PHY 201
Time and Date Stamps (logged): 07:28:00 09-04-2009
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Test is to be taken without reference to text or outside notes.
Graphing Calculator is allowed, as is blank paper or testing center paper.
No time limit but test is to be taken in one sitting.
Please place completed test in Dave Smith's folder, OR mail to Dave Smith, Science and Engineering, Va. Highlands CC, Abingdon, Va., 24212-0828 OR email copy of document to dsmith@vhcc.edu, OR fax to 276-739-2590. Test must be returned by individual or agency supervising test. Test is not to be returned to student after it has been taken. Student may, if proctor deems it feasible, make and retain a copy of the test..
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Numerical answers should be correct to 3 significant figures. You may round off given numerical information to a precision consistent with this standard.
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Problem Number 1
Using proportionality, the acceleration of gravity at the surface of the Earth and the fact that the radius of the Earth is approximately 6400 km, use proportionality to find:
The field strength at twice the radius of the Earth from its center. 1/4
The strength at 4 times the radius of the Earth from its center. 1/16
The strength at a distance of 25700 kilometers from its center. 25700 / 6400 = 1/ 16.1
25700 / 6400 = 1/4, not 1/16.
Because of the inverse square law this should be (25700 / 6400)^2.
It appears that this is how you calculated your result; 1/16 is the correct ratio. I suspect you just forgot to type in the square.
The distance from Earth's center where the
gravitational field of the Earth is half its value at the surface. 1.414 * 6400 = 9051 km.This is correct, but you don't say how you got this result.
Problem Number 2
A turbine accelerates uniformly at 2.2 radians/second/second.
How long will it a to accelerate from 2.2 radians/second to 4.6 radians/second?
Through what angular displacement will it turn in this time?
.V= Vo + at
(note: I've changed your W's to omega's; the correct symbol is w).
theta = wot + ½ αt^2 x = Vot
t = w wo
. α
4.6 r/s 2.2 r/s =
2.4 r/s = 1.09 s2.4 rad/s is not equal to 1.09 s, nor is 1.09 s equal to 4.6 rad/s - 2.2 rad/s.
However I believe you calculated your result correctly. The calculation should be expressed as follows:
`dOmega = 6.4 rad/s - 2.2 rad/s = 2.4 rad/s, and
`dt = `dOmega / alpha = 2.4 rad/s / (2.2 rad/s^2) = 1.09 s.
The = sign means 'equal to'. It shouldn't be used to express 'train of thought'. The sign needs to be reserved for equality. To do otherwise is to risk serious error and miscommunication.</h3>
. 2.2 r/s 2.2 r/s/s
.S = rθ
θ = Vot + ½ α t^2
2.2 r/s (1.09) + ½ (2.2
r/s) (1.09s)^22.398 r/s^2 + .5995 =
2.9975 rad..<h3>Your meaning is clear, but isn't expressed precisely.
`ds = r `dθ is the arc distance corresponding to angular displacement `dTheta on a circle of radius r.
θ = omega_0 t + ½ α t^2 is a correct equation; the equation implicitly assumes that theta = 0 when t = 0.
In the notation I use in this course, which focuses attention on intervals and makes fewer implicit assumptions (e.g., the assumption in the preceding that theta = 0 when t = 0), the notation would read:
`dθ
= omega_0 `dt + ½ α `dt^2Your units don't work out correctly in the next equation, which should read
2.2 rad/s
(1.09 s) + ½ (2.2 rad/s) (1.09s)^22.398 rad + .5995 rad = 2.9975 rad.
I don't recommend abbreviating 'rad' as 'r'; much too easy to confuse with the radius of the circle.
Problem Number 3
What is the acceleration of an object of mass 760 kilograms in circular orbit about a planet of mass 2 *10^ 24 kilograms at a radius of 20000 kilometers?
How fast must be object be traveling if it is to remain in a circular orbit about the planet?
How long will it take the object to complete one orbit? Neglect any difference between the radius of the orbit and the distance between the object and the center of the planet.
.Fg = G m1 m2
. r^2
<h3>Your notation didn't come through correctly; it's clear however that you mean
F_grav = G m1 m2 / r^2.</h3>
Fg = (6.67 x 10^-11 N*m^2 /
kg^2) ( (2 x 10^24 kg) (760 kg)) / (20000000 m )^2F = ma
A = F/m = 253.46 N /
(760 kg) = .3335 m/s^2V1 = A_r
* R = 0.3335 m/s^2The acceleration you calculate is the centripetal acceleration, not the radial acceleration. Gravity attracts the satellite toward the center of the planet. In a circular orbit, the force is completely perpendicular to the orbit and hence does not change the speed of the satellite, only its direction.
Thus
a_cent = F_grav / m = .33 m/s^2.
a_cent = v^2 / r so v = sqrt( a_cent * r) = sqrt( .33 m/s^2 * 20 000 000 m) = 2600 m/s, approx..
This is consistent with the result you give below for v2.
Note that lower-case symbols are generally used for velocity and acceleration.</h3>
V2 = (0.3335
m/s^2)(20000000 m) = sqrt (6700000 m^2 / s^2)V = 2588.4 m/s
Ar = 4π^2 r / a = sqrt
(2367521296) = 48657.2 s = 13.5 hr..<h3>the circumference of the circle is 2 pi r
the time required to complete a revolution is therefore
T = 2 pi r / v = 2 pi * 20 000 000 m / (2600 m/s). I believe this comes out to nearly double the 13.5 hr you calculated.
Problem Number 4
How much paint is applied per square meter if 4 gallons of paint are uniformly spread out over the surface of a sphere of radius 4.1 meters?
By what factor does the amount per square meter change in each of the following situations:
The paint is applied over a sphere of double the radius. 1/4
The paint is applied over a sphere of quadruple the radius. 1/16
The paint is applied over a sphere of radius 11 meters. 1/7.2
A = 4πr^2
A = 4π(4.1)^2 = 211.2 m^2
4 / 211.2 = .0189 gal / m^2
Problem Number 5
A small object orbits a planet at a distance of 20000 kilometers from the center of the planet with a period of 66 minutes. What is the mass of the planet?
.T^2 / r^3 = 4π^2 / GM
<h3>You don't need this formula. You can calculate this in terms of the velocity v = sqrt( G M / r) and the fact that orbital period = circumference / velocity.</h3>
T^2 GM = r^3 4π^2
M = 4π^2 r^3 =
4π^2 (20,000 km)^3 = 7.425 x 10^18. GT^2 6.67 x 10^-11 (66)^2
orbital circumference is 2 pi r = 2 pi * 20 000 000 m
orbital velocity is therefore 2 pi * 20 000 000 m / (66 min * 3600 s / min)
Solving v = sqrt( G M / r) for M we get M = v^2 r / G. Using the velocity from above, with r = 20 000 000 m and G = 6.67 * 10^-11 N m^2 / kg^2, you can easily find the planet's mass.
The only formulas necessary for these problems are
F_grav = G m1 m2 / r^2
PE = - G m1 m2 / r
a_cent = v^2 / r
Of course this assumes that you understand conservation of energy, Newton's Second Law and the basic geometry of the circle. With this knowledge you can easily derive the important formula v = sqrt( G M / r):
for a circular orbit of a satellite of small mass about a planet the centripetal force F_cent = m * a_cent is provided by the gravitational attraction between satellite and planet so that
m2 * a_cent = G m1 m2 / r^2, or
m2 * v^2 / r = G m1 m2 / r^2. This is easily solved for v. We obtain
v = sqrt( G m1 / r). m1 is the mass of the planet, more often expressed as M, giving us
v = sqrt( G M / r).
You should either memorize this equation or be able to derive it from the three basic equations.
Orbital period is easy to determined in two simple steps, using the three basic relationships, from the fact that circumference = 2 pi r and v = sqrt( G M / r). It's OK to do so, but it should be unnecessary to memorize and rely on a separate formula. The formula can easily be derived:
v = sqrt( G M / r) and
T = 2 pi r / v so
T = 2 pi r / sqrt( G M / r) = 2 pi sqrt( r^3 / (G M) ).
This is easily rearranged into the equation you quote above
T = 2 pi sqrt(r^3 / (G M) ) so
sqrt( r^3 / (G M) ) = T / (2 pi). Squaring both sides
r^3 / (G M) = T^2 / (4 pi^2). If we choose to express this without denominators we get
4 pi^2 r^3 = T^2 G M.
It's OK to memorize this, but it's a fairly confusing equation to remember (among other things, it's not obvious why in the world is there a 4 pi^2 in the equation, but it is clear from middle-school geometry why the circumference of the orbit is 2 pi r) and for most students it's easier to work from basic principles.
Problem Number 6
How long does it take an object moving around a circular track to sweep out an angle of 10.99 radians while accelerating uniformly at .2 radians/second ^ 2? Its initial angular velocity is 6 radians/second.
What is its angular velocity after having swept out the 10.99 radians?
α * 2θ = w^2 wo^2
In the interval-orieneted notation of this course this is a rearrangement of the fourth equation of motion
omega_f^2 = omega_0^2 + 2 alpha `dTheta; rearranged you get
2 alpha `dTheta = omega_f^2 - omega_0^2.
Your equation
2 α * θ = w^2 w_0^2
has the same meaning, if you recall the implicit assumption that theta = 0 when t = 0, and use omega for the variable angular velocity.
w^2 = α2θ + wo^2
(.2 rad /
s ^2) (2) (10.99 rad) + (6 rad/s)^2w^2 = 158.256
The units of both terms, and hence the sum, would be rad^2 / s^2.
w = 12.58 rad / s
T = w wo = 12.58 rad / s 6.0 rad / s
= 32.9 sUppercase T is generally used for things like the period of an orbit or a cycle; lowercase t is standard notation for clock time; in the interval notation of this course we generally use `dt, in order to avoid often-confusing implicit assumptions, but as long as those assumptions are understood t is fine.
However 12.58 rad / s 6.0 rad / s = 32.9 s is a false statement. The units of one side are rad / sec and the units of the other are s. Also 12.58 - 6.0 is not equal to 32.9; the numbers simply don't match.
Your intention is clear. You mean
t
= (w wo) / alpha = (12.58 rad / s 6.0 rad / s) / (.2 rad/s^2) = 32.9 s,which is the correct result for the time interval required for the given change in angular velocity (again, being a time interval I recommend but do not insist that it be denoted `dt).
. α 0.2 rad /s ^2
Problem Number 7
How many degrees are in each of the following angles:
1 radian
57.325 degrees`pi radians 180.092
degrees`pi /2 radians and 90.046 degrees
`pi /6 radians?
30.015 degrees.You appear to be using the approximation 1 radian = 57.325 degrees as a basis for your calculations.
This leads to approximation errors, which might or might not be significant. You wouldn't want to send a spacecraft to Mars using that approximation. At best you would waste valuable fuel correcting your incorrect course; at worst you would miss the planet or crash into it.
In any case, you need to use the exact conversion, which is based on the simple fact that 2 pi radians = 360 degrees. It follows that 1 radian = 360 / (2 pi) deg = (180 / pi) deg, which is the exact result you have approximated.
It also follows that 1 degree = (pi / 180) rad.
Having obtained the exact result, you can then approximate as appropriate to the situation. In this case the exact results are expressed very simply, with no need for approximation:
The conversions requested here would be
pi rad = pi * (180 / pi) deg = 180 deg
pi/2 rad = pi/2 ( 180 / pi) deg = 90 deg
pi/6 rad = pi/6 (180 / pi) deg = 30 deg.
These results are exact.</h3>
Problem Number 8
During an observation, a rotating object is observed to rotate through 63.6 radians while uniformly accelerating from 1.25 radians/second to 4.599 radians/second.
If the object has moment of inertia 1.899 kg m ^ 2, what net torque was required?
α = w^2
wo^2 = (4.599 rad / s)^2 (1.25)^2 = 622.9 rad / s^2 2θ 2(63.6 rad)
Σϒ = I α
Σϒ = (1.899 kg * m^2) (622.9 rad/ s^2)
Σϒ = 1182.9 m*N kg / m^2 / s^2 * rad
Your notation didn't come through completely as you intended, but while you were on the right track you do have an incorrect result for the angular acceleration.
The correct angular acceleration is
alpha = (omega_f^2 - omega_0^2) / (2 `dTheta) = ( (4.6 rad/s)^2 - (1.25 rad/s)^2) / (2 * 63.6 rad) = .1 rad / s^2, very approximately.
You are using the correct relationships throughout this problem. Your only errors seem to be in details.
Continuing:
Your symbol for torque didn't come through at all, but I've inserted the symbol for the Greek letter tau in your solution below, I've changed the angular acceleration to the very approximate result obtained above, and I've corrected the units at the end:
Σt
= I αΣt
= (1.899 kg * m^2) (.1 rad/ s^2)Σt
= .18 kg * m^2 / s^2 = .18 m N.The unit kg * m^2 * rad / sec^2 simplifies to kg * m^2 / s^2; a radian of angle corresponds to an arc distance equal to the radius so m * rad converts simply to m (a meter of radius multiplies by a radian is a meter of arc).
kg * m^2 / s^2 = m * (kg m/s^2) = m * N.
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21:37:25
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What would be the tension in the string if the
system was on and stationary with respect to the surface of the Earth, with the ball being swung in a vertical circle, when the ball is at the top of its arc?......!!!!!!!!...................................
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21:37:47
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If the ball is at the bottom of its arc the net
force consists of the tension plus the gravitational force, with tension up and gravity down. Again using downward as the positive direction and noting that the upward centripetal acceleration is with this assumption negative we have......!!!!!!!!...................................
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Problem Number 5
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What will be their total kinetic energy?
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Using the Impulse-Momentum Theorem determine the
average force exerted on the bullet as it accelerates along the length of the barrel.......!!!!!!!!...................................
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21:38:53
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