^2 approx

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Given Solution:

`aThe jet will have centripetal acceleration

a_cent = v^2 / r, where v is its speed and r

the radius of the circle on which it is

traveling. In this case we have v = 525 m/s and

r = 6.00 km = 6000 meters.

The centripetal acceleration is therefore

a_cent = v^2 / r = (525 m/s)^2 / (6000 m) = 45

m/s^2, approx.. One 'g' is 9.8 m/s^2, so this

is about (45 m/s^2) / (9.8 m/s^2) = 4.6 'g's'.

STUDENT QUESTION:

there are roughly 1600m in a mile I believe, so

45m/s would be 2700m a minute and 162,000m/hr.

so that would be roughly 100mi/hour, am I

making a math error here or is that speed

really 4.6g’s???

INSTRUCTOR RESPONSE: That speed would be about

100 mph. However 100 mph is not an

acceleration, but as you say, a speed.

g's measure acceleration, not speed.

Nothing here is moving at 45 m/s.

There is a centripetal acceleration of 45

m/s^2. One 'g' is 9.8 m/s^2. So 45 m/s^2 is

somewhat more than 4 'g's'. It is in fact 4.6

g's.

STUDENT QUESTION

What does g stand for?

INSTRUCTOR RESPONSE

g stands for the acceleration of gravity. One

'g' is 9.8 m/s^2. Two 'g's' would be 19.6

m/s^2. etc.

At 10 g's you pass out; if you continue this

acceleration for more than a couple of minutes

you die.

A fighter jet in a turn can withstand 10 g's;

the pilot can't.

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Question: `qUniv. Why is it that the center of

mass doesn't move?

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Your solution:

???

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Given Solution:

`a** There is no net force on the system as a

whole so its center of mass can't accelerate.

From the frame of reference of the system,

then, the center of mass remains stationary. **

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Self-critique (if necessary):

Is this saying the sum of the system? So

relative to every object in the system, the

center of the mass of the entire system remains

stationary as every mass in the system flies

around?

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@& From the frame of reference of the center of mass, that description is correct.

To an observer whose frame of reference is moving at with respect to the center of mass, the center of mass moves and the rest of the system moves around it.

For example if someone throws a baseball bat or a golf club, it will rotate about its center of mass. If air resistance is negligible, the center of mass will move along in a parabolic arc, just as would a thrown ball. The center of mass is closer to the 'fat' end of the bat or the head of the club.

It would be theoretically possible to throw a ball so that its motion matches that of the bat. The ball would then be moving in the frame of reference of the center of mass. The center of mass of the bat would, in this frame, appear stationary. The ends of the bat would rotate about this stationary point, the fat end rotating about a circle of smaller radius than the handle.

*@

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&#This looks good. See my notes. Let me know if you have any questions. &#