FUND OF ENG THERMODYN(LLF)+WILEYPLUS
9th Edition
ISBN: 9781119391777
Author: MORAN
Publisher: WILEY
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Air enters a 3600-kW turbine operating at steady state with a mass flow rate of 18 kg/s at 800, 3 bar and a velocity of 100 m/s. The air expands adiabatically through the turbine and exits at a velocity of 150 m/s. Employing the ideal gas model, determine
the pressure and temperature of the air at the turbine exit, in bar and , respectively.
the rate of entropy production in the turbine, in kW/K.
the isentropic efficiency of the turbine.
Show the processes on a T–s diagram
The figure shows a turbine operating at a steady state that provides power to an air
compressor and an electric generator. Air enters the turbine with a volumetric flow rate of 1.3
m³/s at 527°C, 10.0 bar and exits the turbine at 107°C, 1 bar. The turbine provides power of
900 kW to the compressor and 1400 kW to the generator. Air can be modeled as an ideal gas
and kinetic and potential energy changes are negligible.
a. Determine the mass flow rate of the air, in kg/s.
b. For the turbine as the control volume, determine the rate of heat transfer, in kW.
Air
1
Compressor
Air
W₁ = 900 kW
(AV)1. P1
T₁ = 527°C
Turbine
2
WEG = 1400 kW
Electric
Generator
T₂ = 107°C
P2 = 1 bar
+
Air enters a diffuser operating at steady state at 645°R, 15 Ibf/in.?, with a velocity of 600 ft/s, and exits with a velocity of 60 ft/s. The
ratio of the exit area to the inlet area is 1o.
Assuming the ideal gas model for the air and ignoring heat transfer, determine the temperature, in °R, and pressure, in Ibf/in.?, at the
exit.
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