A turbojet aircraft moving with a velocity of 790 ft/s at a runway where the pressure & temperature is found to be 14.7psi & 546R. The axial flow compressor provides a pressure ratio of 14 to 1. Temperature at the turbine inlet is 2000R. The mass flowrate of air inside the engine is 133 lbm/s. Determine the following: a. T-S diagram
A turbojet aircraft moving with a velocity of 790 ft/s at a runway where the pressure & temperature is found to be 14.7psi & 546R. The axial flow compressor provides a pressure ratio of 14 to 1. Temperature at the turbine inlet is 2000R. The mass flowrate of air inside the engine is 133 lbm/s. Determine the following: a. T-S diagram
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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A turbojet aircraft moving with a velocity of 790 ft/s at a runway where the pressure
& temperature is found to be 14.7psi & 546R. The axial flow compressor provides a
pressure ratio of 14 to 1. Temperature at the turbine inlet is 2000R. The mass flowrate of air
inside the engine is 133 lbm/s. Determine the following:
a. T-S diagram
b. Pressure & temperature at each state
c. Thrust force (lbf)
d. Propulsive power developed (BTU/min)
e. Propulsive Efficiency
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