
a)
The mass flow rate of the steam.
a)

Explanation of Solution
Given:
The initial pressure of the steam
The initial temperature of the steam
The initial velocity
The final pressure of the steam
The final velocity
The power output of the turbine
The isentropic efficiency
Conclusion:
Refer the Table A-6, “superheated water table”, obtain the following properties at a pressure of
The initial enthalpy
The initial entropy
The entropy remains constant since the process is isentropic
Refer the Table A-6, “superheated water table”, obtain the following properties at a pressure of
The enthalpy at final state in isentropic process
Calculate the power output for the isentropic process.
Write the expression for the energy balance equation for closed system.
Here, rate of net energy transfer in to the control volume is
The rate of change in internal energy of the system is zero at steady state.
Substitute
Thus, the mass flow rate of the steam is
b)
The exit temperature of the steam.
b)

Explanation of Solution
Write the expression to calculate the mass flow rate of the steam.
Refer the Table A-6, “superheated water table”, obtain final entropy at pressure of
Refer the Table A-6, “Superheated water”, obtain the value of exit temperature
Show exit temperature and enthalpy values from the Table A-6.
Temperature | Enthalpy |
2675 | 100 |
2683.5 | ? |
2776.6 | 150 |
Write the formula of interpolation method of two variables.
Here, the variables denoted by x and y are exit temperature and enthalpy.
Substitute
The value of exit temperature
Thus, the exit temperature of the steam is
c)
The entropy generation in the turbine.
c)

Explanation of Solution
Calculate the entropy generation in the turbine
Thus, the entropy generation in the turbine is
Want to see more full solutions like this?
Chapter 8 Solutions
Fundamentals of Thermal-Fluid Sciences
- 0.36 m Problem 2.27 P=5kN D Each of the links AB and CD is made of aluminum (E=75 GPa) and has a cross-sectional area of 125 mm². Knowing that they support the rigid member BC, determine the deflection of point E. B E 0.44 m 0.20 marrow_forward(read image) (Answer Given)arrow_forward(read image) Answer: A = 1192 Narrow_forward
- The correct answer is ~168 MPa, how was this found?arrow_forwardAir enters the compressor of a regenerative gas turbine engine at 310 K and 100 kPa, where it is compressed to 900 kPa and 650 K. The regenerator has an effectiveness of 75%, and the air enters the turbine at 1400 K. Assume variable specific heats for air. For a turbine efficiency of 90 percent, determine the amount of heat transfer in the regenerator. The amount of heat transfer in the regenerator is kJ/kg.arrow_forwardAir enters the compressor of a regenerative gas turbine engine at 310 K and 100 kPa, where it is compressed to 900 kPa and 650 K. The regenerator has an effectiveness of 79 percent, and the air enters the turbine at 1400 K. Assume constant specific heats for air at room temperature. The properties of air at room temperature are cp = 1.005 kJ/kg·K and k = 1.4. For a turbine efficiency of 90 percent, determine the amount of heat transfer in the regenerator. The amount of heat transfer in the regenerator is kJ/kg.arrow_forward
- Hints: Find the closed loop transfer function and then plot the step response for diFerentvalues of K in MATLAB. Show step response plot for different values of K. Auto Controls Show solutions and provide matlab code NO COPIED ANSWERS OR WILL REPORT!!!! Use own solutionarrow_forwardwhat is shear stress and normal? how to tell them while calculating?arrow_forward12 mm 45 mm 20 kN 20 kN 12 mm 45 mm PROBLEM 1.61 For the assembly and loading of Problem 1.60, determine (a) the average shearing stress in the pin at C, (b) the average bearing stress at C in member BC, (c) the average bearing stress at B in member BC. PROBLEM 1.60 Two horizontal 20-kN forces are applied to pin B of the assembly shown. Knowing that a pin of 20-mm diameter is used at each connection, determine the maximum value of the average normal stress (a) in link AB, (b) in link BC.arrow_forward
- Elements Of ElectromagneticsMechanical EngineeringISBN:9780190698614Author:Sadiku, Matthew N. O.Publisher:Oxford University PressMechanics of Materials (10th Edition)Mechanical EngineeringISBN:9780134319650Author:Russell C. HibbelerPublisher:PEARSONThermodynamics: An Engineering ApproachMechanical EngineeringISBN:9781259822674Author:Yunus A. Cengel Dr., Michael A. BolesPublisher:McGraw-Hill Education
- Control Systems EngineeringMechanical EngineeringISBN:9781118170519Author:Norman S. NisePublisher:WILEYMechanics of Materials (MindTap Course List)Mechanical EngineeringISBN:9781337093347Author:Barry J. Goodno, James M. GerePublisher:Cengage LearningEngineering Mechanics: StaticsMechanical EngineeringISBN:9781118807330Author:James L. Meriam, L. G. Kraige, J. N. BoltonPublisher:WILEY





