Your second task would be to explore the relative performance for each of the four major types of turbine engines given below. This means calculating performance parameters such as specific thrust, fuel to gir ratio, propulsive efficiency, thermol efficiency, overall efficiency, propeller efficiency. TSFC or SFC etc. (where applicable) for each of the given gas turbine engines and commenting on their relative performance. Please note the folowing assumptions: 1) Assume all processes to be ideal, unless otherwise stated. 2) Assume constant values of (y, Cp) [y = 1.4 and Cp 1.005 kJ/kg K: R 287 J/kg K). %3D

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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Your second task would be to explore the relative performance for each of the four major types of turbine engines
given below. This means calculating performance parameters such as specific thrust, fuel to gir ratio, propulsive
efficiency, thermol efficiency, overall efficiency, propeller efficiency. TSFC or SFC etc. (where applicable) for each
of the given gas turbine engines and commenting on their relative performance. Please note the folowing assumptions:
1) Assume all processes to be ideal, unless otherwise stated.
2) Assume constant values of (y, Cp) [y = 1.4 and Cp 1.005 kJ/kg K: R 287 J/kg K).
%3D
Transcribed Image Text:Your second task would be to explore the relative performance for each of the four major types of turbine engines given below. This means calculating performance parameters such as specific thrust, fuel to gir ratio, propulsive efficiency, thermol efficiency, overall efficiency, propeller efficiency. TSFC or SFC etc. (where applicable) for each of the given gas turbine engines and commenting on their relative performance. Please note the folowing assumptions: 1) Assume all processes to be ideal, unless otherwise stated. 2) Assume constant values of (y, Cp) [y = 1.4 and Cp 1.005 kJ/kg K: R 287 J/kg K). %3D
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