Determine the air-fuel ratio at 6000 m altitude in a carburettor adjusted to given anair-fuel ratio 15:1 at sea level where air temperature is 27°C and pressure is 1.013bar.The temperature of air decreases with altitude and is given by the expression T Ts-0.0065 h, where 'h' is height in meters and Ts temperature at sea level in °C.1.013%3DThe air pressure decreases with altitude as per the relation h 19220 In

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el ratio at 6000 m altit sea level where air ter

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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Question

Determine the air-fuel ratio at 6000 m altitude in a carburettor adjusted to given an
air-fuel ratio 15:1 at sea level where air temperature is 27°C and pressure is 1.013
bar.
The temperature of air decreases with altitude and is given by the expression T Ts
-0.0065 h, where 'h' is height in meters and Ts temperature at sea level in °C.
1.013
%3D
The air pressure decreases with altitude as per the relation h 19220 In

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