Wednesday, 25 March 2026

Numerical Assignment On Thermodynamics, Mass And Heat Transfer

Solved Problems: Thermodynamics and Mass & Heat Transfer Assignment

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Numericals on Thermodynamics:

Numerical Assignment On Thermodynamics...

1. Mass enters an open system with one inlet and one exit at a constant rate of 50 kg/min. At the exit, the mass flow rate is 60 kg/min. If the system initially contains 1000 kg of working fluid, determine the time when the system mass becomes 500 kg.

pv diagram and first law of thermodynamics


2. Mass leaves an open system with a mass flow rate of \( c \cdot m \), where c is a constant and m is the system mass. If the mass of the system at t = 0 is \( m_0 \), derive an expression for the mass of the system at time t.


3. Water enters a vertical cylindrical tank of cross-sectional area 0.01 \( m^2 \) at a constant mass flow rate of 5 kg/s. It leaves the tank through an exit near the base with a mass flow rate given by the formula 0.2h kg/s, where h is the instantaneous height in m. If the tank is empty initially, develop an expression for the liquid height h as a function of time t. Assume density of water to remain constant at 1000 \( kg/m^3 \).


4. A conical tank of base diameter D and height H is suspended in an inverted position to hold water. A leak at the apex of the cone causes water to leave with a mass flow rate of \( c \sqrt{h} \), where c is a constant and h is the height of the water level from the leak at the bottom.

  • (a) Determine the rate of change of height h.
  • (b) Express h as a function of time t and other known constants, \( \rho \) (constant density of water), D, H, and c if the tank was completely full at t=0.


5. Steam enters a mixing chamber at 100 kPa, 20 m/s, with a specific volume of 0.4 \( m^3/kg \). Liquid water at 100 kPa and \( 25 ^\circ C \) enters the chamber through a separate duct with a flow rate of 50 kg/s and a velocity of 5 m/s. If liquid water leaves the chamber at 100 kPa and \( 43 ^\circ C \) with a volumetric flow rate of 3.357 \( m^3/min \) and a velocity of 5.58 m/s, determine the port areas at the inlets and exit. Assume liquid water density to be 1000 \( kg/m^3 \) and steady state operation.


6. Air is pumped into and withdrawn from a 10 \( m^3 \) rigid tank as shown in the accompanying figure. The inlet and exit conditions are as follows. Inlet: \( v_1 \, = \, 2 \, m^3/kg \), \( V_1 \) = 10 m/s, \( A_1 \) = 0.01 \( m^2 \); Exit: \( v_2 \) = 5 \( m^3/kg \), \( V_2 \) = 5m/s, \( A_2 \) = 0.015 \( m^2 \). Assuming the tank to be uniform at all time with the specific volume and pressure related through pv = 9.0 \( kPa.m^3 \), determine the rate of change of pressure in the tank.


7. A gas flows steadily through a circular duct of varying cross-section area with a mass flow rate of 10 kg/s. The inlet and exit conditions are as follows. Inlet: \( V_1 \) = 400 m/s, \( A_1 \) = 179.36 \( cm^2 \); Exit: \( V_2 \) = 584 m/s, \( v_2 \) = 1.1827 m/kg.

  • (a) Determine the exit area.
  • (b) Do you find the increase in velocity of the gas accompanied by an increase in flow area counter intuitive? Why?


8. Steam enters a turbine with a mass flow rate of 10 kg/s at 10 MPa, \( 600 ^\circ C \), 30 m/s, it exits the turbine at 45 kPa, 30 m/s with a quality of 0.9. Assuming steady-state operation, determine

  • (a) the inlet area, and
  • (b) the exit area.
To solve Question 1 from the provided text, we can use the principle of conservation of mass for an open system.
Question 1:
Mass enters an open system with one inlet and one exit at a constant rate of \( 50 \text{ kg/min} \). At the exit, the mass flow rate is \( 60 \text{ kg/min} \). If the system initially contains \( 1000 \text{ kg} \) of working fluid, determine the time when the system mass becomes $500 \text{ kg}$.
Solution:

1. Identify the Given Data:

Inlet mass flow rate ($\dot{m}_{in}$): $50 \text{ kg/min}$

Exit mass flow rate ($\dot{m}_{out}$): $60 \text{ kg/min}$

Initial mass in the system ($m_{initial}$): $1000 \text{ kg}$

Final mass in the system ($m_{final}$): $500 \text{ kg}$


2. Determine the Rate of Change of Mass:

The continuity equation for an open system is:

$\dfrac{dm}{dt} = \dot{m}_{in} - \dot{m}_{out}$


Substituting the given values:

$\dfrac{dm}{dt} = 50 \text{ kg/min} - 60 \text{ kg/min} = -10 \text{ kg/min}$

This means the system is losing mass at a constant rate of $10 \text{ kg}$ every minute.


3. Calculate the Total Change in Mass:

$\Delta m = m_{final} - m_{initial}$

$\Delta m = 500 \text{ kg} - 1000 \text{ kg} = -500 \text{ kg}$


4. Solve for Time ($t$):

Since the flow rates are constant, the time can be found using the formula:

$\Delta m = \left( \dfrac{dm}{dt} \right) \times t$


Rearranging for $t$:

$t = \dfrac{\Delta m}{\dfrac{dm}{dt}}$

$t = \dfrac{-500 \text{ kg}}{-10 \text{ kg/min}}$

$t = 50 \text{ minutes}$

Answer:

The system mass will become $500 \text{ kg}$ after $50 \text{ minutes}$.

Question 2: Mass leaves an open system with a mass flow rate of $c \cdot m$, where $c$ is a constant and $m$ is the system mass. If the mass of the system at $t = 0$ is $m_0$, derive an expression for the mass of the system at time $t$.

Solution:

1. Conservation of Mass Principle:

For an open system, the rate of change of mass within the control volume is equal to the net mass flow rate across the boundary:

$\dfrac{dm}{dt} = \dot{m}_{in} - \dot{m}_{out}$

2. Identify Given Parameters:

Inlet mass flow rate ($\dot{m}_{in}$): $0$ (since mass only leaves the system)

Exit mass flow rate ($\dot{m}_{out}$): $c \cdot m$

Initial condition: At $t = 0$, $m = m_0$

3. Set up the Differential Equation:

Substituting the values into the continuity equation:

$\dfrac{dm}{dt} = 0 - (c \cdot m)$

$\dfrac{dm}{dt} = -c \cdot m$

4. Solve using Separation of Variables:

Rearrange the equation to group $m$ terms and $t$ terms:

$\dfrac{dm}{m} = -c \, dt$

5. Integrate Both Sides:

Integrate from the initial state ($t=0, m=m_0$) to an arbitrary state at time $t$:

$\int_{m_0}^{m} \dfrac{1}{m} \, dm = \int_{0}^{t} (-c) \, dt$

Calculating the integrals:

$[\ln(m)]_{m_0}^{m} = [-ct]_{0}^{t}$

$\ln(m) - \ln(m_0) = -ct$

6. Simplify the Expression:

Using logarithmic properties ($\ln a - \ln b = \ln \dfrac{a}{b}$):

$\ln\left(\dfrac{m}{m_0}\right) = -ct$

To solve for $m$, take the exponential ($e$) of both sides:

$\dfrac{m}{m_0} = e^{-ct}$

$m(t) = m_0 e^{-ct}$

Final Expression:

The mass of the system at any time $t$ is given by:

$m(t) = m_0 e^{-ct}$

This expression shows that the mass in the system decreases exponentially over time.

Question 3: Water enters a vertical cylindrical tank of cross-sectional area $0.01\text{ m}^2$ at a constant mass flow rate of $5\text{ kg/s}$. It leaves the tank through an exit near the base with a mass flow rate given by $0.2h\text{ kg/s}$, where $h$ is the instantaneous height in m. If the tank is empty initially, develop an expression for the liquid height $h$ as a function of time $t$. (Assume $\rho = 1000\text{ kg/m}^3$).

Solution:

1. Conservation of Mass:

The rate of change of mass in the tank is the difference between the inlet and outlet mass flow rates:

$\frac{dm}{dt} = \dot{m}_{in} - \dot{m}_{out}$

2. Express Mass ($m$) in terms of Height ($h$):

For a cylindrical tank: $m = \rho \cdot V = \rho \cdot A \cdot h$

Since $\rho$ and $A$ are constant, $\frac{dm}{dt} = \rho A \frac{dh}{dt}$.

3. Substitute Given Values:

$\dot{m}_{in} = 5$

$\dot{m}_{out} = 0.2h$

$\rho = 1000$

$A = 0.01$

The equation becomes:

$(1000 \cdot 0.01) \frac{dh}{dt} = 5 - 0.2h$

$10 \frac{dh}{dt} = 5 - 0.2h$

4. Separate Variables:

Divide both sides by $10$:

$\frac{dh}{dt} = 0.5 - 0.02h$

$\frac{dh}{0.5 - 0.02h} = dt$

5. Integrate:

Integrate from $t = 0$ (where $h = 0$ as the tank is empty) to time $t$:

$\int_{0}^{h} \frac{dh}{0.5 - 0.02h} = \int_{0}^{t} dt$

Using the integral rule $\int \frac{1}{a+bx} dx = \frac{1}{b}\ln(a+bx)$:

$\left[ \frac{\ln(0.5 - 0.02h)}{-0.02} \right]_{0}^{h} = t$

$\ln(0.5 - 0.02h) - \ln(0.5) = -0.02t$

6. Solve for $h$:

$\ln\left(\frac{0.5 - 0.02h}{0.5}\right) = -0.02t$

$\frac{0.5 - 0.02h}{0.5} = e^{-0.02t}$

$0.5 - 0.02h = 0.5e^{-0.02t}$

$0.02h = 0.5(1 - e^{-0.02t})$

$h(t) = 25(1 - e^{-0.02t})$

Final Expression:

The liquid height $h$ as a function of time $t$ is:

$h(t) = 25(1 - e^{-0.02t})$

Question 5:

Steam enters a mixing chamber at $100\text{ kPa}$, $20\text{ m/s}$, with a specific volume of $0.4\text{ m}^3/\text{kg}$. Liquid water at $100\text{ kPa}$ and $25^\circ\text{C}$ enters through a separate duct at $50\text{ kg/s}$ and $5\text{ m/s}$. Liquid water leaves at $100\text{ kPa}$ and $43^\circ\text{C}$ with a volumetric flow rate of $3.357\text{ m}^3/\text{min}$ and a velocity of $5.58\text{ m/s}$. Determine the port areas at the inlets and exit. (Assume $\rho_{liquid} = 1000\text{ kg/m}^3$ and steady state).

Solution:

1. Define State Points:

Inlet 1 (Steam): $P_1 = 100\text{ kPa}$, $V_1 = 20\text{ m/s}$, $v_1 = 0.4\text{ m}^3/\text{kg}$

Inlet 2 (Liquid Water): $\dot{m}_2 = 50\text{ kg/s}$, $V_2 = 5\text{ m/s}$, $\rho_2 = 1000\text{ kg/m}^3$

Exit 3 (Liquid Mixture): $\dot{Q}_3 = 3.357\text{ m}^3/\text{min}$, $V_3 = 5.58\text{ m/s}$, $\rho_3 = 1000\text{ kg/m}^3$

2. Calculate Exit Mass Flow Rate ($\dot{m}_3$):

First, convert the volumetric flow rate to $\text{m}^3/\text{s}$:

$\dot{Q}_3 = \dfrac{3.357}{60} = 0.05595\text{ m}^3/\text{s}$

Now, find the mass flow rate:

$\dot{m}_3 = \rho_3 \cdot \dot{Q}_3 = 1000 \cdot 0.05595 = 55.95\text{ kg/s}$

3. Find Steam Inlet Mass Flow Rate ($\dot{m}_1$):

Using the Conservation of Mass (Steady State):

$\dot{m}_1 + \dot{m}_2 = \dot{m}_3$

$\dot{m}_1 + 50 = 55.95 \implies \dot{m}_1 = 5.95\text{ kg/s}$

4. Calculate Port Areas ($A = \dfrac{\dot{m} \cdot v}{V}$ or $A = \dfrac{\dot{Q}}{V}$):

Area at Inlet 1 (Steam):

  • $A_1 = \dfrac{\dot{m}_1 \cdot v_1}{V_1} = \dfrac{5.95 \cdot 0.4}{20}$
  • $A_1 = 0.119\text{ m}^2$

Area at Inlet 2 (Liquid Water):

  • Specific volume $v_2 = \dfrac{1}{\rho} = \dfrac{1}{1000} = 0.001\text{ m}^3/\text{kg}$
  • $A_2 = \dfrac{\dot{m}_2 \cdot v_2}{V_2} = \dfrac{50 \cdot 0.001}{5}$
  • $A_2 = 0.01\text{ m}^2$

Area at Exit 3:

  • $A_3 = \dfrac{\dot{Q}_3}{V_3} = \dfrac{0.05595}{5.58}$
  • $A_3 = 0.01002\text{ m}^2$ (approximately $0.01\text{ m}^2$)

Final Results:

Port Area ($\text{m}^2$)
Inlet 1 (Steam) $0.119$
Inlet 2 (Water) $0.01$
Exit 3 (Mixture) $0.01$

Question 6:

Air is pumped into and withdrawn from a $10\text{ m}^3$ rigid tank. The conditions are:

Inlet: $v_1 = 2\text{ m}^3/\text{kg}$, $V_1 = 10\text{ m/s}$, $A_1 = 0.01\text{ m}^2$

Exit: $v_2 = 5\text{ m}^3/\text{kg}$, $V_2 = 5\text{ m/s}$, $A_2 = 0.015\text{ m}^2$

Assuming the tank is uniform at all times with $pv = 9.0\text{ kPa}\cdot\text{m}^3$, determine the rate of change of pressure in the tank.

Solution:

1. Conservation of Mass:

For the control volume (the tank):

$\dfrac{dm}{dt} = \dot{m}_{in} - \dot{m}_{out}$

2. Calculate Mass Flow Rates:

Inlet ($\dot{m}_{in}$):

$\dot{m}_1 = \dfrac{A_1 V_1}{v_1} = \dfrac{0.01 \cdot 10}{2} = 0.05\text{ kg/s}$

Exit ($\dot{m}_{out}$):

$\dot{m}_2 = \dfrac{A_2 V_2}{v_2} = \dfrac{0.015 \cdot 5}{5} = 0.015\text{ kg/s}$

3. Determine Rate of Change of Mass ($\dfrac{dm}{dt}$):

$\dfrac{dm}{dt} = 0.05 - 0.015 = 0.035\text{ kg/s}$

4. Relate Mass to Pressure:

The total mass in the tank is $m = \dfrac{\text{Volume}}{\text{specific volume}} = \dfrac{V}{v}$.

From the given relation $pv = 9.0$, we have $v = \dfrac{9.0}{p}$.

Substituting $v$ into the mass equation:

$m = \dfrac{V}{\left(\dfrac{9.0}{p}\right)} = \dfrac{V \cdot p}{9.0}$

Since the tank is rigid, Volume ($V = 10\text{ m}^3$) is constant:

$m = \dfrac{10}{9.0}p = \dfrac{10}{9}p$

5. Calculate Rate of Change of Pressure ($\dfrac{dp}{dt}$):

Differentiate the mass equation with respect to time:

$\dfrac{dm}{dt} = \dfrac{10}{9} \dfrac{dp}{dt}$

Substitute the value of $\dfrac{dm}{dt}$ calculated in step 3:

$0.035 = \dfrac{10}{9} \dfrac{dp}{dt}$

$\dfrac{dp}{dt} = \dfrac{0.035 \cdot 9}{10}$

$\dfrac{dp}{dt} = 0.0315\text{ kPa/s}$

Final Result:

The rate of change of pressure in the tank is $0.0315\text{ kPa/s}$. Since the value is positive, the pressure in the tank is increasing.

Question 7:

A gas flows steadily through a circular duct of varying cross-section area with a mass flow rate of $10 \text{ kg/s}$. The inlet and exit conditions are as follows:

Inlet: $V_1 = 400 \text{ m/s}$, $A_1 = 179.36 \text{ cm}^2$

Exit: $V_2 = 584 \text{ m/s}$, $v_2 = 1.1827 \text{ m}^3/\text{kg}$

  • (a) Determine the exit area.
  • (b) Do you find the increase in velocity of the gas accompanied by an increase in flow area counter-intuitive? Why?

Solution:

Part (a): Determine the exit area

1. Identify Given Data:

Mass flow rate ($\dot{m}$): $10 \text{ kg/s}$ (Constant for steady flow)

Exit Velocity ($V_2$): $584 \text{ m/s}$

Exit Specific Volume ($v_2$): $1.1827 \text{ m}^3/\text{kg}$

2. Use the Mass Flow Rate Equation:

The formula for mass flow rate is:

$\dot{m} = \frac{A_2 V_2}{v_2}$

3. Rearrange to solve for Exit Area ($A_2$):

$A_2 = \frac{\dot{m} \cdot v_2}{V_2}$

4. Substitute the values:

$A_2 = \frac{10 \cdot 1.1827}{584}$

$A_2 = \frac{11.827}{584}$

$A_2 \approx 0.02025 \text{ m}^2$

5. Convert to $\text{cm}^2$ (for comparison with inlet):

$A_2 = 0.02025 \times 10,000 = 202.5 \text{ cm}^2$

Part (b): Discussion on Intuition

Is it counter-intuitive?

At first glance, yes. Usually, we expect a fluid to speed up when the duct narrows (like a nozzle). Here, the velocity increased ($400 \rightarrow 584 \text{ m/s}$), but the area also increased ($179.36 \rightarrow 202.5 \text{ cm}^2$).

Why does this happen?

This occurs because the fluid is a compressible gas.

In incompressible flow (like water), $A_1V_1 = A_2V_2$. If $V$ goes up, $A$ must go down.

In compressible flow, the density ($\rho$) or specific volume ($v$) changes significantly.

In this specific case, the gas expanded so much (its specific volume increased) that the duct had to widen just to let the higher-volume flow pass through, even though it was moving faster. This is typical of supersonic flow in a divergent section or high-magnitude expansion.

Final Results:

Exit Area ($A_2$): $202.5 \text{ cm}^2$

Reasoning: The increase in area despite increased velocity is due to the significant increase in the gas's specific volume (expansion).

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