Question

Nitrogen gas at 50 kPa and 7°C enters an adiabatic diffuser steadily with a velocity of...

Nitrogen gas at 50 kPa and 7°C enters an adiabatic diffuser steadily with a velocity of 180 m/s and leaves at 109 kPa and 22°C. Determine (a) the exit velocity of the nitrogen and (b) the ratio of the inlet to exit area A1/A2

Homework Answers

Know the answer?
Your Answer:

Post as a guest

Your Name:

What's your source?

Earn Coins

Coins can be redeemed for fabulous gifts.

Not the answer you're looking for?
Ask your own homework help question
Similar Questions
Nitrogen gas at 60 kPa and 78C enters an adiabatic diffuser steadily with a velocity of...
Nitrogen gas at 60 kPa and 78C enters an adiabatic diffuser steadily with a velocity of 275 m/s and leaves at 85 kPa and 278C. Determine (a) the exit velocity of the nitrogen and (b) the ratio of the inlet to exit area A1/A2. Reconsider Using EES (or other) software, investigate the effect of the inlet veloc- ity on the exit velocity and the ratio of the inlet-to-exit area. Let the inlet velocity vary from 210 to 350 m/s. Plot...
Refrigerant-134a enters a diffuser steadily as saturated vapour at 600 kPa with a velocity of 160...
Refrigerant-134a enters a diffuser steadily as saturated vapour at 600 kPa with a velocity of 160 m/s, and it leaves at 700 kPa and 40°C. The refrigerant is gaining heat at a rate of 2 kJ/s as it passes through the diffuser : determine (a- the exit velocity (b- the mass flow rate of the refrigerant. If the exit area is twice the inlet area (A2=2A1),
Air at 10º C and 80kPa enters the diffuser of a jet engine steadily with a...
Air at 10º C and 80kPa enters the diffuser of a jet engine steadily with a velocity of. 200 m/s. The inlet area of the diffuser is 0.5 m. 2 . The air leaves the diffuser with a velocity that is very small compared with the inlet velocity. Determine a).the mass flow rate of the air b).the temperature of the air leaving the diffuser.
Steam enters a diffuser at 250°C and 300kPa with an inlet velocity of 402 m/s. Steam...
Steam enters a diffuser at 250°C and 300kPa with an inlet velocity of 402 m/s. Steam leaves the diffuser at 350°C and 600kPa. The heat gain in the diffuser is 80 kW. The inlet area of the diffuser is 820 cm2. Determine the velocity and the volume flow rate of the steam at the diffuser exit.
An unknown ideal gas enters a 25 cm-diameter pipe steadily at 250 kPa and 47C with...
An unknown ideal gas enters a 25 cm-diameter pipe steadily at 250 kPa and 47C with a velocity of 5 m/s. The ideal gas gains heat as it flows and leaves the pipe at 77C and 225 kPa. The gas constant of the ideal gas is R=0.285 kJ/kg.K. Determine: a) the volume flow rate at the inlet b) the mass flow rate c) the velocity at the exit
A turboprop engine consists of a diffuser, compressor, combustor, turbine, and nozzle. The turbine drives a...
A turboprop engine consists of a diffuser, compressor, combustor, turbine, and nozzle. The turbine drives a propeller as well as the compressor. Air enters the diffuser with a volumetric flow rate of 63.7 m3/s at 40 kPa, 240 K, and a velocity of 180 m/s, and decelerates essentially to zero velocity. The compressor pressure ratio is 10 and the compressor has an isentropic efficiency of 85%. The turbine inlet temperature is 1240 K, and its isentropic efficiency is 85%. The...
1.      Air enters a converging-diverging nozzle with a total pressure of 1100 kPa and a total...
1.      Air enters a converging-diverging nozzle with a total pressure of 1100 kPa and a total temperature of 127°C. The exit area to throat area ratio is 1.8. The throat area is 5 cm2. The velocity at the throat is sonic and the diverging section acts as a nozzle. The diverging section is now acts as a supersonic nozzle. Assume that a normal shock stands in the exit plane of the nozzle. Determine the following: a.       The static pressure and...
Steam enters an adiabatic turbine at 140 bar and 560 C and leaves at 10 kPa....
Steam enters an adiabatic turbine at 140 bar and 560 C and leaves at 10 kPa. At the exit, the pressure and quality are 50 KPa and .90, respectively. Determine the power produced (kW) by the turbine if the mass flow rate is 1.63 kg/s.
Air enters the diffuser of a jet engine operating at a steady state at a pressure...
Air enters the diffuser of a jet engine operating at a steady state at a pressure of 18 kPa, a temperature of 213 K and a velocity of 285 m/s. The air flows adiabatically through the diffuser and exits at a temperature of 240 K. Using the ideal gas model for the air, please determine the velocity of the air at the diffuser exit, in m/s.
Question 1 Steam enters a nozzle at 300 kPa and 700ºC with a velocity of 20...
Question 1 Steam enters a nozzle at 300 kPa and 700ºC with a velocity of 20 m/s. The nozzle exit pressure is 200 kPa. Assuming this process is reversible and adiabatic, determine (a) the exit temperature and (b) the exit velocity.
ADVERTISEMENT
Need Online Homework Help?

Get Answers For Free
Most questions answered within 1 hours.

Ask a Question
ADVERTISEMENT