Air flows steadily at the rate of 1 kg/s through an air compressor at 10 m/s, 100 kPa and 1 m3/kg and leaving at 6 m/s, 800 kPa and 0.2 m3/kg. The internal energy of the air leaving is 100 kJ/kg greater than the air entering. Cooling water in the compressor jacket absorbs heat from air at the rate of 100 kW. Find the rate of work done.
260 kW
This problem involves the application of the First Law of Thermodynamics for a steady-flow open system, specifically an air compressor. We need to determine the rate of work done on the air as it passes through the compressor. The steady-flow energy equation will be our primary tool, considering changes in enthalpy, kinetic energy, and heat transfer.
Let's list the properties of the air at the inlet (state 1) and outlet (state 2) of the air compressor, along with the mass flow rate and heat transfer rate:
| Parameter | Symbol | Value (Inlet, 1) | Value (Outlet, 2) |
|---|---|---|---|
| Mass flow rate | \(\dot{m}\) | 1 kg/s | |
| Velocity | \(V\) | 10 m/s | 6 m/s |
| Pressure | \(P\) | 100 kPa | 800 kPa |
| Specific Volume | \(v\) | 1 m3/kg | 0.2 m3/kg |
| Internal Energy Change | \((u_2 - u_1)\) | 100 kJ/kg | |
| Heat Absorbed by Cooling Water (from air) | \(\dot{Q}_{out}\) | 100 kW | |
Since heat is absorbed by cooling water from the air, it means heat is rejected from the air (our system). Therefore, the heat transfer rate for the air compressor is negative: \(\dot{Q} = -100 \text{ kW}\).
For a steady-flow system like an air compressor, the First Law of Thermodynamics (Steady-Flow Energy Equation) is given by:
\[ \dot{Q} - \dot{W} = \dot{m} \left[ (h_2 - h_1) + \frac{(V_2^2 - V_1^2)}{2} + g(z_2 - z_1) \right] \]
Where:
For a horizontal air compressor, the change in potential energy is negligible, so \((z_2 - z_1) = 0\).
The equation simplifies to:
\[ \dot{Q} - \dot{W} = \dot{m} \left[ (h_2 - h_1) + \frac{(V_2^2 - V_1^2)}{2} \right] \]
The specific enthalpy (\(h\)) is related to specific internal energy (\(u\)), pressure (\(P\)), and specific volume (\(v\)) by the equation: \(h = u + Pv\).
Therefore, the change in specific enthalpy is:
\[ (h_2 - h_1) = (u_2 - u_1) + (P_2 v_2 - P_1 v_1) \]
Let's calculate the \(Pv\) terms:
Now, substitute these values and the given internal energy change into the enthalpy change equation:
\[ (h_2 - h_1) = 100 \text{ kJ/kg} + (160 \text{ kJ/kg} - 100 \text{ kJ/kg}) \]
\[ (h_2 - h_1) = 100 \text{ kJ/kg} + 60 \text{ kJ/kg} = 160 \text{ kJ/kg} \]
The change in specific kinetic energy is:
\[ \frac{(V_2^2 - V_1^2)}{2} = \frac{(6 \text{ m/s})^2 - (10 \text{ m/s})^2}{2} \]
\[ \frac{(V_2^2 - V_1^2)}{2} = \frac{36 \text{ m}^2/\text{s}^2 - 100 \text{ m}^2/\text{s}^2}{2} \]
\[ \frac{(V_2^2 - V_1^2)}{2} = \frac{-64 \text{ m}^2/\text{s}^2}{2} = -32 \text{ m}^2/\text{s}^2 \]
Since \(1 \text{ J/kg} = 1 \text{ m}^2/\text{s}^2\), we have \(-32 \text{ J/kg}\). To convert to kJ/kg:
\[ \frac{(V_2^2 - V_1^2)}{2} = -32 \text{ J/kg} \times \frac{1 \text{ kJ}}{1000 \text{ J}} = -0.032 \text{ kJ/kg} \]
Now, we substitute all calculated values and given parameters into the simplified steady-flow energy equation:
\[ \dot{Q} - \dot{W} = \dot{m} \left[ (h_2 - h_1) + \frac{(V_2^2 - V_1^2)}{2} \right] \]
Given: \(\dot{m} = 1 \text{ kg/s}\) and \(\dot{Q} = -100 \text{ kW}\).
\[ -100 \text{ kW} - \dot{W} = (1 \text{ kg/s}) \left[ 160 \text{ kJ/kg} + (-0.032 \text{ kJ/kg}) \right] \]
\[ -100 \text{ kW} - \dot{W} = (1 \text{ kg/s}) \left[ 159.968 \text{ kJ/kg} \right] \]
\[ -100 \text{ kW} - \dot{W} = 159.968 \text{ kW} \]
Now, solve for \(\dot{W}\):
\[ -\dot{W} = 159.968 \text{ kW} + 100 \text{ kW} \]
\[ -\dot{W} = 259.968 \text{ kW} \]
\[ \dot{W} = -259.968 \text{ kW} \]
The negative sign indicates that work is done on the air (the system), which is expected for an air compressor. The magnitude of the rate of work done is approximately 260 kW.
Comparing this result with the given options, 260 kW matches one of the choices.
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