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The efficiencies of aircraft can be very important indicators for meeting emission standards. Often thermal efficiency needs to be estimated indirectly instead of conducting combustion tests. A business jet is conducting testing at Mach 0.70 at sea level using the Jet A1 fuel (LCV=43.15 MJ/kg) at a specific fuel consumption of 0.06 kg/(Nh). The propulsive jet velocity is about 340 m/s. The local ambient air temperature is 288 K. Calculate the thermal efficiency of the engine. Hand written plzz

The efficiencies of aircraft can be very important indicators for meeting emission standards. Often thermal efficiency needs to be estimated indirectly instead of conducting combustion tests. A business jet is conducting testing at Mach 0.70 at sea level using the Jet A1 fuel (LCV=43.15 MJ/kg) at a specific fuel consumption of 0.06 kg/(Nh). The propulsive jet velocity is about 340 m/s. The local ambient air temperature is 288 K. Calculate the thermal efficiency of the engine. Hand written plzz

Elements Of Electromagnetics
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
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4. The efficiencies of aircraft can be very important indicators for meeting emission standards. Often thermal efficiency needs to be estimated indirectly instead of conducting combustion tests. A business jet is conducting testing at Mach 0.70 at sea level using the Jet A1 fuel (LCV=43.15 MJ/kg) at a specific fuel consumption of 0.06 kg/(Nh). The propulsive jet velocity is about 340 m/s. The local ambient air temperature is 288 K. Calculate the thermal efficiency of the engine. Hand written plzz
Transcribed Image Text:4. The efficiencies of aircraft can be very important indicators for meeting emission standards. Often thermal efficiency needs to be estimated indirectly instead of conducting combustion tests. A business jet is conducting testing at Mach 0.70 at sea level using the Jet A1 fuel (LCV=43.15 MJ/kg) at a specific fuel consumption of 0.06 kg/(Nh). The propulsive jet velocity is about 340 m/s. The local ambient air temperature is 288 K. Calculate the thermal efficiency of the engine. Hand written plzz
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