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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 carburetor, tested in the laboratory has its float chamber vented to
atmosphere. The main metering system is adjusted to give an air-fuel
ratio of 15:1 at sea level conditions. The pressure at the venturi thront
is 0.8 bar. The atmospheric pressure is 1 bar. The same carburetor is
tested again when an air cleaner is fitted at the inlet to the carburetor.
The pressure drop to air cleaner is found to be 30 mm of Hg when air
flow at sea level condition is 240 kg/h. Assuming zero tip and constams
coefficient of flow, calculate (i) the throat pressure when the air-cleaner
is fitted and (ii) air-fuel rat io when the air cleaner is fitted.
Transcribed Image Text:A carburetor, tested in the laboratory has its float chamber vented to atmosphere. The main metering system is adjusted to give an air-fuel ratio of 15:1 at sea level conditions. The pressure at the venturi thront is 0.8 bar. The atmospheric pressure is 1 bar. The same carburetor is tested again when an air cleaner is fitted at the inlet to the carburetor. The pressure drop to air cleaner is found to be 30 mm of Hg when air flow at sea level condition is 240 kg/h. Assuming zero tip and constams coefficient of flow, calculate (i) the throat pressure when the air-cleaner is fitted and (ii) air-fuel rat io when the air cleaner is fitted.
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