Air flows through a 0.25-m-diameter duct. At the inlet the velocity is 300 m/s, and the...

Air flows through a 0.25-m-diameter duct. At the inlet the velocity is 300 m/s, and the stagnation temperature is 90°C. If the Mach number at the exit is 0.3, determine the direction and the rate of heat transfer. For the same conditions at the inlet, determine the amount of heat that must be transferred to the system if the flow is to be sonic at the exit of the duct.

Expert Solution

samet mamat answered 2 years ago

Air flows through a 8-in-diameter, 60-ft-long adiabatic duct with inlet conditions of V1= 550 ft/s, T01=...

Air flows through a 8-in-diameter, 60-ft-long adiabatic duct with inlet conditions of V1= 550 ft/s, T01= 650 R, and P1= 50 psia. For an average friction factor of 0.03, determine the velocity, temperature, and pressure at the exit of the duct. Please DO NOT merely copy other expert's work. I would like original work.

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Air is cooled from 300 K to 273 K as it flows steadily through a duct....

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Air flows through a pipe that has a length of 45 m with an inside diameter...

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Air flows into a commercial steel pipe of 5 cm ID at 70 m/s. The inlet...

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Air flows in a pipe with a diameter, D=50 mm. The inlet conditions are: M1 =...

Air flows in a pipe with a diameter, D=50 mm. The inlet conditions are: M1 = 3; total pressure, P01 = 1000 kPa absolute; and temperature, T1 = 550 K. The friction coefficient is, f = 0.004. The exit Mach number decreases with the length of the pipe. Plot the following while the exit Mach number to be changed from 2.5 to 0.99 with decrements of ?M=0.01: a) L, length of the pipe that is going to give the desired...

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