Air enters the adiabatic nozzle of a turbojet engine at 230 kPa, 600C with a velocity of
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Air enters the adiabatic nozzle of a turbojet engine at 230 kPa, 600°C with a velocity of 60 m/s as shown in Figure P3.7. At the nozzle exit, the air is at 70 kPa, 450°C.
The dead state is 100 kPa, 20°C. Determine the following information,
a. The exit velocity of the air (m/s)
b. The isentropic efficiency of the nozzle
c. The exergy destruction per kg of air flowing through the nozzle (kJ/kg)
d. Devise and calculate an exergetic efficiency for the nozzle
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Related Book For
Thermal Energy Systems Design And Analysis
ISBN: 9781138735897
2nd Edition
Authors: Steven G. Penoncello
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