31 An eight-cylinder, four-stroke engine of 9 cm bore and 8 cm stroke with a compression ratio of 7 is tested at 4500 rpm on a dynamometer which has 54 em arm. During a 10 minutes test the dynamometer scale beam reading was 42 kg and the engine consumed 4.4 kg of gasoline having a calorific value of 44000 kJ/kg. Air 27 °C and 1 bar was supplied to the carburettor at the rate of 6 kg/min. Find (i) the brake power delivered (ii) the brake mean effective pressure (iii) the brake specific fuel consumption (iv) the brake specific air consumption (v) the brake thermal efficiency (vi) the volumetric efficiency and (vii) the air-fuel ratio.

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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An eight-cylinder, four-st roke engine of 9 cm bore and 8 cm atroke with
a compression ratio of 7 is tested at 4500 rpm on a dynamometer which
has 54 cm arm. During a 10 minutes test the dynamometer scale beam
reading was 42 kg and the engine consumed 4.4 kg of gasoline having
a calorifie value of 44000 kJ/kg. Air 27 °C and 1 bar was supplied
to the earburettor at the rate of 6 kg/min. Find (i) the brake power
delivered (ii) the brake mean effective presaure (iii) the brake specific
fuel consumption (iv) the brake specific air conaumption (v) the brake
thermal efficiency (vi) the volumetric efficiency and (vi) the air-fuel
ratio.
21.3
Transcribed Image Text:An eight-cylinder, four-st roke engine of 9 cm bore and 8 cm atroke with a compression ratio of 7 is tested at 4500 rpm on a dynamometer which has 54 cm arm. During a 10 minutes test the dynamometer scale beam reading was 42 kg and the engine consumed 4.4 kg of gasoline having a calorifie value of 44000 kJ/kg. Air 27 °C and 1 bar was supplied to the earburettor at the rate of 6 kg/min. Find (i) the brake power delivered (ii) the brake mean effective presaure (iii) the brake specific fuel consumption (iv) the brake specific air conaumption (v) the brake thermal efficiency (vi) the volumetric efficiency and (vi) the air-fuel ratio. 21.3
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