The air flow through a jet engine is 30 kg/s and the fuel flow is 1 kg/s. The exhaust gases leave with a relative velocity of 610 m/s. Pressure equilibrium exists over the exit plane. Compute the velocity of the airplane if the thrust power is 1.12 x 108 W. The air flow through a jet engine is 30 kg/s and the fuel flow is 1 kg/s. The exhaust gases leave with a relative velocity of 610 m/s. Pressureequilibrium exists over the exit plane. Compute the velocity of the airplane if the thrust power is 1.12 x 106 w.

Given Data ma =30kg/s mf =1kg/s Ve =610m/s f=1.12x106 w

Answered: The air flow through a jet engine is 30…

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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The air flow through a jet engine is 30 kg/s and the fuel flow is 1 kg/s. The exhaust gases leave with a relative velocity of 610 m/s. Pressure equilibrium exists over the exit plane. Compute the velocity of the airplane if the thrust power is 1.12 x 108 W.

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