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Q1/A/ The heat capacity, Cp, depends on temperature and can be expressed as a function of temperature: Cp = A + BT + CT² + DT-² R The enthalpy change, AH which is equal to heat is given by: -T2 AH = Q = n :n Cpdr T1 Write a script file to calculate the heat required if we need to increase the temperature of 15 kgmole/hr of methane from 298.13 to 373.13 K. Where A=1.702, B=9.081*10³, C=-2.164*106, D=0, and R=8.314.

Q1/A/ The heat capacity, Cp, depends on temperature and can be expressed as a function of temperature: Cp = A + BT + CT² + DT-² R The enthalpy change, AH which is equal to heat is given by: -T2 AH = Q = n :n Cpdr T1 Write a script file to calculate the heat required if we need to increase the temperature of 15 kgmole/hr of methane from 298.13 to 373.13 K. Where A=1.702, B=9.081*10³, C=-2.164*106, D=0, and R=8.314.

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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Q1/A/ The heat capacity, Cp, depends on temperature and can be expressed as a function of temperature: Cp A+ BT + CT² + DT-² R The enthalpy change, AH which is equal to heat is given by: T2 AH = Q = nCpdr T1 Write a script file to calculate the heat required if we need to increase the temperature of 15 kgmole/hr of methane from 298.13 to 373.13 K. Where A=1.702, B=9.081*10³, C=-2.164*106, D=0, and R=8.314.
Transcribed Image Text:Q1/A/ The heat capacity, Cp, depends on temperature and can be expressed as a function of temperature: Cp A+ BT + CT² + DT-² R The enthalpy change, AH which is equal to heat is given by: T2 AH = Q = nCpdr T1 Write a script file to calculate the heat required if we need to increase the temperature of 15 kgmole/hr of methane from 298.13 to 373.13 K. Where A=1.702, B=9.081*10³, C=-2.164*106, D=0, and R=8.314.
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