Homework Help is Here – Start Your Trial Now!
Engineering
Mechanical Engineering
Examine the following open gas turbine process. The temperature of the inlet air is 296 K and pressure is 100 kPa. The polytropic efficiency of the compressor is 81.0 % and pressure ratio 7. The heat flow rate (fuel power) into process is 1.25 MW. The maximum temperature of the process (after combustion chamber) is 1440 K and the polytropic efficiency of the turbine is 87.0 %. The mass flow rate of air is 1.207 kg/s. A constant specific heat cp = 1.15 kJ/kgk can be used for the working fluid. Combustion chamber can be considered as adiabatic. Air in Calculate: C Fuel 10 CH 3 1) Temperature after compressor T₂ 2) Compressor power Pc 3) Temperature after turbine T 4) Turbine power Pt 5) Thermal efficiency of the system nt T Flue gas K (with zero decimal accuracy) MW (with three decimal accuracy) K (with zero decimal accuracy) MW (with three decimal accuracy) % (with one decimal accuracy)

Examine the following open gas turbine process. The temperature of the inlet air is 296 K and pressure is 100 kPa. The polytropic efficiency of the compressor is 81.0 % and pressure ratio 7. The heat flow rate (fuel power) into process is 1.25 MW. The maximum temperature of the process (after combustion chamber) is 1440 K and the polytropic efficiency of the turbine is 87.0 %. The mass flow rate of air is 1.207 kg/s. A constant specific heat cp = 1.15 kJ/kgk can be used for the working fluid. Combustion chamber can be considered as adiabatic. Air in Calculate: C Fuel 10 CH 3 1) Temperature after compressor T₂ 2) Compressor power Pc 3) Temperature after turbine T 4) Turbine power Pt 5) Thermal efficiency of the system nt T Flue gas K (with zero decimal accuracy) MW (with three decimal accuracy) K (with zero decimal accuracy) MW (with three decimal accuracy) % (with one decimal accuracy)

Elements Of Electromagnetics
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
See similar textbooks
icon
Related questions
Question
Examine the following open gas turbine process. The temperature of the inlet air is 296 K and pressure is 100 kPa. The polytropic efficiency of the compressor is 81.0% and pressure ratio is 7. The heat flow rate (fuel power) into process is 1.25 MW. The maximum temperature of the process (after combustion chamber) is 1440 K and the polytropic efficiency of the turbine is 87.0 %. The mass flow rate of air is 1.207 kg/s. A constant specific heat cp = 1.15 kJ/kgk can be used for the working fluid. Combustion chamber can be considered as adiabatic. Air in Calculate: O Fuel ∞ CH 3 1) Temperature after compressor T2 2) Compressor power Pc 3) Temperature after turbine T4 4) Turbine power Pt 5) Thermal efficiency of the system nt H P Flue gas K (with zero decimal accuracy) MW (with three decimal accuracy) K (with zero decimal accuracy) MW (with three decimal accuracy) % (with one decimal accuracy)
Transcribed Image Text:Examine the following open gas turbine process. The temperature of the inlet air is 296 K and pressure is 100 kPa. The polytropic efficiency of the compressor is 81.0% and pressure ratio is 7. The heat flow rate (fuel power) into process is 1.25 MW. The maximum temperature of the process (after combustion chamber) is 1440 K and the polytropic efficiency of the turbine is 87.0 %. The mass flow rate of air is 1.207 kg/s. A constant specific heat cp = 1.15 kJ/kgk can be used for the working fluid. Combustion chamber can be considered as adiabatic. Air in Calculate: O Fuel ∞ CH 3 1) Temperature after compressor T2 2) Compressor power Pc 3) Temperature after turbine T4 4) Turbine power Pt 5) Thermal efficiency of the system nt H P Flue gas K (with zero decimal accuracy) MW (with three decimal accuracy) K (with zero decimal accuracy) MW (with three decimal accuracy) % (with one decimal accuracy)
Expert Solution
trending now

Trending now

This is a popular solution!

steps

Step by step

Solved in 4 steps with 31 images

SEE SOLUTIONCheck out a sample Q&A here
Blurred answer
Knowledge Booster
Power Plant Engineering
Learn more about
Need a deep-dive on the concept behind this application? Look no further. Learn more about this topic, mechanical-engineering and related others by exploring similar questions and additional content below.
Recommended textbooks for you
Elements Of Electromagnetics
Elements Of Electromagnetics
Mechanical Engineering
ISBN:
9780190698614
Author:
Sadiku, Matthew N. O.
Publisher:
Oxford University Press
Mechanics of Materials (10th Edition)
Mechanics of Materials (10th Edition)
Mechanical Engineering
ISBN:
9780134319650
Author:
Russell C. Hibbeler
Publisher:
PEARSON
Thermodynamics: An Engineering Approach
Thermodynamics: An Engineering Approach
Mechanical Engineering
ISBN:
9781259822674
Author:
Yunus A. Cengel Dr., Michael A. Boles
Publisher:
McGraw-Hill Education
Control Systems Engineering
Control Systems Engineering
Mechanical Engineering
ISBN:
9781118170519
Author:
Norman S. Nise
Publisher:
WILEY
Mechanics of Materials (MindTap Course List)
Mechanics of Materials (MindTap Course List)
Mechanical Engineering
ISBN:
9781337093347
Author:
Barry J. Goodno, James M. Gere
Publisher:
Cengage Learning
Engineering Mechanics: Statics
Engineering Mechanics: Statics
Mechanical Engineering
ISBN:
9781118807330
Author:
James L. Meriam, L. G. Kraige, J. N. Bolton
Publisher:
WILEY
SEE MORE TEXTBOOKS