Sample Solution

BCHCT-133 Solved Assignment

PART A: CHEMICAL ENERGETICS AND EQUILIBRIA

  1. (a) (i) Define chemical thermodynamics and outline its significance.
    (ii) Explain the concept of thermodynamic reversibility with the help of a suitable example.
    (b) (i) 223 J of heat was supplied to a thermodynamic system and its internal energy was found to decrease by 92 J . Calculate the amount of associated work and state whether the work was done by the system or done on the system?
    (ii) Derive the relationship between the temperature and pressure for a reversible adiabatic process.
  2. (a) (i) 0.5 mole of an ideal gas is taken in a container at 298 K . Calculate the values of its heat capacities at constant pressure and at constant volume conditions.
    (ii) 1 mole of an ideal gas is allowed to undergo isothermal reversible expansion at 25 C 25 C 25^(@)C25^{\circ} \mathrm{C}25C from a volume of 10 dm 3 10 dm 3 10dm^(3)10 \mathrm{dm}^310dm3 to 20 dm 3 20 dm 3 20dm^(3)20 \mathrm{dm}^320dm3. Calculate the maximum amount of work done by the gas on the surroundings.
(b) (i) Derive the relationship between Δ r U Δ r U Delta _(r)U\Delta_r UΔrU and Δ s H Δ s H Delta _(s)H\Delta_s HΔsH.
(ii) Describe the method for experimental determination of energy changes accompanying chemical reactions under constant volume conditions.
  1. (a) (i) State Hess’ law of constant heat summation and give its significance
    (ii) Using the bond enthalpy datafrom Table 3.2 of (Unit 3; p, 76), calculate the enthalpy of hydrogenation of 1-propene.
(b) (i) Give the mathematical expressions for the thermodynamic and statistical definitions of entropy.
(ii) Explain the effect of temperature on the enthalpy of a reaction and derive the Kirchhoff’s equation.
  1. (a) (i) What is residual entropy? What kind of systems show residual entropy?
    (ii) Explain the difference between enthalpy driven and entropy driven reactions.
(b) (i) Define equilibrium constant and write the expressions for concentration equilibrium constant for the following reaction
N 2 ( g ) + 3 H 2 ( g ) 2 NH 3 ( g ) N 2 ( g ) + 3 H 2 ( g ) 2 NH 3 ( g ) N_(2)(g)+3H_(2)(g)⇌2NH_(3)(g)\mathrm{N}_2(\mathrm{~g})+3 \mathrm{H}_2(\mathrm{~g}) \rightleftharpoons 2 \mathrm{NH}_3(\mathrm{~g})N2( g)+3H2( g)2NH3( g)
(ii) For the following equilibrium reaction
2 SO 2 ( g ) + O 2 ( g ) 2 SO 3 ( g ) K c = 245 ( at 100 K ) 2 SO 2 ( g ) + O 2 ( g ) 2 SO 3 ( g ) K c = 245 ( at 100 K ) 2SO_(2)(g)+O_(2)(g)⇌2SO_(3)(g)K_(c)=245(” at “100K)2 \mathrm{SO}_2(\mathrm{~g})+\mathrm{O}_2(\mathrm{~g}) \rightleftharpoons 2 \mathrm{SO}_3(\mathrm{~g}) K_{\mathrm{c}}=245(\text { at } 100 \mathrm{~K})2SO2( g)+O2( g)2SO3( g)Kc=245( at 100 K)
the equilibrium concentrations are [ SO 2 ] = 0.204 , [ O 2 ] = 0.0264 SO 2 = 0.204 , O 2 = 0.0264 [SO_(2)]=0.204,[O_(2)]=0.0264\left[\mathrm{SO}_2\right]=0.204,\left[\mathrm{O}_2\right]=0.0264[SO2]=0.204,[O2]=0.0264 and [ SO 3 ] = 0.368 SO 3 = 0.368 [SO_(3)]=0.368\left[\mathrm{SO}_3\right]=0.368[SO3]=0.368. Show that the equilibrium will shift towards the reactants side if the concentration of SO 2 SO 2 SO_(2)\mathrm{SO}_2SO2 is suddenly doubled.
  1. (a) (i) Define degree of hydrolysis and derive its relationship with hydrolysis constant
    (ii) Explain the effect of addition of inert gas to a gaseous equilibrium reaction under the conditions of i) constant volume and ii) constant pressure.
    (b) (i) Calculate the pH of 0.1 M aqueous solution of sodium formate at 298 K . [Given: Ka ( HCOOH ) = 1.7 × 10 4 Ka ( HCOOH ) = 1.7 × 10 4 Ka(HCOOH)=1.7 xx10^(-4)\mathrm{Ka}(\mathrm{HCOOH})=1.7 \times 10^{-4}Ka(HCOOH)=1.7×104 at 298 K
    (ii) Define solubility product constant and derive an expression for the solubility product constant for a sparingly soluble salt of M 2 A 3 M 2 A 3 M_(2)A_(3)\mathrm{M}_2 \mathrm{~A}_3M2 A3 type having a solubility of S mol dm 3 mol dm 3 moldm^(-3)\mathrm{mol} \mathrm{dm}{ }^{-3}moldm3.

PART B: FUNCTIONAL GROUP ORGANIC CHEMISTRY-I

  1. (a) Both 1,3,5-cycloheptatrienyl cation and 1,3,5-cycloheptatriene have 6 π 6 π 6pi6 \pi6π elections, comments on the aromaticity of these compounds.
    (b) Discuss the role of Lewis acids in halogenations and alkylation reactions of benzene. Write the limitations of Freidel Crafts alkylation reaction.
  2. (a) Nitro group is meta directing, explain.
    (b) What would be the final products of the reaction of HI with diethyl ether and anisol? Write the mechanism of both the reactions.
  3. (a) What is aldol condensation? Write its mechanism.
    (b) Arrange the following in order of their increasing reactivity towards S N 2 S N 2 S_(N)2\mathrm{S}_{\mathrm{N}} 2SN2 substitution reactions: bromomethane, 1-bromo-propane, 2-bromopropane, 2 -bormo-2-methyl propane. Justify your answer.
  4. (a) Write their representative reaction for the following reactions.
    (b) Sandmeyer reaction
    (c) Reimer-Tiemann reaction
    (d) Mannich reaction
    (e) Willgerodt reaction
    (f) Knoevenagel reaction
10 (a) Write the mechanism of Pinacol-pinacolone reaction.
(b) How you will introduce a formyl group into phenol ring.

Answer:

Question:-1

1. (a) (i) Define chemical thermodynamics and outline its significance.

Answer:

Chemical Thermodynamics is the branch of physical chemistry that deals with the relationships between heat, work, energy, and the properties of matter during chemical reactions. It focuses on understanding how energy is transferred and transformed in chemical processes and helps in predicting the direction and extent of reactions.
Significance of Chemical Thermodynamics:
  1. Predicting Reaction Feasibility: It helps in determining whether a chemical reaction will occur spontaneously under specific conditions.
  2. Understanding Energy Transfer: It provides insights into how energy is absorbed or released during chemical reactions, essential for designing efficient processes in industries.
  3. Equilibrium Analysis: Chemical thermodynamics aids in understanding the conditions under which a chemical equilibrium is reached, guiding the optimization of industrial reactions.
  4. Calculating Work and Heat: It enables the calculation of work done by or on a system and the heat exchanged, crucial for processes like engines, refrigeration, and chemical manufacturing.
  5. Design of Chemical Processes: The principles of thermodynamics are key in designing processes like distillation, refrigeration, and power plants, ensuring they are energy-efficient and cost-effective.
  6. Enzyme and Biological Reactions: It helps explain biochemical processes in living organisms, from metabolic pathways to the functioning of enzymes.

1. (a) (ii) Explain the concept of thermodynamic reversibility with the help of a suitable example.

Answer:

Thermodynamic Reversibility refers to a process that can be reversed without any net change in both the system and its surroundings. In a reversible process, the system is in equilibrium at every stage, meaning it can be returned to its original state by infinitesimally small changes in external conditions, without dissipation of energy.
For a process to be truly reversible, it must be carried out infinitely slowly, so the system remains in thermodynamic equilibrium throughout. In real-life situations, some degree of irreversibility always occurs due to friction, heat loss, or other factors.

Example: Reversible Isothermal Expansion of an Ideal Gas

Imagine an ideal gas confined in a piston at a certain temperature and pressure. If the gas expands isothermally (at a constant temperature) in a perfectly reversible manner, it does so in such a way that the temperature of the gas remains constant throughout the expansion. The gas does work on the piston, but the heat energy required for the expansion is supplied from the surroundings, maintaining the temperature.
  • Process description:
    • The gas is allowed to expand slowly by pushing the piston up.
    • At every point during the expansion, the gas is in thermal equilibrium with its surroundings (since heat is exchanged to maintain temperature).
    • The system’s pressure and volume change continuously and uniformly, ensuring no entropy is generated.
  • Reversibility:
    • If you reverse the process, you can compress the gas back to its original volume and pressure by lowering the piston very slowly, again ensuring equilibrium at every stage.
    • No energy is lost in the process, and both the system and surroundings are returned to their original states with no net change in entropy.
In contrast, an irreversible process (like the rapid expansion of the gas into a vacuum, also known as free expansion) involves a sudden change, causing a large increase in entropy and heat dissipation to the surroundings, making it impossible to reverse the process without additional work.
Thus, thermodynamic reversibility ensures the maximum possible efficiency and no energy loss, a concept critical to understanding idealized processes in thermodynamics.

1. (b) (i) 223 J of heat was supplied to a thermodynamic system and its internal energy was found to decrease by 92 J. Calculate the amount of associated work and state whether the work was done by the system or done on the system?

Answer:

To solve this problem, we can use the First Law of Thermodynamics, which states:
Δ U = Q W Δ U = Q W Delta U=Q-W\Delta U = Q – WΔU=QW
Where:
  • Δ U Δ U Delta U\Delta UΔU is the change in internal energy of the system.
  • Q Q QQQ is the heat supplied to the system.
  • W W WWW is the work done by the system.

Given:

  • Heat supplied, Q = 223 J Q = 223 J Q=223″J”Q = 223 \, \text{J}Q=223J
  • Change in internal energy, Δ U = 92 J Δ U = 92 J Delta U=-92″J”\Delta U = -92 \, \text{J}ΔU=92J (The internal energy decreases, so it’s negative.)
Now, substitute the values into the equation:
92 = 223 W 92 = 223 W -92=223-W-92 = 223 – W92=223W
Rearranging to solve for W W WWW:
W = 223 + 92 = 315 J W = 223 + 92 = 315 J W=223+92=315″J”W = 223 + 92 = 315 \, \text{J}W=223+92=315J

Interpretation:

The positive value of W = 315 J W = 315 J W=315″J”W = 315 \, \text{J}W=315J means that 315 J of work was done by the system on its surroundings.
Thus, the system did work as it lost some of the supplied heat to do work while its internal energy decreased.

1. (b) (ii) Derive the relationship between the temperature and pressure for a reversible adiabatic process.

Answer:

Deriving the Relationship between Temperature and Pressure for a Reversible Adiabatic Process

We aim to find the relationship between temperature and pressure for a reversible adiabatic process.

Step 1: Start with the First Law of Thermodynamics

For an adiabatic process, there is no heat exchange, so the change in internal energy is equal to the work done by or on the gas:
d U = p d V d U = p d V dU=-pdV\mathrm{d}U = -p \, \mathrm{d}VdU=pdV
Since internal energy change for an ideal gas is given by d U = C V d T d U = C V d T dU=C_(V)dT\mathrm{d}U = C_V \, \mathrm{d}TdU=CVdT, where C V C V C_(V)C_VCV is the heat capacity at constant volume, we can equate the two expressions:
C V d T = p d V C V d T = p d V C_(V)dT=-pdVC_V \, \mathrm{d}T = -p \, \mathrm{d}VCVdT=pdV

Step 2: Substitute Ideal Gas Equation

For an ideal gas, we have the equation of state:
p = n R T V p = n R T V p=(nRT)/(V)p = \frac{nRT}{V}p=nRTV
Substitute this into the equation:
C V d T = n R T V d V C V d T = n R T V d V C_(V)dT=-(nRT)/(V)dVC_V \, \mathrm{d}T = -\frac{nRT}{V} \, \mathrm{d}VCVdT=nRTVdV
Rearrange this equation:
C V d T T = n R d V V C V d T T = n R d V V (C_(V)dT)/(T)=-(nRdV)/(V)\frac{C_V \, \mathrm{d}T}{T} = -\frac{nR \, \mathrm{d}V}{V}CVdTT=nRdVV

Step 3: Integrate to Find the Relationship

Now, integrate both sides from state 1 to state 2. Assuming that C V C V C_(V)C_VCV is constant:
C V T 1 T 2 d T T = n R V 1 V 2 d V V C V T 1 T 2 d T T = n R V 1 V 2 d V V C_(V)int_(T_(1))^(T_(2))(dT)/(T)=-nRint_(V_(1))^(V_(2))(dV)/(V)C_V \int_{T_1}^{T_2} \frac{\mathrm{d}T}{T} = -nR \int_{V_1}^{V_2} \frac{\mathrm{d}V}{V}CVT1T2dTT=nRV1V2dVV
This gives:
C V ln ( T 2 T 1 ) = n R ln ( V 2 V 1 ) C V ln T 2 T 1 = n R ln V 2 V 1 C_(V)ln((T_(2))/(T_(1)))=-nR ln((V_(2))/(V_(1)))C_V \ln\left(\frac{T_2}{T_1}\right) = -nR \ln\left(\frac{V_2}{V_1}\right)CVln(T2T1)=nRln(V2V1)
Rearrange the equation:
C V n R ln ( T 2 T 1 ) = ln ( V 1 V 2 ) C V n R ln T 2 T 1 = ln V 1 V 2 (C_(V))/(nR)ln((T_(2))/(T_(1)))=ln((V_(1))/(V_(2)))\frac{C_V}{nR} \ln\left(\frac{T_2}{T_1}\right) = \ln\left(\frac{V_1}{V_2}\right)CVnRln(T2T1)=ln(V1V2)

Step 4: Apply Logarithmic Properties

Using logarithmic properties, we get:
ln ( T 2 T 1 ) C V n R = ln ( V 1 V 2 ) ln T 2 T 1 C V n R = ln V 1 V 2 ln ((T_(2))/(T_(1)))^((C_(V))/(nR))=ln((V_(1))/(V_(2)))\ln\left(\frac{T_2}{T_1}\right)^{\frac{C_V}{nR}} = \ln\left(\frac{V_1}{V_2}\right)ln(T2T1)CVnR=ln(V1V2)
Taking the antilogarithm of both sides:
( T 2 T 1 ) C V n R = V 1 V 2 T 2 T 1 C V n R = V 1 V 2 ((T_(2))/(T_(1)))^((C_(V))/(nR))=(V_(1))/(V_(2))\left(\frac{T_2}{T_1}\right)^{\frac{C_V}{nR}} = \frac{V_1}{V_2}(T2T1)CVnR=V1V2
Now, simplify to get:
T 2 T 1 = ( V 1 V 2 ) C V n R T 2 T 1 = V 1 V 2 C V n R (T_(2))/(T_(1))=((V_(1))/(V_(2)))^((C_(V))/(nR))\frac{T_2}{T_1} = \left(\frac{V_1}{V_2}\right)^{\frac{C_V}{nR}}T2T1=(V1V2)CVnR

Step 5: Substitute the Specific Heat Ratio γ γ gamma\gammaγ

We know that γ = C P C V γ = C P C V gamma=(C_(P))/(C_(V))\gamma = \frac{C_P}{C_V}γ=CPCV, where C P C P C_(P)C_PCP is the heat capacity at constant pressure. Therefore:
T 2 T 1 = ( V 1 V 2 ) γ 1 T 2 T 1 = V 1 V 2 γ 1 (T_(2))/(T_(1))=((V_(1))/(V_(2)))^(gamma-1)\frac{T_2}{T_1} = \left(\frac{V_1}{V_2}\right)^{\gamma – 1}T2T1=(V1V2)γ1
This simplifies to the well-known adiabatic equation:
T 1 V 1 γ 1 = T 2 V 2 γ 1 T 1 V 1 γ 1 = T 2 V 2 γ 1 T_(1)V_(1)^(gamma-1)=T_(2)V_(2)^(gamma-1)T_1 V_1^{\gamma – 1} = T_2 V_2^{\gamma – 1}T1V1γ1=T2V2γ1

Step 6: Deriving the Temperature-Pressure Relationship

To get the temperature-pressure relationship, we use the ideal gas law for one mole of gas:
p 1 V 1 T 1 = p 2 V 2 T 2 p 1 V 1 T 1 = p 2 V 2 T 2 (p_(1)V_(1))/(T_(1))=(p_(2)V_(2))/(T_(2))\frac{p_1 V_1}{T_1} = \frac{p_2 V_2}{T_2}p1V1T1=p2V2T2
This simplifies to:
V 1 V 2 = p 2 T 1 p 1 T 2 V 1 V 2 = p 2 T 1 p 1 T 2 (V_(1))/(V_(2))=(p_(2)T_(1))/(p_(1)T_(2))\frac{V_1}{V_2} = \frac{p_2 T_1}{p_1 T_2}V1V2=p2T1p1T2
Substitute this into the previous equation T 2 T 1 = ( V 1 V 2 ) γ 1 T 2 T 1 = V 1 V 2 γ 1 (T_(2))/(T_(1))=((V_(1))/(V_(2)))^(gamma-1)\frac{T_2}{T_1} = \left(\frac{V_1}{V_2}\right)^{\gamma – 1}T2T1=(V1V2)γ1:
T 2 T 1 = ( p 2 T 1 p 1 T 2 ) γ 1 T 2 T 1 = p 2 T 1 p 1 T 2 γ 1 (T_(2))/(T_(1))=((p_(2)T_(1))/(p_(1)T_(2)))^(gamma-1)\frac{T_2}{T_1} = \left( \frac{p_2 T_1}{p_1 T_2} \right)^{\gamma – 1}T2T1=(p2T1p1T2)γ1
Simplify the equation:
( T 2 T 1 ) γ = ( p 2 p 1 ) γ 1 T 2 T 1 γ = p 2 p 1 γ 1 ((T_(2))/(T_(1)))^(gamma)=((p_(2))/(p_(1)))^(gamma-1)\left(\frac{T_2}{T_1}\right)^{\gamma} = \left(\frac{p_2}{p_1}\right)^{\gamma – 1}(T2T1)γ=(p2p1)γ1
Finally, rearranging to express T 2 T 2 T_(2)T_2T2 in terms of p 2 p 2 p_(2)p_2p2 and T 1 T 1 T_(1)T_1T1, p 1 p 1 p_(1)p_1p1:
T 2 T 1 = ( p 1 p 2 ) 1 γ γ T 2 T 1 = p 1 p 2 1 γ γ (T_(2))/(T_(1))=((p_(1))/(p_(2)))^((1-gamma)/(gamma))\frac{T_2}{T_1} = \left(\frac{p_1}{p_2}\right)^{\frac{1-\gamma}{\gamma}}T2T1=(p1p2)1γγ
Thus, the relationship between temperature and pressure for an adiabatic process is:
T 1 p 1 1 γ γ = T 2 p 2 1 γ γ T 1 p 1 1 γ γ = T 2 p 2 1 γ γ T_(1)p_(1)^((1-gamma)/(gamma))=T_(2)p_(2)^((1-gamma)/(gamma))T_1 p_1^{\frac{1-\gamma}{\gamma}} = T_2 p_2^{\frac{1-\gamma}{\gamma}}T1p11γγ=T2p21γγ
This equation shows how temperature and pressure are related during an adiabatic expansion or compression.


Question:-2

2. (a) (i) 0.5 mole of an ideal gas is taken in a container at 298 K. Calculate the values of its heat capacities at constant pressure and at constant volume conditions.

Answer:

To calculate the heat capacities of an ideal gas at constant pressure ( C P C P C_(P)C_PCP) and constant volume ( C V C V C_(V)C_VCV), we will use the general relationships for ideal gases and the values of the specific heat capacities in terms of the gas constant.

Step 1: Understanding the given information

  • Number of moles of the gas, n = 0.5 mol n = 0.5 mol n=0.5″mol”n = 0.5 \, \text{mol}n=0.5mol
  • Temperature, T = 298 K T = 298 K T=298″K”T = 298 \, \text{K}T=298K
We’ll assume the gas behaves ideally and that we are working with a diatomic ideal gas (which is typical unless otherwise specified).

Step 2: Use of heat capacities for ideal gases

For an ideal gas, the heat capacities at constant volume and constant pressure are related to the molar specific heats:
  • C V = f 2 R C V = f 2 R C_(V)=(f)/(2)RC_V = \frac{f}{2} RCV=f2R, where f f fff is the number of degrees of freedom of the gas molecules.
  • C P = C V + R C P = C V + R C_(P)=C_(V)+RC_P = C_V + RCP=CV+R, where R R RRR is the universal gas constant ( R = 8.314 J/mol·K R = 8.314 J/mol·K R=8.314″J/mol·K”R = 8.314 \, \text{J/mol·K}R=8.314J/mol·K).

Step 3: Assumption about the type of gas

If the gas is diatomic (e.g., oxygen or nitrogen), then the number of degrees of freedom f f fff is typically 5 (3 translational and 2 rotational degrees of freedom, assuming we are neglecting vibrational modes at this temperature).
For a diatomic gas:
  • C V = 5 2 R C V = 5 2 R C_(V)=(5)/(2)RC_V = \frac{5}{2} RCV=52R
  • C P = C V + R = 5 2 R + R = 7 2 R C P = C V + R = 5 2 R + R = 7 2 R C_(P)=C_(V)+R=(5)/(2)R+R=(7)/(2)RC_P = C_V + R = \frac{5}{2} R + R = \frac{7}{2} RCP=CV+R=52R+R=72R

Step 4: Calculate the heat capacities

Using R = 8.314 J/mol·K R = 8.314 J/mol·K R=8.314″J/mol·K”R = 8.314 \, \text{J/mol·K}R=8.314J/mol·K:

For C V C V C_(V)C_VCV:

C V = 5 2 × 8.314 = 20.785 J/mol·K C V = 5 2 × 8.314 = 20.785 J/mol·K C_(V)=(5)/(2)xx8.314=20.785″J/mol·K”C_V = \frac{5}{2} \times 8.314 = 20.785 \, \text{J/mol·K}CV=52×8.314=20.785J/mol·K

For C P C P C_(P)C_PCP:

C P = 7 2 × 8.314 = 29.099 J/mol·K C P = 7 2 × 8.314 = 29.099 J/mol·K C_(P)=(7)/(2)xx8.314=29.099″J/mol·K”C_P = \frac{7}{2} \times 8.314 = 29.099 \, \text{J/mol·K}CP=72×8.314=29.099J/mol·K

Step 5: Calculate for 0.5 mole of gas

Now, since we have 0.5 moles of the gas:

For C V C V C_(V)C_VCV for 0.5 moles:

C V = 20.785 × 0.5 = 10.3925 J/K C V = 20.785 × 0.5 = 10.3925 J/K C_(V)=20.785 xx0.5=10.3925″J/K”C_V = 20.785 \times 0.5 = 10.3925 \, \text{J/K}CV=20.785×0.5=10.3925J/K

For C P C P C_(P)C_PCP for 0.5 moles:

C P = 29.099 × 0.5 = 14.5495 J/K C P = 29.099 × 0.5 = 14.5495 J/K C_(P)=29.099 xx0.5=14.5495″J/K”C_P = 29.099 \times 0.5 = 14.5495 \, \text{J/K}CP=29.099×0.5=14.5495J/K

Final Answer:

  • The heat capacity at constant volume ( C V C V C_(V)C_VCV) is 10.39 J/K 10.39 J/K 10.39″J/K”\boxed{10.39 \, \text{J/K}}10.39J/K.
  • The heat capacity at constant pressure ( C P C P C_(P)C_PCP) is 14.55 J/K 14.55 J/K 14.55″J/K”\boxed{14.55 \, \text{J/K}}14.55J/K.

2. (a) (ii) 1 mole of an ideal gas is allowed to undergo isothermal reversible expansion at 25 C 25 C 25^(@)C25^{\circ} \mathrm{C}25C from a volume of 10 dm 3 10 dm 3 10dm^(3)10 \mathrm{dm}^310dm3 to 20 dm 3 20 dm 3 20dm^(3)20 \mathrm{dm}^320dm3. Calculate the maximum amount of work done by the gas on the surroundings.

Answer:

To calculate the maximum work done by the gas on the surroundings during an isothermal reversible expansion, we can use the formula for work in an isothermal process for an ideal gas:
W = n R T ln ( V 2 V 1 ) W = n R T ln V 2 V 1 W=nRT ln((V_(2))/(V_(1)))W = nRT \ln \left(\frac{V_2}{V_1}\right)W=nRTln(V2V1)
Where:
  • W W WWW is the work done by the gas.
  • n n nnn is the number of moles of the gas.
  • R R RRR is the universal gas constant ( R = 8.314 J/mol·K R = 8.314 J/mol·K R=8.314″J/mol·K”R = 8.314 \, \text{J/mol·K}R=8.314J/mol·K).
  • T T TTT is the temperature in Kelvin.
  • V 1 V 1 V_(1)V_1V1 and V 2 V 2 V_(2)V_2V2 are the initial and final volumes, respectively.

Step 1: Convert all given values to proper units

  • Number of moles of gas, n = 1 mol n = 1 mol n=1″mol”n = 1 \, \text{mol}n=1mol
  • Temperature, T = 25 C = 25 + 273.15 = 298.15 K T = 25 C = 25 + 273.15 = 298.15 K T=25^(@)”C”=25+273.15=298.15″K”T = 25^\circ \text{C} = 25 + 273.15 = 298.15 \, \text{K}T=25C=25+273.15=298.15K
  • Initial volume, V 1 = 10 dm 3 = 10 × 10 3 m 3 = 0.01 m 3 V 1 = 10 dm 3 = 10 × 10 3 m 3 = 0.01 m 3 V_(1)=10″dm”^(3)=10 xx10^(-3)”m”^(3)=0.01″m”^(3)V_1 = 10 \, \text{dm}^3 = 10 \times 10^{-3} \, \text{m}^3 = 0.01 \, \text{m}^3V1=10dm3=10×103m3=0.01m3
  • Final volume, V 2 = 20 dm 3 = 20 × 10 3 m 3 = 0.02 m 3 V 2 = 20 dm 3 = 20 × 10 3 m 3 = 0.02 m 3 V_(2)=20″dm”^(3)=20 xx10^(-3)”m”^(3)=0.02″m”^(3)V_2 = 20 \, \text{dm}^3 = 20 \times 10^{-3} \, \text{m}^3 = 0.02 \, \text{m}^3V2=20dm3=20×103m3=0.02m3

Step 2: Apply the formula for work

W = ( 1 ) × ( 8.314 ) × ( 298.15 ) × ln ( 0.02 0.01 ) W = ( 1 ) × ( 8.314 ) × ( 298.15 ) × ln 0.02 0.01 W=(1)xx(8.314)xx(298.15)xx ln((0.02)/(0.01))W = (1) \times (8.314) \times (298.15) \times \ln \left(\frac{0.02}{0.01}\right)W=(1)×(8.314)×(298.15)×ln(0.020.01)
Now, calculate the logarithmic term:
ln ( 0.02 0.01 ) = ln ( 2 ) 0.693 ln 0.02 0.01 = ln ( 2 ) 0.693 ln((0.02)/(0.01))=ln(2)~~0.693\ln \left(\frac{0.02}{0.01}\right) = \ln(2) \approx 0.693ln(0.020.01)=ln(2)0.693
Substitute this value into the equation:
W = 8.314 × 298.15 × 0.693 W = 8.314 × 298.15 × 0.693 W=8.314 xx298.15 xx0.693W = 8.314 \times 298.15 \times 0.693W=8.314×298.15×0.693
W 8.314 × 207.515 W 8.314 × 207.515 W~~8.314 xx207.515W \approx 8.314 \times 207.515W8.314×207.515
W 1722.2 J W 1722.2 J W~~1722.2″J”W \approx 1722.2 \, \text{J}W1722.2J

Final Answer:

The maximum work done by the gas on the surroundings during the isothermal reversible expansion is approximately 1722.2 J 1722.2 J 1722.2″J”\boxed{1722.2 \, \text{J}}1722.2J.

2. (b) (i) Derive the relationship between Δ r U Δ r U Delta _(r)U\Delta_r UΔrU and Δ s H Δ s H Delta _(s)H\Delta_s HΔsH.

Answer:

To derive the relationship between the change in internal energy ( Δ r U Δ r U Delta _(r)U\Delta_r UΔrU) and the change in enthalpy ( Δ r H Δ r H Delta _(r)H\Delta_r HΔrH) for a reversible reaction, we need to start with the fundamental thermodynamic definitions and use the first law of thermodynamics.

Step 1: Recall the first law of thermodynamics

The first law of thermodynamics states that the change in internal energy ( Δ U Δ U Delta U\Delta UΔU) for a system is related to the heat ( Q Q QQQ) and the work ( W W WWW) done by or on the system:
Δ U = Q W Δ U = Q W Delta U=Q-W\Delta U = Q – WΔU=QW
For a reversible process, the work done by an ideal gas is W = P Δ V W = P Δ V W=P Delta VW = P \Delta VW=PΔV, where P P PPP is the pressure and Δ V Δ V Delta V\Delta VΔV is the change in volume.

Step 2: Define Enthalpy

Enthalpy H H HHH is defined as:
H = U + P V H = U + P V H=U+PVH = U + PVH=U+PV
The change in enthalpy ( Δ H Δ H Delta H\Delta HΔH) is therefore:
Δ H = Δ U + Δ ( P V ) Δ H = Δ U + Δ ( P V ) Delta H=Delta U+Delta(PV)\Delta H = \Delta U + \Delta (PV)ΔH=ΔU+Δ(PV)
Now, if the pressure is constant during the process (which is often assumed in many reactions), the term Δ ( P V ) Δ ( P V ) Delta(PV)\Delta(PV)Δ(PV) can be written as P Δ V P Δ V P Delta VP \Delta VPΔV. So, we get:
Δ H = Δ U + P Δ V Δ H = Δ U + P Δ V Delta H=Delta U+P Delta V\Delta H = \Delta U + P \Delta VΔH=ΔU+PΔV

Step 3: Relating Δ r U Δ r U Delta _(r)U\Delta_r UΔrU and Δ r H Δ r H Delta _(r)H\Delta_r HΔrH for a Reversible Process

Now, let’s relate this to a reversible reaction. For a reversible reaction, we can write the change in internal energy ( Δ r U Δ r U Delta _(r)U\Delta_r UΔrU) and change in enthalpy ( Δ r H Δ r H Delta _(r)H\Delta_r HΔrH) for the reaction as:
Δ r H = Δ r U + P Δ V Δ r H = Δ r U + P Δ V Delta _(r)H=Delta _(r)U+P Delta V\Delta_r H = \Delta_r U + P \Delta VΔrH=ΔrU+PΔV
This equation relates the change in enthalpy to the change in internal energy and the work done during the process.

Step 4: Generalize for Reactions Involving Heat Transfer

In many cases, heat is transferred during a reaction, and this heat is related to the enthalpy change. For an isothermal process (constant temperature) or a process where the heat exchanged is not a function of the change in volume alone, the relationship will take the form:
Δ r U = Δ r H P Δ V Δ r U = Δ r H P Δ V Delta _(r)U=Delta _(r)H-P Delta V\Delta_r U = \Delta_r H – P \Delta VΔrU=ΔrHPΔV
This equation shows how the change in internal energy for a reversible reaction ( Δ r U Δ r U Delta _(r)U\Delta_r UΔrU) is related to the change in enthalpy ( Δ r H Δ r H Delta _(r)H\Delta_r HΔrH) and the work done by the system.

Step 5: Special Case for Ideal Gases

For ideal gases, where P Δ V = n R Δ T P Δ V = n R Δ T P Delta V=nR Delta TP \Delta V = n R \Delta TPΔV=nRΔT (and assuming temperature is constant or known), the above equation simplifies further, but this equation gives the general relationship between Δ r U Δ r U Delta _(r)U\Delta_r UΔrU and Δ r H Δ r H Delta _(r)H\Delta_r HΔrH in terms of the pressure-volume work.

Final Answer:

Thus, the relationship between the change in internal energy and the change in enthalpy is:
Δ r U = Δ r H P Δ V Δ r U = Δ r H P Δ V Delta _(r)U=Delta _(r)H-P Delta V\Delta_r U = \Delta_r H – P \Delta VΔrU=ΔrHPΔV
This expresses how the internal energy change for a reversible reaction depends on the change in enthalpy and the volume change in the system.

2. (b) (ii) Describe the method for experimental determination of energy changes accompanying chemical reactions under constant volume conditions.

Answer:

The experimental determination of energy changes ( Δ U Δ U Delta U\Delta UΔU) accompanying chemical reactions under constant volume conditions is typically performed using a bomb calorimeter. This is a device designed to measure the heat released or absorbed during a reaction while keeping the volume constant, which allows for the determination of the internal energy change ( Δ U Δ U Delta U\Delta UΔU).

Method for Experimental Determination of Energy Changes

Here’s a step-by-step outline of the method:

Step 1: Set Up a Bomb Calorimeter

A bomb calorimeter consists of a sealed, rigid container known as the "bomb," which holds the sample (usually a fuel or reactant). The bomb is surrounded by water, and temperature sensors are placed inside both the bomb and the surrounding water.
  • The bomb is designed to withstand high pressures, especially when the reaction involves combustion.
  • The system is isolated to ensure no heat exchange with the external environment (adiabatic conditions).

Step 2: Place the Reactants in the Bomb

  • The reactants (e.g., a known mass of a substance like a fuel) are placed inside the bomb, typically in the form of a solid or liquid.
  • The bomb is filled with pure oxygen to ensure complete combustion or reaction in the case of a combustion reaction.

Step 3: Ignite the Reaction

  • The reaction is initiated (e.g., by using an electrically heated wire) to ensure it proceeds completely under controlled conditions.
  • Since the bomb is sealed and the volume is constant, no expansion of the gases is allowed, and the system is effectively at constant volume.

Step 4: Measure the Temperature Change

  • After the reaction is initiated, the heat released (or absorbed) by the reaction is transferred to the surrounding water.
  • The temperature of the water is carefully monitored using temperature sensors (often thermocouples or resistance thermometers).

Step 5: Calculate the Heat Released (or Absorbed)

  • The heat change ( q water q water q_(“water”)q_{\text{water}}qwater) in the surrounding water is calculated using the formula:
q water = m w C w Δ T q water = m w C w Δ T q_(“water”)=m_(w)C_(w)Delta Tq_{\text{water}} = m_w C_w \Delta Tqwater=mwCwΔT
Where:
  • m w m w m_(w)m_wmw = mass of the water surrounding the bomb.
  • C w C w C_(w)C_wCw = specific heat capacity of water.
  • Δ T Δ T Delta T\Delta TΔT = temperature change of the water.

Step 6: Determine the Energy Change ( Δ U Δ U Delta U\Delta UΔU)

  • Under constant volume, the heat absorbed or released by the system is equal to the change in internal energy ( Δ U Δ U Delta U\Delta UΔU) of the system. This is because no work is done (since Δ V = 0 Δ V = 0 Delta V=0\Delta V = 0ΔV=0, and W = P Δ V W = P Δ V W=P Delta VW = P \Delta VW=PΔV).
  • The energy change ( Δ U Δ U Delta U\Delta UΔU) for the reaction at constant volume is thus:
Δ U = q water Δ U = q water Delta U=-q_(“water”)\Delta U = – q_{\text{water}}ΔU=qwater
Where the negative sign accounts for the heat lost by the system (the reaction) being absorbed by the surrounding water.

Step 7: Account for Heat Capacity of the Calorimeter

To improve accuracy, the heat capacity of the entire calorimeter (which includes the bomb, the water, and other components) is often measured beforehand. If the calorimeter is not perfectly insulated, a correction may be applied based on the heat capacity C calorimeter C calorimeter C_(“calorimeter”)C_{\text{calorimeter}}Ccalorimeter to determine the true energy change.
Δ U = ( q water + C calorimeter Δ T ) Δ U = ( q water + C calorimeter Δ T ) Delta U=-(q_(“water”)+C_(“calorimeter”)Delta T)\Delta U = – (q_{\text{water}} + C_{\text{calorimeter}} \Delta T)ΔU=(qwater+CcalorimeterΔT)

Step 8: Analysis and Calculation

  • The energy change Δ U Δ U Delta U\Delta UΔU is determined based on the temperature change measured in the water and the known calorimetric constants.
  • If the reaction involves a change in temperature, volume, or involves gases, additional corrections may be required to account for the properties of the reactants and products.

Final Answer:

The experimental determination of energy changes ( Δ U Δ U Delta U\Delta UΔU) under constant volume conditions is typically done using a bomb calorimeter. This method involves measuring the heat transferred to the surrounding water, from which the energy change is derived. The process assumes no work is done by the system (constant volume), and the heat released or absorbed corresponds directly to the change in internal energy of the system.

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