Using the principle of a venturi-meter,explain the working of a carburetor and a spray pump.

Vedclass pdf generator app on play store
Vedclass iOS app on app store
(N/A) The carburetor of an automobile uses a venturi channel (nozzle) through which air flows at a high speed.
According to Bernoulli's principle,as the speed of air increases in the narrow neck of the venturi,the pressure decreases.
This low pressure at the narrow neck sucks petrol from the fuel chamber into the air stream,creating the correct air-fuel mixture necessary for combustion in the engine.
Devices like Bunsen burners,atomizers,perfume sprayers,and insecticide sprayers operate on the same principle.
In a spray pump,a piston forces air at high speed over the open end of a tube connected to a liquid container. This creates a region of low pressure at the top of the tube,causing the liquid to rise and be sprayed out along with the air stream.

Explore More

Similar Questions

An ideal fluid of density $800 \; kg \cdot m^{-3}$ flows smoothly through a bent pipe (as shown in the figure) that tapers in cross-sectional area from $a$ to $\frac{a}{2}$. The pressure difference between the wide and narrow sections of the pipe is $4100 \; Pa$. At the wider section,the velocity of the fluid is $\frac{\sqrt{x}}{6} \; m \cdot s^{-1}$. Find the value of $x$. (Given $g = 10 \; m \cdot s^{-2}$)

An $L$-shaped glass tube is just immersed in flowing water such that its opening is pointing against the flowing water. If the speed of the water current is $v$,then

Water is in streamline flow along a horizontal pipe with non-uniform cross-section. At a point in the pipe where the area of cross-section is $10 \,cm^{2}$, the velocity of water is $1 \,ms^{-1}$ and the pressure is $2000 \,Pa$. The pressure at another point where the cross-sectional area is $5 \,cm^{2}$ is (in $\,Pa$)

Which of the following is not an assumption for an ideal fluid flow for which Bernoulli's principle is valid?

$A$ plane is in level flight at constant speed and each of its two wings has an area of $25 \; m^{2}$. If the speed of the air is $180 \; km/h$ over the lower wing and $234 \; km/h$ over the upper wing surface,determine the plane's mass in $kg$. (Take air density to be $1 \; kg \; m^{-3}$ and $g = 9.8 \; m/s^{2}$).

Vedclass Products

For Students

Vedclass Test Series

Mock tests in real JEE/NEET style with performance analysis. 5-day free trial.

Start Free Trial
For Teachers

Exam Paper Generator

Generate Set A/B/C/D exam papers from 7.5L+ questions in 2 minutes. 3 chapters free.

Try Free
For Institutes

Online Exam Module

Live online exams with unlimited students, 360° analytics & white-label branding.

See Demo