..A 6.8-liter, in-line, eight-cylinder CI engine has a compression ratio rc=18.5 and a crevice volume equ to 3% of the clearance volume. During the engine cycle pressure the crevice volume equals combustic chamber pressure while remaining at the cylinder wall temperature of 190°C. Cylinder conditions at th start of compression are 75°C and 120 kPa, and peak pressure is 11,000 kPa. Cutoff ratio is 2.3. Calculat (a) Crevice volume of one cylinder. (b) Percent of air-fuel mixture in the crevice volume at the end compression.(c) Percent of air-fuel mixture in the crevice volume at the end of combustion.

Elements Of Electromagnetics
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ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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..A 6.8-liter, in-line, eight-cylinder Cl engine has a compression ratio rc-18.5 and a crevice volume equal
to 3% of the clearance volume. During the engine cycle pressure the crevice volume equals combustion
chamber pressure while remaining at the cylinder wall temperature of 190°C. Cylinder conditions at the
start of compression are 75°C and 120 kPa, and peak pressure is 11,000 kPa. Cutoff ratio is 2.3. Calculate:
(a) Crevice volume of one cylinder. (b) Percent of air-fuel mixture in the crevice volume at the end of
compression.(c) Percent of air-fuel mixture in the crevice volume at the end of combustion.
Transcribed Image Text:..A 6.8-liter, in-line, eight-cylinder Cl engine has a compression ratio rc-18.5 and a crevice volume equal to 3% of the clearance volume. During the engine cycle pressure the crevice volume equals combustion chamber pressure while remaining at the cylinder wall temperature of 190°C. Cylinder conditions at the start of compression are 75°C and 120 kPa, and peak pressure is 11,000 kPa. Cutoff ratio is 2.3. Calculate: (a) Crevice volume of one cylinder. (b) Percent of air-fuel mixture in the crevice volume at the end of compression.(c) Percent of air-fuel mixture in the crevice volume at the end of combustion.
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