Query 2

#$&*

course Phy 242

002. `query 2*********************************************

Question: from Introductory Problem Set 5 # 11: Finding the conductivity given rate of energy flow, area,

temperatures, thickness of wall.

Describe how we find the conductivity given the rate of energy flow, area, temperatures, and thickness of the wall.

YYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYY

Your Solution: When given the rate of energy flow, area, temperatures, and thickness of the wall you start out by

finding the temperature gradient. The temperature gradient is equal to the change in temperature divided by the

thickness of the wall. Since rate of energy flow is equal to the temperature gradient times the area of the wall

times the conductivity, you plug in the known values (rate of energy flow, area of wall, and temperature gradient)

and solve for the unknown (conductivity).

The equation:

Rate of energy flow=temperature gradient*area of the wall*conductivity

Once you solve for the temperature gradient, everything else is pretty straight forward.

Isolate conductivity by dividing over the temperature gradient and the area of the wall.

confidence rating #$&*:

^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^

.............................................

Given Solution:

** The rate at which thermal energy is conducted across for a object made of a given substance is proportional to the

temperature gradient (the rate at which temperature changes across the object), and to the cross-sectional area of

the object.

The conductivity is the constant of proportionality for the given substance. So we have the proportionality equation

· rate of thermal energy conduction = conductivity * temperature gradient * area, or in symbols

· R = k * (`dT/`dx) * A.

(note: R is the rate at which thermal energy Q is transferred with respect to clock time t. Using the definition

of rate of change, we see that the average rate over a time interval is `dQ / `dt, and the instantaneous rate is dQ /

dt. Either expression may be used in place of R, as appropriate to the situation.)

For an object of uniform cross-section, `dT is the temperature difference across the object and `dx is the distance

between the faces of the object. The distance `dx is often denoted L. Using L instead of `dx, the preceding

proportionality can be written

· R = k * `dT / L * A

We can solve this equation for the proportionality constant k to get

· k = R * L / (`dT * A).

(alternatively this may be expressed as k = `dQ / `dt * L / (`dT * A), or as k = dQ/dt * L / (`dT * A)).

STUDENT COMMENT

I really cannot tell anything from this given solution. I don’t see where the single, solitary answer is.

INSTRUCTOR RESPONSE

The key is the explanation of the reasoning, more than the final answer, though both are important.

However the final answer is given as k = R * L / (`dT * A), where as indicated in the given solution we use L instead

of `dx. Two alternative answers are also given.

Your solution was

'Well, according to the information given in the Introductory Problem Set 5, finding thermal conductivity (k)

can be determined by using k = (‘dQ / ‘dt) / [A(‘dT / ‘dx)].'

The given expressions are equivalent to your answer. If you replace `dx by L, as in the given solution, and simplify

you will get one of the three given forms of the final expression.

However note that you simply quoted and equation here (which you did solve correctly, so you didn't do badly), and

gave no explanation or indication of your understanding of the reasoning process.

Self-Critique: I didn't go into nearly as much detail but the point was the same.

------------------------------------------------

Self-Critique Rating: 3

*********************************************

Question: Explain in terms of proportionalities how thermal energy flow, for a given material, is affected by area

(e.g., is it proportional to area, inversely proportional, etc.), thickness and temperature gradient.

your answer: vvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvvv Thermal energy flow is proportional to area and temperature gradient. This is easy to tell by looking at

the equation used in the question above:

Rate of thermal energy flow=temperature gradient*area of the wall*conductivity

If you increase the area or the temperature gradient, the rate of thermal energy flow will increase. If you decrease

the area of the temperature gradient, the rate of thermal energy flow will also decrease. This is why I said they are

proportional to each other.

However, this is not the case for the thickness. This is harder to see since in the formula above, thickness is not

in plain sight. You have to remember that when you solved for the temperature gradient, you took the difference in

temperatuer and divided by thickness. So if I rewrite the equation above showing this, this is how it looks:

Rate of thermal energy flow=[(T2-T1)/thickness]*area of the wall*conductivity

Now, it is easier to see the relationship thickness has with rate of thermal energy flow. Since the thickness is in

the denominator, as it increases, this will decrease the rate of thermal energy and when it decreases, this will

increase the rate of thermal energy flow. This means that thickness is inversely proportional to the rate of thermal

energy flow.

confidence rating #$&*:

^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^

.............................................

Given Solution:

** CORRECT STUDENT ANSWER WITHOUT EXPLANATION:

Energy flow is:

· directly proportional to area

· inversely proportional to thickness and

· directly proportional to temperature gradient

Good student answer, slightly edited by instructor:

The energy flow for a given object increases if the cross-sectional area (i.e., the area perpendicular to the

direction of energy flow) increases. Intuitively, this is because the more area you have the wider the path

available so more stuff can move through it. By analogy a 4 lane highway will carry more cars in a given time

interval than will a two lane highway. In a similar manner, energy flow is directly proportional to cross-sectional

area.

Temperature gradient is the rate at which temperature changes with respect to position as we move from one side of

the material to the other. That is, temperature gradient is the difference in temperature per unit of distance

across the material:

· temperature gradient is `dT / `dx.

(a common error is to interpret temperature gradient just as difference in temperatures, rather than temperature

difference per unit of distance).

For a given cross-sectional area, energy flow is proportional to the temperature gradient. If the difference in the

two temperatures is greater then the energy will move more quickly from one side to the other.

For a given temperature difference, greater thickness `dx implies smaller temperature gradient `dT / `dx. The

temperature gradient is what 'drives' the energy flow. Thus

greater thickness implies a lesser temperature gradient

the lesser temperature gradient implies less energy flow (per unit of cross-sectional area) per unit of time and we

can say that

the rate of energy flow (with respect to time) is inversely proportional to the thickness.

Self-Critique: OK

------------------------------------------------

Self-Critique Rating: OK

*********************************************

Question: principles of physics and general college physics 13.8: coeff of expansion .2 * 10^-6 C^-1, length 2.0

m. What is expansion along length if temp increases by 5.0 C?

YYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYY

Your Solution: ???I'm assuming this doesn't apply to me since I am university physics???

@&

That is correct.

*@

confidence rating #$&*:

^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^

.............................................

Given Solution:

This problem is solved using the concept of a coefficient of expansion.

The linear coefficient of thermal expansion of a material, denoted alpha, is the amount of expansion per unit of

length, per unit of temperature:

· expansion per unit of length is just (change in length) / (original length), i.e.,

· expansion per unit of length = `dL / L0

Thus expansion per unit of length, per unit of temperature is (expansion per unit of length) / `dT. Denoting this

quantity alpha we have

· alpha = (`dL / L0) / `dT. This is the 'explanatory form' of the coefficient of expansion. In

algebraically simplified form this is

· alpha = `dL / (L0 * `dT).

In this problem we want to find the amount of the expansion. If we understand the concept of the coefficient of

expansion, we understand that the amount of the expansion is the product of the coefficient of expansion, the

original length and the temperature difference: If we don’t completely understand the idea, or even if we do

understand it and want to confirm our understanding, we can solve the formula alpha = `dL / (L0 * `dT) for `dL and

plug in our information:

· `dL = alpha * L0 * `dT = .2 * 10^-6 C^(-1) * 2.0 m * 5.0 C = 2 * 10^-6 m.

This is 2 microns, two one-thousandths of a millimeter.

By contrast the coefficient of expansion of steel is 12 * 10^-6 C^(-1); using this coefficient of expansion yields a

change in length of 1.2 * 10^-4 m, or 120 microns, which is 60 times as much as for the given alloy.

Self-Critique:

------------------------------------------------

Self-Critique Rating:

*********************************************

Question: query general phy 13.12: what is the coefficient of volume expansion for quartz, and by how much does

the volume change? (Note that Principles of Physics and University Physics students do not do General Physics

problems)

YYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYY

Your Solution:

confidence rating #$&*:

^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^

.............................................

Given Solution:

** The coefficient of volume expansion for quartz is 1 x 10^(-6) C^(-1).

The sphere has diameter 8.75 cm, so its volume is 4/3 pi r^3 = 4/3 pi ( 4.38 cm)^3 = 352 cm^3, approx..

The coefficient of volume expansion is the proportionality constant beta in the relationship `dV = beta * V0 * `dT

(completely analogous to the concept of a coefficient of linear expansion).

We therefore have

`dV = beta* V0*dT = 3 x 10^(-6) C^ (-1) * 352 cm^3 * (200C - 30 C) = 0.06 cm^3 **

STUDENT COMMENT:

Similar to length an increase in temp. causes the molecules that make up this substance to move faster and that is

the cause of expansion?

INSTRUCTOR RESPONSE:

At the level of this course, I believe that's the best way to think of it.

There is a deeper reason, which comes from to quantum mechanics, but that's is way beyond the scope of this course.

STUDENT COMMENT

I found it difficult to express this problem because I was unable to type a lot of my steps into word, as they

involved integration. However, I will take from this exercise that I should be more specific about where I got my

numbers from and what I was doing for each of the steps I am unable to write out.

INSTRUCTOR RESPONSE

Your explanation was OK, though an indication of how that integral is constructed would be desirable. I understood

what you integrated and your result was correct.

For future reference:

The integral of f(x) with respect to x, between x = a and x = b, can be notated

int(f(x) dx, a, b).

A common notation in computer algebra systems, equivalent to the above, is

int(f(x), x, a, b).

Either notation is easily typed in, and I'll understand either.

Self-Critique:

------------------------------------------------

Self-Critique Rating:

*********************************************

Question: `q001. A wall of a certain material is 15 cm thick and has cross-sectional area 5 m^2. It requires

1200 watts to maintain a temperature of 20 Celsius on one side of the wall when the other side is held at 10 Celsius.

What is the thermal conductivity of the material?

How many watts would be required to maintain a wall of the same material at 20 Celsius when the other is at 0

Celsius, if the cross-sectional area of the wall was 3000 cm^2?

YYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYY

Your Solution: The thermal conductivity is 1.8 watts/(C m). I found this by using the equation 'dQ/'dt=kA*'dT/'dx.

@&

You don't show the quantities you used to calculate this, but I got double what you got.

*@

Note: the thickness was in cm so I converted it to m and got 0.15 meters.

72 watts would be required. I found this by using the thermal conductivity that I found above and multiplying that by

the temperature gradient and the area. Note: the area was in cm^2 and needed to be converted to m^2 and when it was

converted it came out to be 0.3 m^2.

@&

3000 cm^2 is 0.3 m^2, which is about 1/17 the cross-sectional area of the preceding. The temperature change is double that of the preceding so, thickness being the same, the temperature gradient is double. Double the temperature gradient and 1/17 the cross-sectional area would result in about 2/17 the energy flow.

*@

confidence rating #$&*:

^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^

------------------------------------------------

Self-Critique Rating: There is no solution to self-critique so I can't give myself a self-critique rating.

*********************************************

Question: `q002. What is the specific heat of a material if it requires 5000 Joules to raise the temperature of

half a kilogram of the material from 20 Celsius to 30 Celsius?

By how much would the temperature of 100 grams of the same material change if it absorbed 200 Joules of heat?

YYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYY

Your Solution: The specific heat is 1000 J/(Kg C). I found this by knowing that specific heat is equal to the thermal

energy divided by the mass and temperature increase. (specific heat= thermal energy/(mass*change in temperature)

The temperature would change by 2 degrees Celsius. I found this by knowing the specific heat that I found above and

using the formula c='dQ/(m'dT). Plugging in the knowns (specific heat (c), change in thermal energy ('dQ), and mass

(m)), you can solve for the change in temperature ('dT).

confidence rating #$&*:

^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^

------------------------------------------------

Self-Critique Rating: There is no solution to self-critique so I can't give myself a self-critique rating.

*********************************************

Question: query univ 17.101 / 17.103 (15.93 10th edition) (Note that Principles of Physics and General College

Physics students don't do University Physics problems).

A copper calorimeter of mass .446 kg contains .095 kg of ice, all at 0 C. .035 kg of steam at 100 C and 1 atm

pressure is added. What is the final state of the system?

YYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYY

Your Solution: The final state of the system is going to be a liquid. I determined this by finding the different

energies required to do different things. First I found the energy required to melt the .095 kg of ice by multiplying

the mass times the heat of fusion (3.3*10^5 J/kg). This equals 31,350 J. If the water then rises from 0 degrees to

100 degrees, the energy required is the mass of the water (.095) times the change in temperature (100-0= 100) times

the specific heat for water (4186 J/kg*C). This is equal to 39767 J. The amount of energy required to raise the

calorimeter to 100 degrees is equal to the mass of the calorimeter (.446) times the specific heat of copper

(390J/kg*C) times the change in temperature (100-0=100). This equals 17,394 J. All of these added together gives

88,511 J. Now I need to see how this compares to the energy needed to condense the steam. This energy is equal to the

mass of the steam (.035) times the heat of vaporization (2.256*10^6) which equals 78,960 J. Because this energy is

less than the heat required to melt the ice, raise the temperature of the ice, and raise the temperature of the

calorimeter, you can see that the state of the system has to be a liquid.

Confidence 3

.............................................

Given Solution:

** Let Tf be the final temperature of the system.

The ice doesn't change temperature until it's melted. It melts at 0 Celsius, and is in the form of water as its

temperature rises from 0 C to Tf.

If all the ice melts, then the melting process requires .0950 kg * (3.3 * 10^5 J / kg) = 30 000 J of energy, very

approximately, from the rest of the system.

If all the steam condenses, it releases .0350 kg * 2.256 * 10^6 J / kg = 80 000 Joules of thermal energy, very

approximately, into the rest of the system.

We can conclude that all the ice melts. We aren't yet sure whether all the steam condenses.

If the temperature of all the melted ice increases to 100 C, the additional thermal energy required is (.0950 kg) *

(4186 J / (kg C) ) * 100 C = 40 000 Joules, very approximately.

The container is also initially at 0 C, so to raise it to 100 C would require .446 kg * (390 J / (kg C) ) * 100 C =

16 000 Joules of energy, very approximately.

Thus to melt the ice and raise the water and the container to 100 C would require about 30 000 J + 40 000 J + 16 000

Joules = 86 000 Joules of energy. The numbers are approximate but are calculated closely enough to determine that

the energy required to achieve this exceeds the energy available from condensing the steam. We conclude that all the

steam condenses, so that the system will come to equilibrium at a temperature which exceeds 0 C (since all the ice

melts) and is less than 100 C (since all the steam will condense).

We need to determine this temperature.

The system will then come to temperature Tf so its change in thermal energy after being condensing to water will be

4186 J / (kg K) * .035 kg * (Tf - 100 C).

The sum of all the thermal energy changes is zero, so we have the equation

m_ice * L_f + m_ice * c_water * (Tf - 0 C) + m_container * c_container * ( Tf - 0 C) - m_steam * L_v - + m_steam *

c_water * ( Tf - 100 C ) = 0.

The equation could be solved for T_f in terms of the symbols, but since we have already calculated many of these

quantities we will go ahead and substitute before solving:

[ 0.0950 kg * 3.3 * 10^5 J / kg ] + [0.0950 kg * 4186 J/kg*K *(Tf - 0 C)] + [.446 kg * 390 J/kg*K * (Tf - 0 C)] -

.0350 kg * 2.256 x 10^6 J/kg + 4186 J / (kg K) * .035 kg * (Tf - 100 C) = 0.

Noting that change in temperature of a Kelvin degree is identical to a change of a Celsius degree we get

170 J/C * Tf + 390 J/C * Tf - 79000 J - 14000 J + 31 000 J + 140 J / C * Tf = 0 or

700 J / C * Tf = 62 000 J, approx. or

Tf = 90 C (again very approximately)

Self-Critique: I didn't solve for Tf because the question asked for the state of the system. However, I read through

the steps of solving for the Tf and I understand them.

------------------------------------------------

Self-Critique Rating: 3

*********************************************

Question: query univ phy 17.98 / 17.100 (90 in 10th edition): C = 29.5 J/mol K + (8.2 + 10^-3 J/mol K^2) T .

How much energy is required to change the temperature of 3 moles from 27 C to 227 C?

YYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYY

Your Solution: The energy required is 21,363. Since the specific heat is dependent on temperature, I took the

integral of the equation given for the specific heat from the temperature 300 K (27 C) to 500 K (227 C) and

multiplied this by 3 moles.

confidence rating #$&*:

^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^

.............................................

Given Solution:

** In this case the specific heat is not constant but varies with temperature.

The energy required to raise the temperature of 3 moles by `dT degrees (where `dT is considered to be small enough

that the change in specific heat is insignificant) while at average temperature T is `dQ = 3 mol * C * dT = 3 mol *

(29.5 J/mol K + (8.2 * 10^-3 J/mol K^2) T) * `dT.

To get the energy required for the given large change in temperature (which does involve a significant change in

specific heat) we integrate this expression from T= 27 C to T = 227 C, i.e., from 300 K to 500 K.

An antiderivative of f(t) = (29.5 J/mol K + (8.2 + 10^-3 J/mol K^2) T) is F(T) = 29.5 J / (mol K) * T + (8.2 + 10^-3

J/mol K^2) * T^2 / 2. We simplify and apply the Fundamental Theorem of Calculus and obtain F(500 K) - F(300 K).

This result is then multiplied by the constant 3 moles.

The result for Kelvin temperatures is about 3 moles * (F(500 K) - F(300 K) = 20,000 Joules. **

Self-Critique: OK

------------------------------------------------

Self-Critique Rating: OK

*********************************************

Question: University Physics Problem 17.106 (10th edition 15.96): Steam at 100 Celsius is bubbled through a .150

kg calorimeter initially containing .340 kg of water at 15 Celsius. The system ends up with a mass of .525 kg at 71

Celsius. From these data, what do we conclude is the heat of fusion of water?

YYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYY

Your Solution: The specific heat of water is 2,156,798 J/kg. I found this by multiplying the required energy to

change the temperature of the water from 15 C to 71 C plus the energy required to bring the calorimeter from a

temperature of 15 C to 71 C. I set these calculations equal to the energy required to condense the steam plus the

energy required to bring the temperature of the steam to 71 C.

NOTE: I HAD TO LOOK AT THE SOLUTION TO FIND THE SPECIFIC HEAT FOR THE CALORIMETER. IN THE PROBLEM, IT DOES NOT

SPECIFY WHAT TYPE OF MATERIAL THE CALORIMETER IS MADE OUT OF. IT WOULD'VE BEEN VERY HELPFUL TO HAVE KNOWN THIS RATHER

THAN HAVING TO LOOK AT THE SOLUTION ONCE I REALIZED I HAD TWO UNKNOWNS (THE SPECIFIC HEAT OF THE CALORIMETER AND THE

HEAT OF VAPORIZATION OF THE WATER).

@&

The problem in the text stated the specific heats.

*@

@&

Statements of text problems in queries are very abbreviated and meant for reference rather than as a sole source of information.

*@

confidence rating #$&*:

^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^

.............................................

Given Solution:

**The final mass of the system is .525 kg, meaning that .525 kg - (.340 kg + .150 kg) = .035 kg of steam condensed

then cooled to 71 C.

The thermal energy change of the calorimeter plus the water is .150 kg * 420 J/(kg C) * 56 C + .34 kg * 4187 J / (kg

C) * 56 C = 83,250 J, approx.

The thermal energy change of the condensed water is -Hf * .035 kg + .035 kg * 4187 J / (kg C) * (-29 C) = -Hf * .035

kg - 2930 J, approx.

Net thermal energy change is zero, so we have

· 83,250 J - Hf * .035 kg - 4930 J = 0 which is easily solved to give us

· Hf = 79,000 J / (.035 kg) = 2,257,000 J / kg. **

------------------------------------------------

Self-Critique Rating: 3

*********************************************

Question: `q003. A container with negligible mass holds 500 grams of water, and 100 grams of ice and 800 grams of

a substance whose specific heat is 1800 Joules / (kilogram * Celsius), all at 0 Celsius. How much steam at 100

Celsius must be bubbled through the waterto raise the temperature of the system to 20 Celsius?

YYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYY

Your Solution: .043 kg of steam must be bubbled through. I calculated this by finding the energy required to melt the

ice, plus the energy required to raise the temperature of the melted ice, plus the energy required to raise the

temperature of the existing water, plus the energy required to raise the temperature of the calorimeter. I set these

values equal to the energy required to condense the steam plus the energy required to lower the temperature of the

steam. Once I did this, my only unknown was the mass of the steam. I solved and got .043. My equation looked like

this:

.1*3.3*10^5+.1*20*4186+.5*20*4186+.8*1800*20=x*2.256*10^6+x*4186*80

Note: x is the unknown value of the mass of the steam.

confidence rating #$&*:

^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^

------------------------------------------------

Self-Critique Rating:

*********************************************

Question: `q004. The specific heat of a certain substance increases linearly from 1200 Joules / (kg C) at 150 C

to 1400 Joules / (kg C) at 350 C. How much heat would be required to increase the temperature of a 5 kg sample from

200 C to 300 C?

Show how this problem could be solved without using an integral.

Show how this problem could be solved using an integral.

YYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYYY

Your Solution: The heat that would be required to increase the temperature of a 5 kg sample from 200 C to 300 C would be 650,000 J. I found this without using an integral by first by graphing the line that represents the change in specific heat. I did this by using my two points and the slope between them. Once I drew this, I calculated the specific heats at 200 C and at 300 C using the slope of the line (1). The two points I found were (200, 1250) and (300, 1350). I calculated the area under the line between those two points using a rectangle and a triangle. Once I found the area, I multiplied by 5 kg. To solve this problem using an integral I found the equation of the line and took the integral between the two temperatures (200 and 300). Then I multiplied this by 5 kg.

confidence rating #$&*:

^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^

@&

Good.

The linear function could also be symbolized and integrated:

The linear function between the two given data points is

c(T) = 1 (J / (kg C)) / C * (T - 150 C) + 1200 J / (kg C).

On a temperature increment `dT containing sample point T* the specific heat is c(T*) and the energy required to raise the temperature of mass m is

`dQ = c(T*) * m * `dT.

The Riemann sum of these contributions on temperature interval T_0 <= T <= T_f thus approaches the limiting integral

integral ( c(T) * m dT, T from T_0 to T_f )

In this case we obtain the integral

integral ( (1 (J / (Kg C)) / C * (T -150 C) + 1200 J / (kg C) ) * 5 kg * dT, T from T_0 to T_f)

Integrating this expression from T_0 = 200 C to T_F = 300 C yields the same result, 650 000 J.

*@

------------------------------------------------

Self-Critique Rating:

"

Self-critique (if necessary):

------------------------------------------------

Self-critique rating:

"

Self-critique (if necessary):

------------------------------------------------

Self-critique rating:

#*&!

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