Question 3 a) A 4-stroke, 4-cylinder 2.0 litre gasoline engine has a compression ratio of 8.5 and operates at 1000 rpm. The thermodynamic cycle of the engine is modelled as an air- standard Otto cycle with constant specific heats (C,=1.005 kJ/kg-K, cv=0.718 kJ/kg-K, k=1.4). At the beginning of compression, the air is at 100 kPa and 295 K and the maximum temperature in the cycle is 2000 K. Determine: i) the mass flow rate of air. ii) the engine power output. iii) the thermal efficiency.

Elements Of Electromagnetics
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ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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Question 3
a) A 4-stroke, 4-cylinder 2.0 litre gasoline engine has a compression ratio of 8.5 and
operates at 1000 rpm. The thermodynamic cycle of the engine is modelled as an air-
standard Otto cycle with constant specific heats (cp=1.005 kJ/kg-K, cv=0.718 kJ/kg-K, k=1.4).
At the beginning of compression, the air is at 100 kPa and 295 K and the maximum
temperature in the cycle is 2000 K. Determine:
i) the mass flow rate of air.
ii) the engine power output.
iii) the thermal efficiency.
Transcribed Image Text:Question 3 a) A 4-stroke, 4-cylinder 2.0 litre gasoline engine has a compression ratio of 8.5 and operates at 1000 rpm. The thermodynamic cycle of the engine is modelled as an air- standard Otto cycle with constant specific heats (cp=1.005 kJ/kg-K, cv=0.718 kJ/kg-K, k=1.4). At the beginning of compression, the air is at 100 kPa and 295 K and the maximum temperature in the cycle is 2000 K. Determine: i) the mass flow rate of air. ii) the engine power output. iii) the thermal efficiency.
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