A simple carburetor under a certain condition delivers 5.45 kg/h of petrol with an air fuel ratio of 15. The fuel jet area is 2mm2 with coefficient of discharge of 0.75. If the tip of the fuel jet is 0.635cm above the level of petrol in the float chamber and the venturi throat coefficient of discharge of 0.80. calculate: (i) The venturi depression in cm of H2O necessary to cause air and fuel flow at the desired rate. (ii) The venturi throat diameter. (iii) The velocity of air across the venturi throat. You make take density of air = 1.29 kg/m3 and specific gravity of petrol =0.72

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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A simple carburetor under a certain condition delivers 5.45 kg/h of petrol with an air fuel ratio of 15. The fuel jet area is 2mm2 with coefficient of discharge of 0.75. If the tip of the fuel jet is 0.635cm above the level of petrol in the float chamber and the venturi throat coefficient of discharge of 0.80.

calculate:

(i) The venturi depression in cm of H2O necessary to cause air and fuel flow at the desired rate.

(ii) The venturi throat diameter.

(iii) The velocity of air across the venturi throat. You make take density of air = 1.29 kg/m3 and specific gravity of petrol =0.72

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