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12.E: Thermodynamic Processes (Exercises)

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  • These are homework exercises to accompany the Textmap created for "Principles of Modern Chemistry" by Oxtoby et al. Complementary General Chemistry question banks can be found for other Textmaps and can be accessed here.


    A sample of \(\ce{O_2}\) gas is under an external pressure of 17 atm and contained in a cylinder with a volume of 50 L. The gas is cooled and the resulting volume is 25 L. Calculate the amount of work done on the \(\ce{O_2}\) gas.


    \[\begin{align*} w &=-P\Delta V \nonumber \\[5pt] &= -P_{ext}(V_2-V_1) \\[5pt] &=-17atm\ (25\,L-50\,L)=425\, L\ atm \\[5pt] &=425\ atm\ L\ (101.325\dfrac{J}{atm\ L}) \\[5pt] &= 43, 063\,J \\[5pt] & =43.06\, kJ \end{align*} \nonumber \]


    A system containing oxygen gas is heated at a constant pressure of 40.0 atm so that its volume increases 177 L to 458 L. Express the amount of work that the system did in kilo-joules.


    The formula for work from the expansion of a gas at constant pressure

    \[w=-P_{ext} \Delta V\nonumber \]

    \[w=-40\; atm \times (458\; L - 177\; L) = -11240\; L\; atm \nonumber \]

    Convert from L atm to joules

    \[-11240 \; L\; atm \times 101.325\; \dfrac{J}{L\ atm} = -1138893\; J \nonumber \]

    Convert from J to kJ and round to get the final answer

    \[ -1138893\; J \times \dfrac{1\; kJ}{1000\; J}=-1140\; kJ \nonumber \]

    \[w=-1140\; kJ \nonumber \]


    The gas mixture inside one of the cylinders of an airplane expands against a constant external pressure of 5.00 atm because of the growing altitude, from an initial volume of 500 mL (at the end of the compression stroke) to the final volume of 1200 mL. Calculate the work done on the gas mixture during this process and express it in Joules.


    $$w = -(5.00\ atm) (1200\ mL - 500\ mL) (\dfrac{1\ L}{1000mL}) (101.3 \dfrac{J}{L\times atm})= -354.55 J\]


    The following events are based on a true story. A butcher for the local Chinese restaurant needs to defrost a large chunk of beef, which weights \(50\,lb\) and is currently at \(0^{\circ}C\). He wants to accomplish this by is going out onto the street and repeatedly drop it onto the ground. Suppose the potential energy of the meat completely transforms into heat each time it hits the ground, and that energy can be calculated from

    \[V = mg\Delta{h}\nonumber \]

    where m is mass of the object, g is the acceleration of gravity, and Δh is change in height. If the man is \(5\,ft\) tall and he wants to get the meat to room temperature (\(25^{\circ}C\)), how many times does he have to drop the piece of meat? Assume the environment has no effect on the meat, and that it does not lose any heat. (Specific Heat of the Meat: \(0.25\dfrac{J}{g^{\circ}C}\)).


    There are two steps to solve this equation. First, to find the amount of heat absorbed by the meat from one drop. Second, to find the total amount of heat needed to warm the meat up from \(0^{\circ}\) to \(25^{\circ}C\).

    To find the total amount of heat required to bring the meat from \(0^{\circ}\) to \(25^{\circ}C\), the equation for calculating heat has to be used:

    \(Q = mC_{p}\Delta{T}\)

    The mass of the meat can be calculated via conversion from \(lb\) to \(g\), and is as follows:

    \(50lb\times{453.592\dfrac{g}{lb}} = 22679.6g\)

    The change in temperature is just the final temperature minus the initial, so it is just \(25^{\circ}C\).

    Lastly, \(C_{p}\) is given. Plugging in all of these values gives:

    \[Q = 22679.6g\times{0.25\dfrac{J}{g^{\circ}C}}\times{25^{\circ}C} = 141747.5 J\nonumber \]

    Thus, \(141747.5 J\) is the total amount of heat needed to heat up the meat to \(25^{\circ}C\).

    Now to find the amount of heat transferred into the meat from one drop. This utilizes the potential energy equation. The question mentions how to calculate the potential energy, and all potential energy is translated into heat. Therefore.

    \[Q= V= mg\Delta{h}\nonumber \]

    The problem gives the mass, the acceleration of gravity is \(9.8\dfrac{m}{s^2}\), and height. Therefore, since the potential energy for one drop is equal to the heat for one drop, the heat can be calculated as such:

    \[Q= 22.6796kg\times9.8\dfrac{m}{s^2}\times{1.524m}= 338.724\dfrac{kg\;m^2}{s^2} = 338.724 J\nonumber \]

    From there, since no heat is lost, it carries over for each drop. Therefore, the number of times he needs to drop the meat is found by simple division:

    \[141747.5 J\div{338.724 J}= 418.474 drops\nonumber \]

    Thus, the drops needed is around 419.

    Abstract: Calculate heat from \(Q = mC_{p}\Delta{T}\) and \(Q= V= mg\Delta{h}\). Divide the two.


    Suppose you have a ball \((C_p= 0.85\dfrac{J}{g^oC})\) at 25°C, what will its final temperature be if the amount of work equal to dropping it down from a height of 86.6m is done to it ? \((g=9.81\dfrac{m}{s^2})\)


    \[\begin{align} U &=mg\Delta h \\[5pt] &=m_{ball}\cdot 86.6m\cdot 9.81\dfrac{m}{s^{2}}\\[5pt] &=850m_{ball} \end{align} \nonumber \]

    If we assuming all the kinetic energy at the time of collision converts to heat, then

    \[\begin{align} \Delta T &=\dfrac{q}{Cp\cdot m_{ball}}\\[5pt] &=\dfrac{U}{C_p\cdot m_{ball}} \\[5pt] &= \dfrac{850 m_{ball}}{85\dfrac{J}{g^oC} \cdot m_{ball}} \dfrac{1\,kg}{1,000\,g} \\[5pt] &= 1.0^{\circ}C \end{align} \nonumber \]

    \[\begin{align} T_{final} &=25^{\circ}C+1^{\circ}C\\[5pt] &=26^{\circ}C \end{align} \nonumber \]


    The rule of Dulong and Petit shows that the molar heat capacities of most metallic elements group around a certain value “X” \(\dfrac{J}{K\ mol}\) at 25oC. By first calculating and showing the molar heat capacities of metals rhenium, silver, lead, tungsten, copper, molybdenum and hafnium (given that the respective specific heat capacities of these metals are 0.14\(\dfrac{J}{K\ g}\), 0.23\(\dfrac{J}{K\ g}\), 0.13\(\dfrac{J}{K\ g}\), 0.13\(\dfrac{J}{K\ g}\), 0.39\(\dfrac{J}{K\ g}\), 0.25\(\dfrac{J}{K\ g}\) and 0.14\(\dfrac{J}{K\ g}\) ), find the value of “X”. (hint: take the average value of the calculated molar heat capacities and round off value to nearest whole number).


    To first find the molar heat capacities of each metal, multiply the molar mass of each metal by their specific heat capacities:

    Molar heat capacity of:

    \(Re= 0.14\dfrac{J}{K\ g}\times186.207\dfrac{g}{mol}= 26.068\dfrac{J}{K\ mol}\) \(Ag= 0.23\dfrac{J}{K\ g}\times 107.868\dfrac{g}{mol}=24.809\dfrac{J}{K\ mol}\) \(Pb= 0.13\dfrac{J}{K\ g}\times 207.2\dfrac{g}{mol}= 26.936\dfrac{J}{K\ mol}\)

    calculate the average molar heat capacity:

    Average molar heat capacity=\(\dfrac{(26.068\dfrac{J}{K\ mol} + 24.809\dfrac{J}{K\ mol} + 26.936\dfrac{J}{K\ mol} + 23.899\dfrac{J}{K\ mol} + 24.7829\dfrac{J}{K\ mol} + 23.99\dfrac{J}{K\ mol} + 24.988\dfrac{J}{K\ mol})}{7}=25.068\dfrac{J}{K\ mol}\)

    \(W= 0.13\dfrac{J}{K\ g}\times 183.84\dfrac{g}{mol}=23.899\dfrac{J}{K\ mol}\)
    \(Cu= 0.39\dfrac{J}{K\ g}\times 63.546\dfrac{g}{mol}=24.7829\dfrac{J}{K\ mol}\)
    \(Mo=0.25\dfrac{J}{K\ g}\times 95.96\dfrac{g}{mol}= 23.99\dfrac{J}{K\ mol}\)
    \(Hf= 0.14\dfrac{J}{K\ g}\times 178.49\dfrac{g}{mol}=24.988\dfrac{J}{K\ mol}\)


    The specific heat capacities of metals aluminum, bismuth, copper, lead, and silver at 25°C are 0.900, 0.123, 0.386, 0.128, and 0.233\(\dfrac{J}{g\ K}\). Calculate the molar heat capacities of these metals. According to the rule of Dulong and Petit, the molar heat capacities of metallic elements, like these, are approximately 25\(\dfrac{J}{K\ mol}\).


    Multiply each of the specific heat capacities by its corresponding molar mass to obtain their molar heat capacities.


    \[0.900 \dfrac{J}{g\ K}\times 26.98 \dfrac{g}{mol} = 24.3 \dfrac{J}{mol\ K}\nonumber \]


    \[0.123 \dfrac{J}{g\ K}\times 208.98 \dfrac{g}{mol} = 25.7 \dfrac{J}{mol\ K}\nonumber \]


    \[0.386 \dfrac{J}{g\ K}\times 63.55 \dfrac{g}{mol} =24.5 \dfrac{J}{mol\ K}\nonumber \]


    \[0.128 \dfrac{J}{g\ K}\times 207.2 \dfrac{g}{mol} =26.5 \dfrac{J}{mol\ K}\nonumber \]


    \[0.223 \dfrac{J}{g\ K}\times 107.87 \dfrac{g}{mol} =25.1 \dfrac{J}{mol\ K}\nonumber \]


    An undisclosed volume of water is tightly sealed in a microwave-safe container at room temperature before it is placed in an ice bath where it is cooled by a student.

    1. During the cooling process within the ice bath, state whether (\(\Delta U\)), Q, and W of the system are negative, zero, or positive. Explain your reasoning.
    2. After being cooled, the student decides that the water seems too cold so it is placed in the microwave where the container of water is heated back to room temperature. What are the new signs of (\(\Delta U\)), Q, and W during the heating process? Explain your reasoning.
    3. Now determine the signs of ( (\(\Delta U\))1 + (\(\Delta U\))2 ), (Q1 + Q2) , and (W1 + W2), where possible, assuming that the cooling process was step 1 and the heating process was step 2.
    1. W is zero, Q is negative, and (\(\Delta U\)) is negative. Work is zero for this step because neither volume nor pressure of the container is changing. Since the water is cooler than before heat has left the system so it is negative; and because (\(\Delta U\)) = Q + W and W = 0 then (\(\Delta U\)) = Q which is negative so, (\(\Delta U\)) is negative.
    2. W is zero, Q is positive, and (\(\Delta U\)) is positive. Work is zero for this step because neither volume nor pressure of the container is changing. Since the water is hotter than before heat has entered the system so it is positive and because (\(\Delta U\)) = Q + W and W = 0 then (\(\Delta U\)) = Q which is positive so, (\(\Delta U\)) is positive.
    3. Since W was equal to zero for both processes above (W1 + W2) is equal to zero. ( (\(\Delta U\))1 + (\(\Delta U\))2 ) = (Q1 + Q2) where they are both equal to zero.

    If the water is cooled from room temperature to a lower temperature and then heated directly back to room temperature, wouldn't ( (\(\Delta U\))1 + (\(\Delta U\))2 ) be 0? Q is the only factor actually changing here and q(heating to cooling) = -q(cooling to heating) provided the change in t is the same. So both ( (\(\Delta U\))1 + (\(\Delta U\))2 ) and q should be 0.


    Your lab partner slipped a sample of unknown hot metal that is 40.0g, which is initially at 130.0°C into a 100.0 g water that is initially at 50.0°C. A temperature probe indicates that equilibrium is reached at 60.15°C. Using the specific heat capacity of water 4.18\(\dfrac{J}{K}\), calculate the specific heat capacity of the unknown metal.


    Imagine two sub-systems: the metal and the water. If mixing the hot metal and cool water inside a well-insulated container (that prevent leaks of heat), then the heat absorbed by the system will equal zero. Since the system is the sum of the two sub-systems:

    \[q_{sys}=0=q_{metal}+q_{water}\nonumber \]

    For both sub-systems, the amount of heat gained is equal to the specific heat capacity times the mass times the temperature change:

    \[q_{metal}+ q_{water }= m_{water}C_{s,water}\Delta\;T_{metal}\ = 0\nonumber \]

    Solving for the specific heat capacity of the metal:

    \[c_{s,metal}=\dfrac{-m_{water}c_{s,water}\Delta\;T_{water}}{m_{metal}\Delta \;T_{metal}}=\dfrac{-100.0\;g\times4.18\dfrac{J}{K\ g}\times10.15^{\circ}C}{40.0\;g\times-69.85^{\circ}C}=1.52\dfrac{J}{K\ g}\nonumber \]

    Tip: Do not convert Celsius to Kelvin. The Kelvin and Celsius scales differ only in their location of their zero points. Temperature change in Celsius is the same temperature change of Kelvin.


    Let's say you 34.5 grams of some hot metal that is initially at 75°C and you put that metal into 64.0 grams of water that is initially at 25°C. If the the two objects reach thermal equilibrium at 39°C, what is the specific heat capacity of the metal when the specific heat capacity of water is \(4.18 \dfrac {J}{K\ g}\).


    The formula used to solve this question is \[m_1c_1 \Delta T_1 = -m_2c_2 \Delta T_2\nonumber \]

    Plug in your known values and solve for \(c_1\)

    \((34.15 \; g)(c_1)(36°C) = -(64 \; g)(4.18 \; \dfrac {J}{K\ g})(-14°C)\)

    \(c_1 = 3.02 \; \dfrac {J}{K\ g}\)


    A 10.00 g sample of Aluminum at 60.0 °C and a 30.0 g sample of copper at a temperature of -20.0 °C were thrown simultaneously into a 50.0 g of water at a temperature of 25.0 °C. What will be the final temperature of the system consisting of the two metal samples and the water? Assuming that this system is completely isolated from the surroundings. Use the information below for your calculations.

    • \(c_{s(Al)}=0.900 J/(K•g)\)
    • \(c_{s(Cu)}=0.385 J/(K•g)\)
    • \(c_{s(H_2 O)}=4.184 J/(K•g)\)

    Since our system is isolated, the thermal energy lost by one component is transferred to the other components.

    \[q_1=-q_2\nonumber \]

    which is equivalent to

    \[C_1 ∆T=-C_2 ∆T\nonumber \]

    Noting that

    \[C=m C_s\nonumber \]

    To avoid the complexity of handling three components, we can utilize the fact that temperature is a state function; we will simplify our calculations by choosing a different path to arrive to our final state.

    We can do this in two steps:

    Ignore the Aluminum sample and treat the copper and water as the only components of our system. After finding the equilibrium temperature, we add the Aluminum sample to the water and copper system, thereby reaching the same final state.

    Which is the same answer we got before. This should make intuitive sense because regardless of the path we take, we end up with the exact same amount of thermal energy in our system.

    Step 1

    \[m_{Cu}×C_{s(Cu)}×(T_f-T_{i(Cu)})=-m_{H_2O}C_{s(H_2 O)}(T_f-T_{i(H_2 O)})\nonumber \]

    \[30.0\,g×0.385\, J/(°C•g)×(T_f+20 °C)=-50.0\,g × 4.184 \,J/(°C•g)×(T_f-25.0 °C)\nonumber \]

    Solving for \(T_f\) for the copper and water system gives us

    \[T_f=22.6 °C\nonumber \]

    Step 2

    \[C_{(Cu+H_2 O)}×(T_f-T_{i(Cu+H_2 O)})=-m_{Al}×C_{s(Al)}×(T_f-T_{i(Al)})\nonumber \]

    Noting that

    \[C_{(Cu+H_2 O)}=m_{H_2O}×C_{s(H_2 O)}+m_{Cu}×C_{s(Cu)}\nonumber \]

    Combining the two equations and plugging the values gives us

    \[[(30.0\,g×0.385 \,J/(°C•g))+(50.0\,g × 4.184 \,J/(°C•g))]×(T_f-22.6 °C)= -10.0\,g×0.900\, J/(K•g)×(T_f-60 °C)\nonumber \]

    Solving for \(T_f\):

    \[T_f=24.1°C\nonumber \]

    Which is the final temperature of the whole system.

    Alternative Approach

    We can also choose a path where we add the Aluminum first, and then we add the copper. Again, temperature is a state function and choosing a different path will not affect the final answer. We also show the calculation for this path for the sake of completion.

    Step 1

    \[m_{Cu}×C_{s(Al)}×(T_f-T_{i(Al)})=-m_{(H_2 O)}×C_{s(H_2 O)}×(T_f-T_{i(H_2 O)})\nonumber \]

    \[10.0\,g×0.900\, J/(°C•g)×(T_f+20 °C)=-50.0\,g × 4.184 \,J/(°C•g)×(T_f-25.0 °C)\nonumber \]

    Solving for \(T_f\) for the aluminum and water system gives us

    \[T_f=26.4 °C\nonumber \]

    Step 2

    \[[(m_{(H_2 O)}×C_{s(H_2O)})+(m_{Al}×C_{s(Al)}) )]×(T_f-T_{i(Al+H_2 O)})=-m_{Al}×C_{s(Cu)}×(T_f-T_{i(Cu)})\nonumber \]

    Plugging the numbers,

    \[[(10.0\,g×0.900\, J/(°C•g))+(50.0\,g × 4.184 \,J/(°C•g)]×(T_f-26.4 °C)=-30.0\,g×0.385 \,J/(K•g)×(T_f+20 °C)\nonumber \]

    Solving for \(T_f\)

    \[T_f=24.1°C\nonumber \]


    Calculated the heat required to melt 3.00 g of ice and the heat required to change the temperature of water from 0°C to 100°C. What is the proportionality of the heat necessary to melt ice compared to the heat required to change the temperature of water from 0°C to 100°C? Use values from Table S2 and assume \(\Delta H_{f}\) =334 J g-1 for calculations? Why is the heat positive instead of negative?


    First lets determine the amount of heat needed to melt ice:

    \(q = m\Delta H_{f}\)

    \(q = 1,002\ J\)

    Next lets determine the heat required to raise the temperature of water 100°C:

    \(q = mC_s \Delta{T}\)

    \(q = 1,254\ J\)

    So the proportionality was determined to be 4:5

    The heat is positive because the heat is required. The heat is needed to make the states go from solid to liquid when melting and then liquid to gas when the temperature is raised from 0 to 100 degrees Celsius.


    An observation in the 18th century stated that the heat that raised a certain mass of water from its freezing point to boiling point is equal to four-thirds of the heat required to melt the same mass of ice. Using the theory behind the observation, estimate the heat required to melt 10 g of ice, know that the heat capacity of water is 4.18J/oC.


    Let the heat required to raise the temperature of water from its freezing point to its boiling point is \(q_1\):

    $$q=mc\Delta T\]

    $$m = mass\]

    $$c = 4.18\dfrac{J}{g\ ^{o}C}\]

    $$\Delta T = freezing\ point - boiling\ point = 100-0=100^{o}C\]

    $$q_{1}=(10g)(4.18\dfrac{J}{g\ ^{o}C})(100^{o}C)\]

    $$q_{1} = 4180J = 4.18 KJ\]

    Let the heat required to melt 10g of ice is q2:





    For his birthday, his John's parents have given him a compressible oven filled with 0.250 mol argon. If he sets this compressible oven at 1.00 atm and 273 K and let it contract from a constant external pressure of 0.100 atm until the gas pressure reaches 10.00 atm and the temperature reaches 400 K, what is the work done on the gas, the internal energy change, and the heat absorbed by the gas?


    Using the ideal gas law \(PV=nRT\), we can see that:

    \[V_o = \dfrac{n\ R\ T_o}{P_o}\nonumber \]

    \[V_f = \dfrac{n\ R\ T_f}{P_f}\nonumber \]

    **n = 0.25 mol, R = 0.082\(\dfrac{atm\ L}{mol\ K}\) Po = 1 atm, Pf = 10 atm To= 273K Tf = 400K**

    where \(V_o\) and \(V_f\) represent the initial and final volume of the chamber. Now, the pressure clearly changes inside the chamber, but outside the chamber, the pressure is held constant, so from the perspective of the surroundings:

    \[W= -P(V_f - V_o)\nonumber \]

    where \(P\) represents the constant external pressure. Now substituting in Vf and Vo we can see that we've solved for work. Now, for any thermodynamic process:

    \[\Delta{U}= \dfrac{3}{2} n\ R(T_f - T_o)\nonumber \]

    So plugging in those values allows us to solve for ∆U. Now, for heat, we simply subtract W from ∆U, by the first law of thermodynamics.

    **First law of thermodynamics: the total energy of an isolated system is a constant, energy can be transformed from one form to another, but it can not be created or destroyed.**


    Take 4 moles of ideal, monatomic gas going through expansion processes. The gas was initially put at a pressure of 5.00 atm and a temperature of 30°C. The gas first goes through isothermal expansion until the volume doubled. An isochoric process follows as the pressure is halved. \(C_v = \dfrac{3}{2}R\)

    1. Build \(\Delta U\), W, and Q table for each process.
    2. Find the final temperature.

    Isothermal Process:

    \[\Delta U = 0\]

    $$W = Q\]

    $$W = nRT\ln \left( \dfrac{V_f}{V_i} \right) =(4\,mol)(8.314\,J.K^{-1} \cdot mol^{-1})(303.15\, K) \ ln (2)=6988\, J = Q\]

    Isochoric Process

    $$W = 0\]

    $$\Delta U = Q\]

    First find the initial pressure of this process.

    Use ideal law to relate pressure to volume. PV=nRT, in which P is inversely proportional to V.

    Thus, when volume is doubled, pressure is halved so \(P_f = 2.50 \,atm\). Now, find the final temperature of this process.

    Once again, relate P to T using ideal gas law. T is found to be directly proportional to P. Thus, if the pressure is halved from 2.50 atm, the temperature must also be halved from 303.15K.

    \(\dfrac{1}{2}(303.15K) = 151.58K\)

    \[Q= nC_v\Delta T=(4.00mol)(\dfrac{3}{2})(8.314\dfrac{J}{K\ mol})(-151.58K)=-7561J = \Delta U\]

    Processes ΔU Q W
    Isothermal 0 6988J 6988J
    Isochoric -7561J -7561J 0


    An apparatus is set up such that an ideal gas is released into vacuum by opening a stopcock, hence allowing it to freely expand (i.e., no external force is applied). Calculate \(\Delta{U}\) of the system, and prove that the free expansion process is adiabatic i.e no heat transfer.


    $$\Delta U = \dfrac{3}{2}nR\Delta T$$

    As the expansion is isothermal, i.e. it occurs without a change in temperature:

    $$\Delta T = 0$$


    $$\Delta U = 0$$


    $$\Delta U = q_p+w$$

    As the external force applied on the gas is zero, the work done by the gas is zero.


    $$0 = q_p + 0$$

    $$q_p = 0$$

    This proves that the process is adiabatic.


    A 150-L vessel contains 8.00 moles of neon at 270 K is compressed adiabatically, so that there is no gain nor loss of any heat, and irreversibly until the final temperature is 470 K. Calculate the change in internal energy, the heat added to the gas, and the work done on the gas.


    Since Ne is a monatomic ideal gas and the volume of the vessel remains constant, the heat capacity of \(Ne\) can be expressed as:

    $$C_{p} = \dfrac{3}{2} \times R = \dfrac{3}{2} \times 8.314 \dfrac{J}{K \cdot mol} = 12.47 \dfrac{J}{K \cdot mol} \]

    $$\Delta U = nC_{p} \Delta T\]

    $$\Delta U = 8.00 \times 12.47 \dfrac{J}{K \cdot mol} \times (470-2700) \; K = 19952 \; J = 20.0 \; kJ\]

    Since the vessel is adiabatically compressed, no heat is added, therefore \(q = 0\)

    $$\Delta U = q + w \]

    $$20.0 \; kJ = 0 + w \]

    $$w = 20.0 \; kJ\]


    A gas expands at constant external pressure of 3.00 atm until its volume has increased by 9.00 to 15.00 L. During this process, it absorbs 800J of heat from the surroundings.

    1. Calculate the energy change of the gas, \(\Delta U\)
    2. Calculate the work, w, done on the gas in an irreversible adiabatic (q = 0) process connecting the same initial and final state.

    a) $$\Delta U = q+w\]

    \[\Delta U= 800J + -((3.00 atm)(15.00 L - 9.00 L) (101.3 \dfrac{J}{L\ atm})) =-1023.4 J\]

    b) $$q=0\]

    \[\Delta U = w\]

    $$\Delta U= -((3.00 atm)(15.00 L - 9.00 L) (101.3 \dfrac{J}{L\ atm}))= -1823.4 J\]


    Using the theorem of equipartition of energy, calculate the specific heat capacity at constant pressure \(C_p\) at 25ºC and 1 atm for \(O_2\) and \(CO\). Compare the calculated values to the experimental data \((O_2=29.36, CO=29.1)\) and thus calculate the percent of the experimental value that results from vibrational motions. Answer: The percent of \(C_p\) due to vibrational motions is 0.897% for \(O_2\) and 0.141% for \(CO\).


    The equipartition theorem states that each degree of freedom in a molecule contributes to ½ RT to the molar internal energy of a gas. To solve this problem, the number of degrees of freedom \(DOF\) in each molecule must be identifies.

    \(O_2\) is a linear diatomic particle, thus it has 3 translational degrees of freedom and 2 rotational degrees of freedom. Since \(CO\) is a linear molecule it also has 3 translational and 2 rotational degrees of freedom. The molecules are at room temperature. Thus, it is assumed that there is no vibration in the bond (other than the zero point energy).

    The low percentage of \(C_p\) due to vibrational modes in both molecules indicates that the vibrational motion is extreamly small and can be neglected.

    \[DOF({O_2}) = {f_t} + {f_r} = 3 + 2 = 5\nonumber \]

    \[DOF(CO) = {f_t} + {f_r} = 3 + 2 = 5\nonumber \]

    Using the equation

    \[U = \left( DOF\right) \cdot \left( \dfrac{1}{2}RT \right)\nonumber \]

    find the internal energy of each gaseous molecule.

    \[U \left( O_2 \right) = \left( 5 \right) \cdot \left( \dfrac{1}{2}RT \right)\nonumber \]

    Since \(O_2\) and \(CO\) have the same degrees of freedom,

    \[U\left( O_2 \right) = U\left( CO \right) = \dfrac{5}{2}RT\nonumber \]

    The internal energy is related to \(C_v\) by

    \[C_v= \left( \dfrac{\partial U}{\partial T} \right) = \left( \dfrac{\partial \dfrac{5}{2}RT}{\partial T} \right) = \dfrac{5}{2}R\nonumber \]

    \(C_v\) is related to \(C_p\) by

    \[C_p = C_v + R = \dfrac{5}{2}R + R = \dfrac{7}{2}R = \dfrac{7}{2} \times 8.314 \dfrac{J}{mol\ K} = 29.099\dfrac{J}{mol\ K}\nonumber \]

    The percent of the experimental value that results from vibration motion is the difference between calculated and experimental value as a percentage of the experimental value.

    \[\% vibrational\,motion(O_2) = \dfrac{ experimental\,value - calculated\,value}{ experimental\,value} \times 100 = \dfrac{ 29.36 - 29.099 }{29.099} \times 100 = 0.897\% \nonumber \]

    \[\% vibrational\,motion (CO) = \dfrac{experimental\,value - calculated\,value}{experimental\,value} \times 100 = \dfrac{ 29.14 - 29.099}{ 29.099} \times 100 = 0.141\% \nonumber \]


    Using the classical equipartition theorem, calculate the value of \(C_p\) at 298K and 1atm for \(HF_{(g)}\) and \(F_{2(g)}\), assuming that their pressure is constant. Then compare your calculation with the experiment values of \(29.13\dfrac{J}{K\ mol}\) and \(31.30\dfrac{J}{K\ mol}\)respectively. What is the per cent of the measured value that arises from vibrational motions?


    Diatomic molecules possess a total of 6 degrees of freedom:

    • 3 degrees in translational motion
    • 2 degrees in rotational motion
    • 1 degree in their vibrational motions

    $$6.11\ for\ F_{2(g)} = 0.735R\]

    The differences are due to the fact that some quantized energy levels are not available at certain temperatures, in this case room temperature. This means that \(HF_{(g)}\) contributed only 0.004R of its experimental value of \(29.13\dfrac{J}{K\ mol}\) to the vibrational degree of freedom, which is 0.014%. \(F_ {2(g)}\) contributed 0.265R of its experimental value \(31.30\dfrac{J}{K\ mol}\), which is 0.847%.

    Each translational and rotational degree of freedom contributes \(\dfrac{R}{2}\) to the heat capacity of a gas, while each vibrational degree of freedom contributes \(\dfrac{2R}{2}\) (=R). Therefore the predicted heat capacity \((C_v)\) at a constant volume is:

    $$C_v = 3\times (\dfrac{R}{2}) + 2\times (\dfrac{R}{2}) + 1\times (\dfrac{2R}{2}) = 7(\dfrac{R}{2})$$

    Since the question is asking for the heat capacity of these gases that are under a constant pressure, the result is multiplied by an additional \(\dfrac{2R}{2}\) because the volume can change in order to keep the pressure constant. Therefore:

    $$C_v= (\dfrac{2R}{2})+(\dfrac{7R}{2}) = \dfrac{9R}{2}$$

    $$R = 8.3145\dfrac{J}{K\ mol}$$

    $$C_p=\dfrac{9(8.3145\dfrac{J}{K\ mol})}{2}=37.41\dfrac{J}{K\ mol}$$

    This is the calculated value for both of the two gases. Since the experiment values were \(29.13\dfrac{J}{K\ mol}\) for \(HF_{(g)}\) and \(31.30\dfrac{J}{K\ mol}\) for \(F_{2(g)}\), the differences between the calculations were:

    $$8.28\ for\ HF_{(g)} = 0.996R$$


    1. Calculate the change of enthalpy when a 69-grams sample of zinc is heated from 753 K to 927 K at a constant pressure of 1 atm.
    2. Calculate the change of enthalpy when 3 moles of butane are heated from 204 K to 258 K at a constant pressure of 1 atm.


    \(q=mC_s\Delta T\)

    \(m=69\ g\)

    \(\Delta T=927-753=174\ K\)

    \(C_{s(zinc)}=0.39\dfrac{J}{g\ ^oC}\)

    \(q=69\times 0.39\times 174=4682.34\ J=4.56\ kJ\)


    \(q=nC_p\Delta T\)


    \(\Delta T=258-204=54\ K\)


    \(q=3\times 132.42\times 54=21452.04\ J= 21.4504\ kJ\)


    What is the change in enthalpy when 8.19 grams of ethane (\(\ce{C_2H_6}\)) vaporizes, assuming a normal boiling point and \(\ce{\Delta H_{vap}}= 14.72\ \dfrac{kJ}{mol}\).


    First, convert grams of ethane to moles:

    \[(8.19\; \cancel{g\; C­_{2}H_{6}}) \left(\dfrac{1\: mol}{30.07\: \cancel{g\; C­_{2}H_{6}}} \right) = 0.272\; mol\nonumber \]

    This step is to match quantity units of ethane to those in the given value of \(\ce{\Delta H_{vap}}\).

    Then, given the \(\ce{\Delta H_{vap}}\),

    \[(0.272\; \cancel{mol \;C­_{2}H_{6}} ) \left (\dfrac{14.72\: kJ}{1\: \cancel{mol\; C­_{3}H_{8}}} \right ) = 4.004\; kJ\nonumber \]

    \(\ce{\Delta H}=4.004\; kJ\)

    This value is the change in enthalpy, or thermodynamic energy, when the specified amount of ethane undergoes the above reaction.


    The heat capacity \(C_p\) of ice is \(38\dfrac{J}{K\ mol}\) and \(C_p\) of water is \(75\dfrac{J}{K\ mol}\). A 24.0 g ice cube at -15 oC is placed into 120g of water at room temperature (25oC). What is the temperature of the water when it reaches equilibrium?


    \[q_{ice} = -q_{water}\]


    \[\left(\dfrac{24g\ ice}{18.02\dfrac{g}{mol}}\right)\times (38\dfrac{J}{K\ mol})\times (T_f - (-15^oC)) = -\left(\dfrac{120g\ water}{18.02\dfrac{g}{mol}}\right)\times (75\dfrac{J}{K\ mol})\times (T_f - 25^oC)\]



    Determine the change in enthalpy \(\left(\ce{\Delta}{H}\right)\) for the following chemical reaction

    \(\ce{4NH_{3(g)} + 5O_{2(g)} \rightleftharpoons 4NO_{(g)} + 6H_2O_{(g)}}\)

    given that:

    \(\ce{O_{2(g)} + N_{2(g)} \rightleftharpoons 2NO_{(g)}}\) \(\ce{\Delta}{H}\) = \(+180.5\ \dfrac{kJ}{mol}\)

    \(\ce{2H_2O_{(g)} \rightleftharpoons 2H_{2\, (g)} + O_{2\, (g)}}\) \(\ce{\Delta}{H}\) = \(+483.64\ \dfrac{kJ}{mol}\)

    \(\ce{3H_{2(g)} + N_{2(g)} \rightleftharpoons 2NH_{3(g)}}\) \(\ce{\Delta}{H}\) = \(-92.22\ \dfrac{kJ}{mol}\).


    Using Hess's Law, we can obtain the \(\ce{\Delta}{H}\) for

    \(\ce{4NH_{3(g)} + 5O_{2(g)} \rightleftharpoons 4NO_{(g)} + 6H_2O_{(g)}}\)

    by adding and modifying the other equations provided until they resemble the equation above.

    \(\ce \left( {O_{2(g)} + N_{2(g)} \rightleftharpoons 2NO_{(g)}} \right) \times \left( 2 \right) \) \(\ce{\Delta}{H}\) = \(+180.5\ \dfrac{kJ}{mol} \times \left( 2 \right) \)

    \(\ce \left( {2H_2O_{(g)} \rightleftharpoons 2H_{2\, (g)} + O_{2\, (g)}} \right) \times \left( -3 \right) \) \(\ce{\Delta}{H}\) = \(+483.64\ \dfrac{kJ}{mol} \left( -3 \right) \)

    \(\ce \left( {3H_{2(g)} + N_{2(g)} \rightleftharpoons 2NH_{3(g)}} \right) \times \left(-2 \right) \) \(\ce{\Delta}{H}\) = \(-92.22\ \dfrac{kJ}{mol} \times \left(-2 \right) \)

    The above modifications simplify out to

    \(\ce {2O_{2(g)} + 2N_{2(g)} \rightleftharpoons 4NO_{(g)}} \) \(\ce{\Delta}{H}\) = \(+361.0\ \dfrac{kJ}{mol} \)

    \(\ce {6H_{2\, (g)} + 3O_{2\, (g)} \rightleftharpoons 6H_2O_{(g)}} \) \(\ce{\Delta}{H}\) = \(-1450.92\ \dfrac{kJ}{mol} \)

    \(\ce {4NH_{3\, (g)} \rightleftharpoons 6H_{2\, (g)} + 2N_{2\, (g)}} \) \(\ce{\Delta}{H}\) = \(184.4\ \dfrac{kJ}{mol} \)

    Species that are common to both sides can be cancelled out.

    \(\ce { 2O_{2(g)} + \require{cancel} \cancel{2N_{2(g)}} \rightleftharpoons 4NO_{(g)}} \) \(\ce{\Delta}{H}\) = \(+361.0\ \dfrac{kJ}{mol} \)

    \(\ce { \require{cancel} \cancel{6H_{2\, (g)}} + 3O_{2\, (g)} \rightleftharpoons 6H_2O_{(g)}} \) \(\ce{\Delta}{H}\) = \(-1450.92\ \dfrac{kJ}{mol} \)

    \(\ce { 4NH_{3\, (g)} \rightleftharpoons \require{cancel} \cancel{6H_{2\, (g)}} + \cancel{2N_{2\, (g)}}} \) \(\ce{\Delta}{H}\) = \(184.4\ \dfrac{kJ}{mol} \)

    Finally, after adding the remaining specimens and the enthalpy change that occurs with them we have:

    \(\ce{4NH_{3(g)} + 5O_{2(g)} \rightleftharpoons 4NO_{(g)} + 6H_2O_{(g)}}\) with \(\ce{\Delta}{H}\) = \(-905.5\ \dfrac{kJ}{mol} \)


    \(\Delta H\) of \(C_6H_{6(g)}\) from \(C_6H_{6(l)}\) to its gaseous form is \(+33.9\dfrac{kJ}{mol}\). Which of these two substances absorbs off more heat when 10 lbs of the substance is burned? Which of these two substances require less energy when condensed to solid form?


    The problem states that the ∆H of the conversion of C6H6(g) to C6H6(l) is positive, and therefore, is an endothermic process. Consequently, ten pounds of C6H6(g) contains more enthalpy than 10 pounds of C6H6(l) . Since these will both produce carbon dioxide and water when burned, their products are of the same final energy level. As a result, C6H6(g) will give off more energy than C6H6(l) when burned and C6H6(l) will require less energy to form a solid.


    Calculate the enthalpy change under standard conditions for the reaction:

    \[\ce{C3H6O(l) + 4 O2 (g) → 3 CO2 (g) + 3 H2O(l)} \nonumber \]

    given information below:

    • mol: 0 kJ/f, O2 (g)H°Δ
    • mol: -393.5 kJ/f, CO2(g)ΔH°
    • ΔH°f, H2O(l): -285.83 kJ/mol
    • ΔH°f, C3H6O(l): -248 kJ/mol

    Hess' Law:

    \[ΔH^o_{rxn} = \sum ΔH^o_{f\,, products} – \sum ΔH^o_{f\,, reactants}\]

    ΔH°rxn = [ 3 (-393.5 kJ/mol) + 3 (-285.83 kJ/mol) ] - [ (-248 kJ/mol) + 4 (0 kJ/mol) ] = -1790 kJ/mol


    A 10 gram sample of pure hydrogen is burned completely with excess oxygen to generate liquid water in a constant volume calorimeter at 25 °C. The amount of heat evolved is 1,420 kJ.

    1. Write and balance the chemical equation for the combustion reaction.
    2. Calculate the standard change in internal energy for the combustion of 1.00 mole hydrogen to liquid water.
    3. Calculate the standard enthalpy change per mole of hydrogen for the same reaction as in part (a).
    4. Calculate the standard enthalpy of formation per mole of hydrogen, using data for the standard enthalpies of formation of liquid water (Table T1).
    1. \(2H_2{(g)} + O_{2(g)} \rightarrow 2H_2O_{(l)}\)
    2. \(ΔU^o= q_v = \dfrac{-1420 \,kJ}{10/(1.008 \times 2 ) g/mol} = -286.3 \,kJ/(mol\, of\, H_2) \)
    3. \(ΔH^o_{rxn}= ΔU^o + Δn_{gas} RT = -286.3 \,kJ/(mol\, of\, H_2) + (2 mol. \, of\, H_2)(-3) (8.314 J/{K/mol}) (298 \,K) = -580\, kJ/mol\)
    4. \(ΔH^o_rxn= 2 \Delta H_f^o \{\ce{H2} \} \) so \(\Delta H_f^o /2 \).

    A consequence of the constant-volume condition is that the heat released corresponds to \(q_v\) and thus to the internal energy change \(ΔU_{sys}\) rather than to \(ΔH_{sys}\) under constant pressure conditions.

    \[\Delta U_{sys} = q_v\nonumber \]

    This comes from the definition of enthalpy

    \[H_{sys} = U_{sys} + PV\nonumber \]

    and associated change

    \[\Delta H_{sys} = \Delta U_{sys} + \Delta (PV)\nonumber \]

    or using the chain rule

    \[\Delta H_{sys} = \Delta U_{sys} + \cancelto{0}{P\Delta V} + V \Delta P \label{Change in Bomb}\nonumber \]

    which simplifies to

    \[\Delta H_{sys} = \Delta U_{sys} + V \Delta P\nonumber \]

    If we assuming ideal gas law for the gases

    \[PV=nRT\nonumber \]


    \[\Delta P = \dfrac{\Delta n R T}{V}\nonumber \]

    substituting this into the equation for enthalpy change gives the enthalpy change under constant volume conditions in terms of changing number of moles

    \[ΔH_{sys} = \Delta U_{sys} + Δn_gRT\nonumber \]


    \[ΔH_{sys} = q_v + Δn_gRT\nonumber \]

    where \(Δn_g\)  is the change in the number of moles of gases in the reaction.


    Carbon dioxide (\(CO_2\)) is a common byproduct of the combustion of fossil fuels. Estimate the standard enthalpy of formation (\(\Delta H_f\)) of carbon dioxide at 25°C, use Table T1.


    First write the equation:

    \[C_{(s)} + O_{2 (g)} \rightarrow CO_{2 (g)}\nonumber \]

    The bond enthalpies in Table T3 allows us to calculate \(\Delta H°\) because 2 C=O and 2 C-O bonds are formed:

    \(\Delta H°\) 2 mol (-192.0 kJ mol-1) + 2 mol (-85.5) = -555 kJ

    Next we need to write the equations for "striping" the atoms from there standard state to single atoms. Each of the atomization has an enthalpy that was found in Table T1:

    \[C_{(s)} \rightarrow C_{(g)}\nonumber \] \(\Delta H°\) = 1 mol (716.7 kJ mol-1) = 716.7 kJ

    \[O_{2 (g)} \rightarrow 2O_{(g)}\nonumber \] \(\Delta H°\) = 2 mol (249.2 kJ mol-1) = 498.4 kJ

    Combine the results of all three equations to calculate \(\Delta H_f\) of 1 mol of CO2:

    -555 kJ + 716.7 kJ + 498.4 kJ = 660.1 kJ

    This solution should be the same if finding the standard enthalpy of formation by using Table T1 which would be -393.5 kJ for one mole of CO2. Since this question is not clear, it is better if the students answering this question to just use Table T1 which will just use the standard heat of formation for and then have the sum of products minus the sum of reactants = the answer. So the answer would be -393.5 kJ.


    Given the table of average bond enthalpies shown below, estimate the enthalpy change \(\Delta H°\) for the following reaction:

    \[2H_2(g) + O_2(g) \rightarrow 2H_2O(l)\nonumber \]

    Bond Bond Enthalpy (kJ/mol)
    \(H-H\) \(436\)
    \(H-O\) \(463\)
    \(O=O\) \(498\)

    To calculate the total enthalpy change of the reaction, we use Hess's Law. Thus, the total enthalpy of formation is equal to the sum of the enthalpy of formation of the reactants and the enthalpy of formation for the products.

    Step 1. \(\Delta H_1\) = the bond enthalpies of \(2H_2(g) + O_2(g)\)

    = \(2(H-H) + (O=O)\)

    = \(2(436) \; kJ/mol + 498 \; kJ/mol\)

    = \(+1370 \; kJ/mol\)

    Step 2. \(\Delta H_2\) = the bond enthalpies of \(2H_2O(l)\)

    = \(2 \times 2 (H-O)\)

    = \(4(463) \; kJ/mol\)

    = \(-1852 \; kJ/mol\)

    Step 3. \(\Delta H°\) = \(\Delta H_1\) + \(\Delta H_2\)

    = \(1370 \; kJ/mol - 1852 \; kJ/mol\)

    = \(-482 \; kJ/mol\)

    Note in Step 1, \(\Delta H_1\) is positive because the process of breaking the bonds into individual atoms is always an endothermic process while in Step 2, \(\Delta H_2\) is negative because the process of creating bonds out of the individual atoms is always an exothermic process.


    Two quantum states are separated by an energy of 0.6 x 10-21J. Calculate the relative populations of the two quantum states at a temperature of 33°C.


    The equation for the relative populations of two quantum states, P2/P1 is given by the equation

    \[\dfrac{P_{2}}{P_{1}}=e^{-(E_{2}-E_{1})/k_B T}\nonumber \]

    Where E2-E1 is the energy difference between the two states, \(k_B\) is the Boltzmann constant, and T is the temperature.

    Plug in the given values into the equation to reach the final answer.

    \[\dfrac{P_{2}}{P_{1}}=e^{-(0.6\bullet10^{-21}J)/1.38\bullet10^{-23}K^{-1}(298K))}\nonumber \]

    \[\dfrac{P_{2}}{P_{1}}=0.86\nonumber \]


    By utilizing the Harmonic Oscillator Model, calculate the relative population of the first energy state and the ground state, both at \(278.15K\), for \(H_{2}\). The force constant for \(H_{2}\) is \(510\dfrac{N}{m}\)


    A few pieces of information need to be understood before going about solving this equation. First, the question asks for the “relative population” of the first energy state at a given temperature (\(278.15K\)) to the energy state at \(0K\). Recall that energy states are basically a way of saying that every chemical species (molecule, atom, etc.) can “have” a specific (discreet) amount of energy. Each of these values are a “state”, and the lowest- value state can be considered the “ground state”, and all states above are “excited states”. Also recall that the states can be named by quantum number; i.e if \(n\) were the quantum number, than the ground state would be \(n=0\) and the first state after that, an excited state, has a quantum number \(n=1\). The next step is to understand what “relative population is”. Basically, this refers to the probability that the species, in this case \(H_{2}\), will be found in one energy state versus another. The equation that describes the probability of a species being in energy level \(n\) is as follows:

    \(P(n)= Ce^{-\varepsilon_{n}/k_{b}T}\)

    Where C is a constant, n is quantum number (energy level), \(k_{b}\) is Boltzmann’s constant, T is temperature, and \(\varepsilon\) is the energy of the molecule, which can be determined as such:

    \(\varepsilon_{n} = \left(n + \dfrac{1}{2}\right)hv\)

    \(hv = \dfrac{h}{2\pi}\sqrt{\dfrac{k}{\mu}}\)

    n, as already seen, is the quantum number. \(hv\) in the equation for \(\varepsilon\) is defined as the product of planck’s constant (\(h\)) divided by \(2\pi\) and the \(\sqrt{\dfrac{k}{\mu}}\), where k is the force constant, which is given in the problem, and the \(\mu\) is the reduced mass, which can be calculated as follows:

    \(\mu = \dfrac{m_{1}m_{2}}{m_{1} + m_{2}}\)

    Where \(m\) is just the mass of each of the atoms. Since the mass of both hydrogens are 1 amu (\(u\),

    \(\mu = \dfrac{1\times1}{1 + 1} = \dfrac{1}{2} u\)

    \(\dfrac{1}{2} u = 8.3027\times10^{-28}kg\)

    Because the question is only interested in relative population, the actual number of molecules there are doesn’t really matter, since relative means to take the ratio between the probability of one energy state to another. Since the two energy states in comparison for this problem is \(n=1, n=0\), (remember ground state is \(n=0\)), the equation is as follows.

    \(\dfrac{P(1)= Ce^{-\varepsilon_{1}/k_{b}278.15K}}{P(0)= Ce^{-\varepsilon_{0}/k_{b}278.15K}}\)

    By simplification,

    \(= e^{\dfrac{\varepsilon_{1} - \varepsilon_{0}}{K_{b}T}}\)

    And, substituting in the formula for energy((\varepsilon\)),

    \(= e^{\dfrac{\left[\left(n + \dfrac{1}{2}\right)hv - \dfrac{1}{2}hv\right]}{K_{b}T}}\)

    \(= e^{nhv/K_{b}T}\)

    Here, \(n=1\) (because the 0 has already been taken into consideration) and \(hv\) is as follows:

    \(hv = \dfrac{h}{2\pi}\sqrt{\dfrac{k}{\mu}}\)

    \(hv = \dfrac{6.62607\times10^{-34}\dfrac{kgm^{2}}{s^2}}{2\pi}\sqrt{\dfrac{510\dfrac{N}{m}}{8.3027\times10^{-28}kg}}\)

    \(hv = \dfrac{6.62607\times10^{-34}Js^{-1}}{2\pi}\sqrt{\dfrac{510\dfrac{N}{m}}{8.3027\times10^{-28}kg}}\)

    \(hv= 8.2650\times 10^{-20} J\)

    All the variables have been found, so all there is left is to substitute and solve.

    \(= e^{\dfrac{-\left(1\right)\left(8.2650\times 10^{-20} J\right)}{1.3806\times10^{-23}\dfrac{m^{2}kg}{s^{2}K}\left(278.15K\right)}}\)

    \(= e^{\dfrac{-\left(1\right)\left(8.2650\times 10^{-20} J\right)}{1.3806\times10^{-23}\dfrac{J}{K}\left(278.15K\right)}}\)

    \(\approx e^{-21.5229}\)

    \(\approx 4.495\times10^{-10}\)

    Thus, the probability of the \(H_{2}\) molecules being in the 1st energy state when compared to the vibrational state of the lowest energy is \(\approx 4.495\times10^{-10}\). This extremely low probability makes sense, because intuition says that the compound will most likely be found at its lowest energy.

    Abstract: Find difference in energy, \(\varepsilon\), divide by Boltzmann's constant (\(K_{b}\)) and Temperature. Plug as \(e^{x}\) and solve.


    A container holds 2 L of gas under 5.00 atm and a ball floating in 10 L of NaOH. As the volume of the gas expands to 20 L, the ball is turned upside down. This turn is caused by the temperature increase of the NaOH after the gas expands. Assuming that no heat is lost, the density of NaOH is 2.13 g/cm3 and the specific heat is 4.184 J/g K, calculate the increase in temperature of the NaOH.


    The "work" completed by the ball to turn equals the negative value of the work the gas absorbs.

    w = -(-P (V2-V1))

    w = -(-5 atm) (20-2) L

    w = 90 atm L (101.325 J/ 1 atm L)

    w = 9119.25 J

    The work carried out by the ball by the NaOH (in order to turn the ball) correlates to the increase in 10 L of NaOH temperature .

    10 L of NaOH (1000 mL/1 L) = 10000 mL = 10000 cm3 (2.13 g/cm3) = 21300 g of NaOH

    q = mCpΔT

    ΔT = (q NaOH) / (Specific Heat NaOH * g NaOH)

    ΔT = (9119.25 J) / (4.184 J/K g)(21300 g)

    ΔT = 0.102 K gained by the NaOH to turn the ball


    Some gas in a piston expands against a constant pressure of 1.2 atm from a volume of 3 L to 18 L. The piston turns an egg beater submerged in 150 g of water. If the water was originally at 25°C, what is its temperature once the gas stops expanding? Assume that all of heat goes into the water and the specific heat capacity of water is 4.184 J K-1 g-1.


    From the first law of thermodynamics

    \[\Delta U = q + w\nonumber \]

    In this case,\(\Delta U =0\), so

    \[q =w = P_{ext}\Delta V = P_{ext} (V_f - V_i)\nonumber \]

    \[ q = (1.2 \;atm )(18\; L - 3\; L) = 14.4 \; L\; atm\nonumber \]

    Convert From L atm to joules using the conversion factor

    \[14.4 \; L\; atm \times 101.325\; J \; L^{-1} atm^{-1} = 1459\; J \nonumber \]

    Now connect the heat transferred to the temperature increased via the specific heat \(c_{sp}\) via

    \[ q = m c_{sp} \Delta T\nonumber \]

    \[ \Delta T = \dfrac{q}{m c_{sp}}\nonumber \]

    \[\Delta T = \dfrac{1459\; J}{(150\;g)(4.184\; J\; K^{-1} g^{-1})} = 2.325 \; K\nonumber \]

    Since initial temperatures is 25° = 298 K so

    \[T_{f} = 298 \; K + 2.325 \;K\nonumber \]

    \[T_{f}=300.325\; K = 27.325°C \nonumber \]