THERMO:
QUESTION 5
Saturated water vapor at 12.92 bar enters an insulated throttling valve which drops the pressure to 1.50 bar. Determine the temperature (oC) of the steam at the exit of the valve.
Note: Give your answer to two decimal places.
QUESTION 6
Air enters an adiabatic diffuser at 320 K and 100 kPa with a velocity of 665.4 m/s. At the diffuser exit, the temperature is 520 K. Determine the velocity (m/s) at the exit of the diffuser. Use the tables for air as an ideal gas.
Note: Give your answer to two decimal places.
QUESTION 7
Air flow of 2.43 kg/s enters a diffuser at 240 K and 40 kPa with a velocity of 594.7 m/s. At the diffuser exit, the temperature is 380 K. Heat transfer from the diffuser to the surroundings occurs at a rate of 5.3 kW. Determine the velocity (m/s) at the exit of the diffuser. Use the tables for air as an ideal gas.
Note: Give your answer to two decimal places.
QUESTION 8
Steam enters an adiabatic nozzle at 4000 kPa, 440oC, with a velocity of 75 m/s. At the exit, the pressure and velocity are 1800 kPa and 635 m/s, respectively. Determine the area (m2) at the exit of the nozzle if the mass flow rate is 1.41 kg/s.
Note: Give your answer to six decimal places.
THERMO: QUESTION 5 Saturated water vapor at 12.92 bar enters an insulated throttling valve which drops...
Steam enters a well-insulated throttling valve (treat the process as adiabatic) at a mass flow rate of m=15 kg/min with an initial pressure of Pi= 550 kPa and initial temperature Ti= 200ºC and exits at a pressure of Pf= 200 kPa. What is the temperature of the steam upon exiting the valve?
5-30 Air enters an adiabatic nozzle steadily at 300 kPa, 200°C, and 30 m/s and leaves at 100 kPa and 180 m/s. The inlet area of the nozzle is 80 cm². Determine (a) the mass flow rate through the nozzle, (b) the exit temperature of the air, and (c) the exit area of the nozzle. Answers: (a) 0.5304 kg/s, (b) 184.6°C, (c) 38.7 cm P = 300 kPa T, = 200°C Vi = 30 m/s A = 80 cm AIR...
Steam enters a well-insulated nozzle at 10 bar and 200ºC. It exits as saturated vapor at 100 kPa. The mass flow rate is 1 kg/s. What is the steady-state exit velocity? What is the outlet cross-sectional area?
Thermo one Question 5 A steam turbine generates energy in the form of work at the rate of 346.1 kJ/kg of steam. The steam at the inlet of the turbine is at 8 MPa, 480oC, and at a velocity of 163.5 m/s. The steam exits the turbine at 2 MPa, 240oC, and a velocity of 55.3 m/s. Heat transfer to the surroundings occurs where the outer surface (boundary) temperature is at 333.5oC. Determine the rate of entropy production (kJ/kg-K) within...
You will need to use steam tables to answer this question and please show steps on how to solve. 3) An insulated throttling valve is connected to a steam line at 300 kPa. If the pressure and temperature after the throttling valve are 100 kPa and 150°C, what is the dryness fraction in the steam line? 3) An insulated throttling valve is connected to a steam line at 300 kPa. If the pressure and temperature after the throttling valve are...
Air at 10 degree C and 80 kPa enters the diffuser of a jet engine steadily with a velocity of 200 m/s. The inlet area of the diffuser is 0.4 m^2.The air leaves the diffuser with a velocity that is very small compared with the inlet velocity. Determine the mass flow rate of the air and the temperature of the air leaving the diffuser. Air at 100 kPa and 280 K is compressed steadily to 600 kPa and 400 K....
PLEASE answer all questions clearly Problem 6.109 SI As shown in the figure below, air enters the diffuser of a jet engine at 18 kPa, Ti 250 K with a velocity of V1 = 201 m/s, all data corresponding to high-altitude flight. The air flows adiabatically through the diffuser, decelerating to a velocity of 50 m/s at the diffuser exit. DiffuserCompressor Combustors Giurbine -Nozzle P1-18 kPa Ti,V V2-50 m/s Air Product in gases out Assume steady-state operation, the ideal gas...
2. Air enters an adiabatic nozzle with a pressure, temperature, and velocity of 900 kPa 500°C, and 2.8 m/s, respectively. The air leaves the nozzle at 850 kPa and 480°C. What is the velocity at the exit of the nozzle? Ans 208.949 m/s 2. Air enters an adiabatic nozzle with a pressure, temperature, and velocity of 900 kPa 500°C, and 2.8 m/s, respectively. The air leaves the nozzle at 850 kPa and 480°C. What is the velocity at the exit...
Water vapor enters a diffuser at a pressure of 0.7 bar, a temperature of 160°C, and a velocity of 180 m/s. The inlet to the diffuser is 100 cm The exit conditions from the diffuser are: velocity of 60 m/s and pressure of 1.0 bar. During the passage of the water vapor through the diffuser, there is heat transfer to the surroundings of 0.6 kJ/kg. Determine (a) the final temperature. (b) the mass flow rate in kg/s, and (c) the...
Required information NOTE: This is a multi-part question. Once an answer is submitted, you will be unable to return to this part. Air at 80 kPa and 127°C enters an adiabatic diffuser steadily at a rate of 5400 kg/h and leaves at 100 kPa. The velocity of the airstream is decreased from 230 m/s to 30 m/s as it passes through the diffuser. The gas constant of air is 0.287 kPa·m3/kg·K. The enthalpy of air at the inlet temperature of...