An aircraft flies at 960 kmph. One of its turbojet engines takes in 40 kg/s of air and expands the gases to the ambient pressure. The air-fuel ratio is 50 and the lower calorific value of the fuel is 43 MJ/kg. For maximum thrust power determine (i) jet velocity, (ü) specific thrust and (üi) thrust power.
An aircraft flies at 960 kmph. One of its turbojet engines takes in 40 kg/s of air and expands the gases to the ambient pressure. The air-fuel ratio is 50 and the lower calorific value of the fuel is 43 MJ/kg. For maximum thrust power determine (i) jet velocity, (ü) specific thrust and (üi) thrust power.
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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![An aircraft flies at 960 kmph. One of its
(c)
turbojet engines takes in 40 kg/s of air
and expands the gases to the ambient
pressure. The air-fuel ratio is 50 and
the lower calorific value of the fuel is
43 MJ/kg. For maximum thrust power
determine (i) jet velocity, (ü) specific
thrust and (üi) thrust power.](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2Fa700fa96-78d0-444c-93fc-b1f3757bca06%2Ff4023396-fbcf-4a6a-b9a2-1066747efbbb%2Fi711cuw_processed.jpeg&w=3840&q=75)
Transcribed Image Text:An aircraft flies at 960 kmph. One of its
(c)
turbojet engines takes in 40 kg/s of air
and expands the gases to the ambient
pressure. The air-fuel ratio is 50 and
the lower calorific value of the fuel is
43 MJ/kg. For maximum thrust power
determine (i) jet velocity, (ü) specific
thrust and (üi) thrust power.
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