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5-161 An ideal gas expands in an adiabatic turbine from 1200 K, 600 kPa to 700 K. Determine the turbine inlet vol- ume flow rate of the gas, in m³/s, required to produce turbine work output at the rate of 200 kW. The average values of the specific heats for this gas over the temperature range are cp 1.13 kJ/kg . K and c = 0.83 kJ/kg - K. R = 0.30 kJ/kg. K. = =

5-161 An ideal gas expands in an adiabatic turbine from 1200 K, 600 kPa to 700 K. Determine the turbine inlet vol- ume flow rate of the gas, in m³/s, required to produce turbine work output at the rate of 200 kW. The average values of the specific heats for this gas over the temperature range are cp 1.13 kJ/kg . K and c = 0.83 kJ/kg - K. R = 0.30 kJ/kg. K. = =

Introduction to Chemical Engineering Thermodynamics
Introduction to Chemical Engineering Thermodynamics
8th Edition
ISBN:9781259696527
Author:J.M. Smith Termodinamica en ingenieria quimica, Hendrick C Van Ness, Michael Abbott, Mark Swihart
Publisher:J.M. Smith Termodinamica en ingenieria quimica, Hendrick C Van Ness, Michael Abbott, Mark Swihart
Chapter1: Introduction
Section: Chapter Questions
Problem 1.1P
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5-161 An ideal gas expands in an adiabatic turbine from 1200 K, 600 kPa to 700 K. Determine the turbine inlet vol- ume flow rate of the gas, in m³/s, required to produce turbine work output at the rate of 200 kW. The average values of the specific heats for this gas over the temperature range are cp 1.13 kJ/kg . K and c = 0.83 kJ/kg K. R = 0.30 kJ/kg. K. =
Transcribed Image Text:5-161 An ideal gas expands in an adiabatic turbine from 1200 K, 600 kPa to 700 K. Determine the turbine inlet vol- ume flow rate of the gas, in m³/s, required to produce turbine work output at the rate of 200 kW. The average values of the specific heats for this gas over the temperature range are cp 1.13 kJ/kg . K and c = 0.83 kJ/kg K. R = 0.30 kJ/kg. K. =
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