Air steadily enters the diffuser section of a jet engine at a velocity of 270 m/s...
Air steadily enters the diffuser section of a jet engine at a
velocity of 270 m/s at 85 kPa and at 250 °C.
There is heat addition from the diffuser walls to the air.
The air exits the diffuser at 1/3 of its inlet velocity.
The heat addition per kg air entering the diffuser is 13
kJ/kg.
What is the change in the specific enthalpy of the air (kJ/kg)?
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Air steadily enters the diffuser section of a jet engine at a
velocity of 270 m/s...
Air at 10 degree C and 80 kPa enters the diffuser of a jet engine steadily...
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....
Air at 10°C and 80 kPa (static values) enters the diffuser of a jet engine steadily...
Air at 10°C and 80 kPa (static values) enters the diffuser of a jet engine steadily with a velocity of 200 m/s. The inlet area of the diffuser is 0.4 m2. The air leaves the diffuser with a velocity of 40 m/s. Calculate 1) air density 2) air mass flow 3) inlet stagnation temprature 4) Inlet stgnation enthelpy 5) Outlet static temprature T2 a. 0.98 kg/m3 b. 1.01 kq/m3 c. 1.33 kg/m3 d. 90.1 kg/s e. 88.3 kg/m3 78.8 kg/m3...
The diffuser in a jet engine is designed to decrease the kinetic energy of the air...
The diffuser in a jet engine is designed to decrease the kinetic energy of the air entering the engine compressor without any work or heat interactions. Calculate the velocity at the exit of a diffuser when air at 100 kPa and 30°C enters it with a velocity of 358 m/s and the exit state is 200 kPa and 90°C. The specific heat of air at the average temperature of 60°C = 333 K is cp = 1.007 kJ/kg·K.
Problem-2 (200) Air at 30 kPa, 200 K, and 250 m/s enters a turbojet engine in...
Problem-2 (200) Air at 30 kPa, 200 K, and 250 m/s enters a turbojet engine in flight. The air mass flow rate is 28 kg/s. The compressor pressure ratio is 13, the turbine inlet temperature is 1460 K, and air exits the nozzle at 30 kPa. The diffuser and nozzle processes are isentropic, the compressor and turbine have isentropic efficiencies of 81% and 88%, respectively, and there is no pressure drop for flow through the combustor. Kinetic energy is negligible...
The diffuser in a jet engine is designed to decrease the kinetic energy of the air entering the j...
The diffuser in a jet engine is designed to decrease the kinetic energy of the air entering the jet engine compressor without any work or heat interactions. Following information is recorded; Entering diffuser Velocity = 500 ms Pressure 100 kPa Temperature 20°0 The exit of a diffuser Velocity- 329.55 m/s Pressure 200 kPa Temperature- 90°0 The molecular mass of air = 28.96 kg/kmol Note for air, Cp/R-A+BT+CT2+DT2 ET3 with T in Kelvin Name Air B*103 0.575 D*10-5 0.016 C*106 E*109...
Q.4 Air at 26 kPa,230 K, and 220 m/s enters a turbojet engine in flight as...
Q.4 Air at 26 kPa,230 K, and 220 m/s enters a turbojet engine in flight as shown below. The mass flow rate of air is 25 kg/s, the compression pressure ratio is 11, inlet temperature to the turbine is 1400 K, and air exits the nozzle at 26 kPa. The diffuser and nozzle processes are isentropic, but the compressor and turbine have isentropic efficiencies of 85 and 90 percent, respectively and there is no pressure drop for flow through the...
Air enters a diffuser at 102 KPa , 57 Celcius , and 285 m/s and exits...
Air enters a diffuser at 102 KPa , 57 Celcius , and 285 m/s and exits at 303 kPa , 10 Celcius , and 12 m/s. The area of the inlet of the diffuser is 97 cm2. Find the mass flow rate of air (kg/s), find the area of the exit of the diffuser (cm2), find the average heat transfer time rate (kW)
Air enters a diffuser at 102 KPa , 57 Celcius , and 285 m/s and exits...
Air enters a diffuser at 102 KPa , 57 Celcius , and 285 m/s and exits at 303 KPa , 10 Celcius , and 12 m/s. The area of the inlet of the diffuser is 97 cm2. Find the mass flow rate of air (kg/s), find the area of the exit of the diffuser (cm2), find the average heat transfer time rate (kW)
Air enters a diffuser at 102 KPa , 57 Celcius , and 285 m/s and exits...
Air enters a diffuser at 102 KPa , 57 Celcius , and 285 m/s and exits at 303 KPa , 10 Celcius , and 12 m/s. The area of the inlet of the diffuser is 97 cm2. Find the mass flow rate of air (kg/s), find the area of the exit of the diffuser (cm2), find the average heat transfer time rate (kW)
Air enters a diffuser at 102 KPa , 57 Celcius , and 285 m/s and exits...
Air enters a diffuser at 102 KPa , 57 Celcius , and 285 m/s and exits at 303 KPa , 10 Celcius , and 12 m/s. The area of the inlet of the diffuser is 97 cm2. Find the mass flow rate of air (kg/s), find the area of the exit of the diffuser (cm2), find the average heat transfer time rate (kW)
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....
Air at 10°C and 80 kPa (static values) enters the diffuser of a jet engine steadily with a velocity of 200 m/s. The inlet area of the diffuser is 0.4 m2. The air leaves the diffuser with a velocity of 40 m/s. Calculate 1) air density 2) air mass flow 3) inlet stagnation temprature 4) Inlet stgnation enthelpy 5) Outlet static temprature T2 a. 0.98 kg/m3 b. 1.01 kq/m3 c. 1.33 kg/m3 d. 90.1 kg/s e. 88.3 kg/m3 78.8 kg/m3...
Problem-2 (200) Air at 30 kPa, 200 K, and 250 m/s enters a turbojet engine in flight. The air mass flow rate is 28 kg/s. The compressor pressure ratio is 13, the turbine inlet temperature is 1460 K, and air exits the nozzle at 30 kPa. The diffuser and nozzle processes are isentropic, the compressor and turbine have isentropic efficiencies of 81% and 88%, respectively, and there is no pressure drop for flow through the combustor. Kinetic energy is negligible...
The diffuser in a jet engine is designed to decrease the kinetic energy of the air entering the jet engine compressor without any work or heat interactions. Following information is recorded; Entering diffuser Velocity = 500 ms Pressure 100 kPa Temperature 20°0 The exit of a diffuser Velocity- 329.55 m/s Pressure 200 kPa Temperature- 90°0 The molecular mass of air = 28.96 kg/kmol Note for air, Cp/R-A+BT+CT2+DT2 ET3 with T in Kelvin Name Air B*103 0.575 D*10-5 0.016 C*106 E*109...
Q.4 Air at 26 kPa,230 K, and 220 m/s enters a turbojet engine in flight as shown below. The mass flow rate of air is 25 kg/s, the compression pressure ratio is 11, inlet temperature to the turbine is 1400 K, and air exits the nozzle at 26 kPa. The diffuser and nozzle processes are isentropic, but the compressor and turbine have isentropic efficiencies of 85 and 90 percent, respectively and there is no pressure drop for flow through the...
Air enters a diffuser at 102 KPa , 57 Celcius , and 285 m/s and exits at 303 kPa , 10 Celcius , and 12 m/s. The area of the inlet of the diffuser is 97 cm2. Find the mass flow rate of air (kg/s), find the area of the exit of the diffuser (cm2), find the average heat transfer time rate (kW)
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