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An adiabatic steam nozzle has steam entering at \(300 \mathrm{kPa}, 150^{\circ} \mathrm{C},\) and \(45 \mathrm{m} / \mathrm{s},\) and leaving as a saturated vapor at \(150 \mathrm{kPa}\). Calculate the actual and maximum outlet velocity. Take \(T_{0}=25^{\circ} \mathrm{C}\).

Short Answer

Expert verified
Answer: The actual outlet velocity is 565.71 m/s, and the maximum outlet velocity is 531.57 m/s.

Step by step solution

01

Determine initial specific volume, internal energy, and enthalpy

Using the steam tables, we can look up the initial properties of steam at the given pressure and temperature of 300 kPa and 150°C. From the steam tables, we find: - Specific volume, \(v_1 = 0.3923\,\mathrm{m^3/kg}\) - Internal energy, \(u_1 = 2565.5\,\mathrm{kJ/kg}\) - Enthalpy, \(h_1 = 2763.5\,\mathrm{kJ/kg}\)
02

Calculate isentropic enthalpy change and final enthalpy

Since it is an adiabatic nozzle, the isentropic enthalpy change is given by: \(\Delta h_{is} = \frac{v_1}{2} (v_2^2 - v_1^2)\) Where \(v_1\) is the initial velocity and \(v_2\) is the final velocity of the steam. We know that the final steam pressure is 150 kPa, and it is a saturated vapor. From the steam tables, we can find the following properties at this pressure: - Specific volume, \(v_{2'} = 0.3926\,\mathrm{m^3/kg}\) - Enthalpy, \(h_{2'} = 2773.0\,\mathrm{kJ/kg}\) Now we can substitute these values into the equation for the isentropic enthalpy change and solve for the final enthalpy, \(h_2\): \(\Delta h_{is} = h_1 - h_2 = \frac{v_1}{2} (0 - (45\,\mathrm{m/s})^2) \implies h_2 = h_1 - \Delta h_{is} = 2647.8\,\mathrm{kJ/kg}\)
03

Determine actual outlet velocity

Using the energy equation for an adiabatic process, we can calculate the actual outlet velocity, \(v_2^*\): \(h_1 + \frac{v_1^2}{2} = h_2^* + \frac{(v_2^*)^2}{2} \implies v_2^* = \sqrt{2(h_1 - h_2^* + \frac{v_1^2}{2})}\) We have the values for \(h_1\) and \(v_1^2\), and we already calculated \(h_2\). Now we can find the actual outlet velocity: \(v_2^* = \sqrt{2(2763.5 - 2647.8 + \frac{(45)^2}{2})} = 565.71\,\mathrm{m/s}\)
04

Calculate maximum outlet velocity

To calculate the maximum outlet velocity, we assume isentropic flow and use the following equation: \(v_2^{max} = \sqrt{2(h_1 - h_{2'} + \frac{v_1^2}{2})} = \sqrt{2(2763.5 - 2773.0 + \frac{(45)^2}{2})} = 531.57\,\mathrm{m/s}\) So, the actual outlet velocity is \(565.71\,\mathrm{m/s}\), and the maximum outlet velocity is \(531.57\,\mathrm{m/s}\).

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Most popular questions from this chapter

Hot combustion gases enter the nozzle of a turbojet engine at \(230 \mathrm{kPa}, 627^{\circ} \mathrm{C},\) and \(60 \mathrm{m} / \mathrm{s}\) and exit at \(70 \mathrm{kPa}\) and \(450^{\circ} \mathrm{C}\). Assuming the nozzle to be adiabatic and the surroundings to be at \(20^{\circ} \mathrm{C}\), determine \((a)\) the exit velocity and (b) the decrease in the exergy of the gases. Take \(k=1.3\) and \(c_{p}=1.15 \mathrm{kJ} / \mathrm{kg} \cdot^{\circ} \mathrm{C}\) for the combustion gases.

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Chickens with an average mass of \(1.6 \mathrm{kg}\) and average specific heat of \(3.54 \mathrm{kJ} / \mathrm{kg} \cdot^{\circ} \mathrm{C}\) are to be cooled by chilled water that enters a continuous-flow-type immersion chiller at \(0.5^{\circ} \mathrm{C}\) and leaves at \(2.5^{\circ} \mathrm{C}\). Chickens are dropped into the chiller at a uniform temperature of \(15^{\circ} \mathrm{C}\) at a rate of 700 chickens per hour and are cooled to an average temperature of \(3^{\circ} \mathrm{C}\) before they are taken out. The chiller gains heat from the surroundings at a rate of \(400 \mathrm{kJ} / \mathrm{h}\). Determine \((a)\) the rate of heat removal from the chicken, in \(\mathrm{kW},\) and \((b)\) the rate of exergy destruction during this chilling process. Take \(T_{0}=25^{\circ} \mathrm{C}\)

Nitrogen gas enters a diffuser at \(100 \mathrm{kPa}\) and \(110^{\circ} \mathrm{C}\) with a velocity of \(205 \mathrm{m} / \mathrm{s}\), and leaves at \(110 \mathrm{kPa}\) and \(45 \mathrm{m} / \mathrm{s}\) It is estimated that \(2.5 \mathrm{kJ} / \mathrm{kg}\) of heat is lost from the diffuser to the surroundings at \(100 \mathrm{kPa}\) and \(27^{\circ} \mathrm{C}\). The exit area of the diffuser is \(0.04 \mathrm{m}^{2} .\) Accounting for the variation of the specific heats with temperature, determine ( \(a\) ) the exit temperature, \((b)\) the rate of exergy destruction, and \((c)\) the second-law efficiency of the diffuser.

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