Air at 12.7psia and 72oF enters an adiabatic diffuser steadily with a velocity of 775 ft/s...
Air at 12.7psia and 72oF enters an adiabatic diffuser steadily with a velocity of 775 ft/s and leaves with a low velocity at a pressure of 14.2 psia. The exit area of the diffuser is 3 times in the inlet area. Determine (a) the exit temperature and (b) the exit velocity of the air.
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Air at 12.7psia and 72oF enters an adiabatic diffuser
steadily with a velocity of 775 ft/s...
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Air at 0.8 bar and 127 Centers an adiabatic diffuser steadily at a rate of 6000 kg/ h and leaves at 1 bar. The velocity of the air stream is decreased from 230 m/st 0 30 m/s as it passes through the diffuser. Find (a) the exit temperature of the ai rand (b) the exit area of the diffuser.
Air at 0.8 bar and 127 Centers an adiabatic diffuser steadily at a rate of 6000...
Air at 0.8 bar and 127 Centers an adiabatic diffuser steadily at a rate of 6000 kg/ h and leaves at 1 bar. The velocity of the air stream is decreased from 230 m/st 0 30 m/s as it passes through the diffuser. Find (a) the exit temperature of the ai rand (b) the exit area of the diffuser.
5-30 Air enters an adiabatic nozzle steadily at 300 kPa, 200°C, and 30 m/s and leaves...
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...
Question # 3 (35pts) 50kg/s of air steadily enter a diffuser at a velocity of 750m/s...
Question # 3 (35pts) 50kg/s of air steadily enter a diffuser at a velocity of 750m/s and a static pressure of 20kPa. The air leaves the diffuser at a velocity of 90m/s and a static pressure of 330kPa. The entrance area of the diffuser is 0.25m², and its exit area is 0.28m². Determine the magnitude and direction of the force on the strut that holds the diffuser stationary assuming that this diffuser is operated in an atmospheric pressure po =...
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Air steadily enters the diffuser section of a jet engine at a velocity of 270 m/s...
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Air enters a diffuser with a velocity of 900km/hr and at 0 C and 50 kPa....
Air enters a diffuser with a velocity of 900km/hr and at 0 C and 50 kPa. It leaves at 80 m/sec. If the exit area exceeds the inlet one by 20% * The exit temperature (C) is.1 22.9 9.22 2.29 92.2 * The exit pressure (kPa) is.2 14.42 143.8 22.93 100.0 O
thermodynamics Thermodynamics P5.31: - Steam at 3 MPa and 400°C enters an adiabatic nozle steadily with...
thermodynamics
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P5.31: - Steam at 3 MPa and 400°C enters an adiabatic nozle steadily with a velocity of 40 m/s and leaves at 2.5 MPa and 300 m/s. Determine (a) the exit temperature (b) the ratio of the inlet to exit area A1/A2. P5.64:- Refrigerant-134a at 800 kPa and 25°C is throttled to a temperature of 220°C. Determine the pressure and the internal energy of the refrigerant at the final state P1-0.8 MPa
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 0.8 bar and 127 Centers an adiabatic diffuser steadily at a rate of 6000 kg/ h and leaves at 1 bar. The velocity of the air stream is decreased from 230 m/st 0 30 m/s as it passes through the diffuser. Find (a) the exit temperature of the ai rand (b) the exit area of the diffuser.
Air at 0.8 bar and 127 Centers an adiabatic diffuser steadily at a rate of 6000 kg/ h and leaves at 1 bar. The velocity of the air stream is decreased from 230 m/st 0 30 m/s as it passes through the diffuser. Find (a) the exit temperature of the ai rand (b) the exit area of the diffuser.
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...
Question # 3 (35pts) 50kg/s of air steadily enter a diffuser at a velocity of 750m/s and a static pressure of 20kPa. The air leaves the diffuser at a velocity of 90m/s and a static pressure of 330kPa. The entrance area of the diffuser is 0.25m², and its exit area is 0.28m². Determine the magnitude and direction of the force on the strut that holds the diffuser stationary assuming that this diffuser is operated in an atmospheric pressure po =...
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Air enters a diffuser with a velocity of 900km/hr and at 0 C and 50 kPa. It leaves at 80 m/sec. If the exit area exceeds the inlet one by 20% * The exit temperature (C) is.1 22.9 9.22 2.29 92.2 * The exit pressure (kPa) is.2 14.42 143.8 22.93 100.0 O
thermodynamics
Thermodynamics
P5.31: - Steam at 3 MPa and 400°C enters an adiabatic nozle steadily with a velocity of 40 m/s and leaves at 2.5 MPa and 300 m/s. Determine (a) the exit temperature (b) the ratio of the inlet to exit area A1/A2. P5.64:- Refrigerant-134a at 800 kPa and 25°C is throttled to a temperature of 220°C. Determine the pressure and the internal energy of the refrigerant at the final state P1-0.8 MPa
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