Examine the following open gas turbine process. The temperature of the inlet air is 292 K and pressure is 100 kPa. The polytropic efficiency of the compressor is 85.0 % and pressure ratio is 8. The heat flow rate (fuel power) into process is 1.25 MW. The maximum temperature of the process (after combustion chamber) is 1560 K and the polytropic efficiency of the turbine is 86.0 %. The mass flow rate of air is 1.063 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. Fuel Air in Calculate: C 21 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 t 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 292 K and pressure is 100 kPa. The polytropic efficiency of the compressor is 85.0 % and pressure ratio is 8. The heat flow rate (fuel power) into process is 1.25 MW. The maximum temperature of the process (after combustion chamber) is 1560 K and the polytropic efficiency of the turbine is 86.0 %. The mass flow rate of air is 1.063 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. Fuel Air in Calculate: C 21 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 t 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
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
Related questions
Question
100%
Please do not rely too much on chatgpt, because its answer may be wrong. Please consider it carefully and give your own answer. You can borrow ideas from gpt, but please do not believe its answer.
Very very grateful!
Please do not rely too much on chatgpt, because its answer may be wrong. Please consider it carefully and give your own answer. You can borrow ideas from gpt, but please do not believe its answer.
Very very grateful!
Transcribed Image Text:Examine the following open gas turbine process. The temperature of the inlet air is 292 K and pressure is 100 kPa.
The polytropic efficiency of the compressor is 85.0 % and pressure ratio is 8. The heat flow rate (fuel power) into
process is 1.25 MW. The maximum temperature of the process (after combustion chamber) is 1560 K and the
polytropic efficiency of the turbine is 86.0 %. The mass flow rate of air is 1.063 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:
2
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
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
This question has been solved!
Explore an expertly crafted, step-by-step solution for a thorough understanding of key concepts.
Step by step
Solved in 4 steps with 31 images
Knowledge Booster
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
Mechanical Engineering
ISBN:
9780190698614
Author:
Sadiku, Matthew N. O.
Publisher:
Oxford University Press
Mechanics of Materials (10th Edition)
Mechanical Engineering
ISBN:
9780134319650
Author:
Russell C. Hibbeler
Publisher:
PEARSON
Thermodynamics: An Engineering Approach
Mechanical Engineering
ISBN:
9781259822674
Author:
Yunus A. Cengel Dr., Michael A. Boles
Publisher:
McGraw-Hill Education
Elements Of Electromagnetics
Mechanical Engineering
ISBN:
9780190698614
Author:
Sadiku, Matthew N. O.
Publisher:
Oxford University Press
Mechanics of Materials (10th Edition)
Mechanical Engineering
ISBN:
9780134319650
Author:
Russell C. Hibbeler
Publisher:
PEARSON
Thermodynamics: An Engineering Approach
Mechanical Engineering
ISBN:
9781259822674
Author:
Yunus A. Cengel Dr., Michael A. Boles
Publisher:
McGraw-Hill Education
Control Systems Engineering
Mechanical Engineering
ISBN:
9781118170519
Author:
Norman S. Nise
Publisher:
WILEY
Mechanics of Materials (MindTap Course List)
Mechanical Engineering
ISBN:
9781337093347
Author:
Barry J. Goodno, James M. Gere
Publisher:
Cengage Learning
Engineering Mechanics: Statics
Mechanical Engineering
ISBN:
9781118807330
Author:
James L. Meriam, L. G. Kraige, J. N. Bolton
Publisher:
WILEY