27 Query

course Phy 201

7/15 9PM

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:

This is all about the ratio

It would be:

(Earths radius/radius of the distance+earth)^2*9.8m/s/s

Confidence rating: 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.

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Self-critique (if necessary):

Would you divide the radius of earth by the total radius for the ratio?

Both radii are measured from the center of the Earth, so you would just use the two radii.

Self-critique Rating: OK

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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:

Raidus of earth/(2*radius of the earth)^2

This would be ¼(radius of earth/orbital)

Which means it would be ¼ of the gravitational field.

This is the only assessment I could come up with, but the notation sounds dumb.

Confidence rating: 1

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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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Self-critique (if necessary): I got the right answer. But this one shows it much more clearly. The use of r1 and r2 is helpful.

It's good to be able to do this without using the symbols, but it's essential to also know how to use the symbols to check our intuition.

Self-critique Rating: 2

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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?

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Your solution:

You would find force by taking (radius of earth+distance/radius of earth)^2(mass)

Then you would take Force(height) to get the Energy. The first step gets the average force since it changes as you get higher

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Confidence rating: 3

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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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Self-critique (if necessary): OK

Self-critique Rating: OK

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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:

This question makes me think about how satellites work and how they fall around the earth.

We you shoot the particles off the building, the ones with slower velocities will fall to earth and will not go as far as those with faster velocities. Once you reach a certain velocity, however, the particles will fall “around” the earth. Since the earth turns and is angled, the particle will never land. This is like a satellite.

Confidence rating: 2

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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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Self-critique (if necessary):

The idea of an elliptical orbit is a nice addition to the student solution.

Self-critique Rating: 3

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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

Confidence rating: 3

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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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Self-critique (if necessary):

Oribital radius is determined by height of tower (earth radius+height)

Self-critique Rating: 3

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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:

I would assume so, but im not really sure why.

Confidence rating: 1

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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.

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Self-critique (if necessary):

The point about air resistance is a good point, this would greatly reduce velocity over time and eventually it wouldn’t fall with earth’s curvature. I understand the point about being perpendicular with the circular orbit, which means it must be parallel with the earth.

Self-critique Rating: 3

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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:

The jet is accelerating in a circle which means this is asking for centripetal acceleration. This would be v^2/r. This is 525m/s^2/6000m which gives an acceleration of 45m/s/s.

Confidence rating:

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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'.

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Self-critique (if necessary):

I didn’t find gs which would be appropriate. This would be my 45m/s/s/(9.9m/s^2) which would be as states 4.6gs.

Self-critique Rating:

3

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

This was received on or about July 16. Responses were composed at that time but the work did not get posted. It is being posted on July 21.