Q40 The venturi of a simple carburettor has a throat diameter of 35 mm and aid the coefficient of air flow is 0.85. The fuel orifice has a diameter of 2.3 mm and the coefficient of fuel flow is 0.66. The petrol surface is 5mm below the throat Find The air Fuel ratio for a pressure drop of 0.07 bar when nozzle lip is neglected. ⑥The air Fuel ratio when the nozzle lip is taken into account win wilt to tout The minimum velocity of air (critical air velocity) required to start The fuelut size flow when nozzle lip is provided. [used Approximate method Just Take density of air and fuel as 1.2 and 750 kg/m³ respectively) Enter APS Answers [a_11.93 b-11-96 c_7.83 m/sec ] 2-1 1920

Automotive Technology: A Systems Approach (MindTap Course List)
6th Edition
ISBN:9781133612315
Author:Jack Erjavec, Rob Thompson
Publisher:Jack Erjavec, Rob Thompson
Chapter33: Emission Control Systems
Section: Chapter Questions
Problem 1RQ: Explain why a small PCV valve opening is adequate at idle speed.
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Q40 The venturi of a simple carburettor has a throat diameter of 35 mm and
aid the coefficient of air flow is 0.85. The fuel orifice has a diameter of 2.3 mm
and the coefficient of fuel flow is 0.66. The petrol surface is 5mm below the throat
Find The air Fuel ratio for a pressure drop of 0.07 bar when nozzle lip is neglected.
⑥The air Fuel ratio when the nozzle lip is taken into account win wilt to tout
The minimum velocity of air (critical air velocity) required to start The fuelut
size flow when nozzle lip is provided. [used Approximate method Just
Take density of air and fuel as 1.2 and 750 kg/m³ respectively)
Enter APS Answers [a_11.93 b-11-96 c_7.83 m/sec ] 2-1 1920
Transcribed Image Text:Q40 The venturi of a simple carburettor has a throat diameter of 35 mm and aid the coefficient of air flow is 0.85. The fuel orifice has a diameter of 2.3 mm and the coefficient of fuel flow is 0.66. The petrol surface is 5mm below the throat Find The air Fuel ratio for a pressure drop of 0.07 bar when nozzle lip is neglected. ⑥The air Fuel ratio when the nozzle lip is taken into account win wilt to tout The minimum velocity of air (critical air velocity) required to start The fuelut size flow when nozzle lip is provided. [used Approximate method Just Take density of air and fuel as 1.2 and 750 kg/m³ respectively) Enter APS Answers [a_11.93 b-11-96 c_7.83 m/sec ] 2-1 1920
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