FUNDAMENTALS OF THERMODYNAMICS
FUNDAMENTALS OF THERMODYNAMICS
10th Edition
ISBN: 9781119634928
Author: Borgnakke
Publisher: WILEY
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The inlet of a nozzle is at 400K and the outlet is 300K. The nozzle operates with air as an ideal gas as the working fluid and the flow is isentropic. The flow velocity in the inlet is 2 m/s, vith pressure of 10 bar and di ameter of 15 cm. The gas constant for air is R = 0.287 kJ/kg*K. Solve for the outlet velocity and diameter.
Air goes through a Brayton cycle gas turbine, entering the compressor at 11 °C and 108 kPa. When it reaches the turbine inlet, the air is at 1,061 °C and 1.23 MPa. What is the net change in specific enthalpy of the working fluid after going through the compressor and heat addition processes? You may assume that the specific heat capacity c, is a constant 1.005 --1. kJ-kg 1.K1 throughout the whole cycle. Give your answer in kJ-kg1 to one decimal place.
There are required 1902.3 kW of compressor power to handle air adiabatically from 1 atm, 26.7°C to 304.06 kPa.  The initial air velocity is 21 m/s; the final is 85 m/s.  (a) If the process is isentropic, find the volume of air handled, m3/min measured at inlet conditions. (b) If the compression is an irreversible adiabatic to a temperature of 157.2°C, with the capacity found in (a), find the power input.
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