Answer the question D and E please. A, B and C are answered by another expert. Problem 4: Consider the following schematic of a simple turbojet engine model that uses air as its workingfluid. With the data given determine (A) the pressure and temperature of all five states, (B) the amount of heatadded in the burner, (C) the necessary air-to-fuel ratio of the engine, (D) the amount of power required by thecompressor, and (E) the velocity of the exhaust stream at the exit of the system.Note: The variable rp is the compressor ratio defined to be the pressure of the compressor exit to the pressure ofthe compressor inlet. Assume that the compressor, turbine, and nozzle are all adiabatic and reversible.The Turbojet Engine2P = Pj: 100 kPaBurnerT,: 300 k6: 125= 1200 KFHV = 43 KJ/g- frel

Given data,1-2→Compressor2-3→Combustion changer3-4→Turbine4-j→Nozzle

d. With the data given determine (A) the pressure and temperature of all five states, (B) the amount of h ed in the burner, (C) the necessary air-to-fuel ratio of the engine, (D) the amount of power required by t apressor, and (E) the velocity of the exhaust stream at the exit of the system. e: The variable rp is the compressor ratio defined to be the pressure of the compressor exit to the pressu compressor inlet. Assume that the compressor, turbine, and nozzle are all adiabatic and reversible. The Turbojet Eagine 3 P = P; : 100 k Pa

d. With the data given determine (A) the pressure and temperature of all five states, (B) the amount of h ed in the burner, (C) the necessary air-to-fuel ratio of the engine, (D) the amount of power required by t apressor, and (E) the velocity of the exhaust stream at the exit of the system. e: The variable rp is the compressor ratio defined to be the pressure of the compressor exit to the pressu compressor inlet. Assume that the compressor, turbine, and nozzle are all adiabatic and reversible. The Turbojet Eagine 3 P = P; : 100 k Pa

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

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