JEE Advance - Physics (2014 - Paper 2 Offline - No. 16)

A spray gun is shown in the below figure where a piston pushes air out of a nozzle. A thin tube of uniform cross-section is connected to the nozzle. The other end of the tube is in a small liquid container. As the piston pushes air through the nozzle, the liquid from the container rises into the nozzle and is sprayed out. For the spray gun shown, the radii of the piston and the nozzle are 20 mm and 1 mm, respectively. The upper end of the container is open to the atmosphere.

A spray gun is shown in the below figure where a piston pushes air out of a nozzle. A thin tube of uniform cross-section is connected to the nozzle. The other end of the tube is in a small liquid container. As the piston pushes air through the nozzle, the liquid from the container rises into the nozzle and is sprayed out. For the spray gun shown, the radii of the piston and the nozzle are 20 mm and 1 mm, respectively. The upper end of the container is open to the atmosphere.

A spray gun is shown in the below figure where a piston pushes air out of a nozzle. A thin tube of uniform cross-section is connected to the nozzle. The other end of the tube is in a small liquid container. As the piston pushes air through the nozzle, the liquid from the container rises into the nozzle and is sprayed out. For the spray gun shown, the radii of the piston and the nozzle are 20 mm and 1 mm, respectively. The upper end of the container is open to the atmosphere.

If the piston is pushed at a speed of 5 mm s$$-$$1, the air comes out of the nozzle with a speed of
$0.1 \mathrm{~ms}^{-1}$
$1 \mathrm{~ms}^{-1}$
$2 \mathrm{~ms}^{-1}$
$8 \mathrm{~ms}^{-1}$

Explanation

The dynamics of the spray gun follow the principle of conservation of mass or the continuity equation from fluid dynamics. This principle states that the mass flow rate of a fluid entering a system must equal the mass flow rate leaving a system. For incompressible fluids like liquids, or compressed air where changes in density are negligible, this is often simplified to the rate of volume flow or the continuity equation:

$$ A_1v_1 = A_2v_2 $$

where

$$A_1$$ is the cross-sectional area of the piston,

$$v_1$$ is the speed of the piston,

$$A_2$$ is the cross-sectional area of the nozzle, and

$$v_2$$ is the velocity of the fluid (air) leaving the nozzle.

We can use this equation to find the speed of air leaving the nozzle. Given that the piston's speed is 5 mm/s and its radius is 20 mm, we have

$$ A_1 = \pi (20\, \text{mm})^2 = 400\pi\, \text{mm}^2 $$

and

$$ v_1 = 5\, \text{mm/s} $$

The nozzle's radius is 1 mm, thus

$$ A_2 = \pi (1\, \text{mm})^2 = \pi\, \text{mm}^2 $$

Substituting the values into the continuity equation, we can solve for $$v_2$$:

$$ A_1v_1 = A_2v_2 \rightarrow 400\pi\, \text{mm}^2 \times 5\, \text{mm/s} = \pi\, \text{mm}^2 \times v_2 \rightarrow v_2 = \frac{400\pi\, \text{mm}^2 \times 5\, \text{mm/s}}{\pi\, \text{mm}^2} = 2000\, \text{mm/s} $$

Converting this to meters per second, we get

$$ v_2 = 2000\, \text{mm/s} \times \frac{1\, \text{m}}{1000\, \text{mm}} = 2\, \text{m/s} $$

Therefore, the air comes out of the nozzle with a speed of 2 m/s, which corresponds to Option C.

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