Fluid Statics : Pressure Variation and Manometers

Fluid Statics

In fluid statics there is no relative motion between fluid particles so there are no shear stresses present (a shear results from a velocity gradient). This does not mean that the fluid particles are not moving, only that they are not moving relative to one another. If they are moving, as in a can of water rotating about its axis, they move as a solid body. The only stress involved in fluid statics is the normal stress, the pressure. It is the pressure acting over an area that gives rise to the force. Three types of problems are presented in this chapter: fluids at rest, as in the design of a dam; flu- ids undergoing linear acceleration, as in a rocket; and fluids that are rotating about an axis.

2.1 Pressure Variation

Pressure is a quantity that acts at a point. But, does it have the same magnitude in all directions at the point? To answer this question, consider Fig. 2.1. A pressure p is assumed to act on the hypotenuse and different pressures p and p on the other two sides of the infinitesimal element which has a uniform depth dz into the paper.

image

Figure 2.1 Pressure acting on an infinitesimal element.

The fluid particle occupying the fluid element could be accelerating so we apply Newton’s second law in both the x- and y-directions:

image

Here we see that the quantities on the right-hand sides of the equations are infinitesimal (multiplied by dx and dy), and can be neglected2 so that Since the angle b is arbitrary, this holds for all angles. We could have selected dimensions dx and dz and arrived at px = pz = p. So, in our applications to fluid statics, the pressure is a scalar function that acts equally in all directions at a point.

In the preceding discussion, pressure at a point was considered. But, how does pressure vary from point to point? The fluid element of depth dy in Fig. 2.2 is assumed to be accelerating. Newton’s second law provides

image

If the element were shown in the y-direction also, the y-component equation would be

imageFigure 2.2 Forces acting on an element of fluid.

Finally, the pressure differential can be written as

image

This can be integrated to give the desired difference in pressure between specified points in a fluid.

In a fluid at rest, there is no acceleration so the pressure variation from Eq. (2.8) is

imageThis implies that as the elevation z increases, the pressure decreases, a fact that we are aware of in nature; the pressure increases with depth in the ocean and decreases with height in the atmosphere.

If g is constant, Eq. (2.9) allows us to write

imagewhere Δp is the pressure change over the elevation change Δz. If we desire an expression for the pressure, a distance h below a free surface (the pressure is zero on a free surface), it would be

p = γ h                                    2.11)

where h = −Δz. Equation (2.11) is used to convert pressure to an equivalent height of a liquid; atmospheric pressure is often expressed as millimeters of mercury (the pressure at the bottom of a 30-in column of mercury is the same as the pressure at the earth’s surface due to the entire atmosphere).

If the pressure variation in the atmosphere is desired, Eq. (2.9) would be used with the ideal-gas law p = ρRT to give

imagewhere p0 is the pressure at z = 0. If the temperature could be assumed constant over the elevation change, this could be integrated to obtain

image

In the troposphere (between the earth’s surface and an elevation of about 10 km), the temperature in kelvins is T = 288 − 0.0065z; Eq. (2.12) can be integrated to give the pressure variation.

EXAMPLE 2.1

Convert 230 kPa to millimeters of mercury, inches of mercury, and feet of water.

Solution

Equation (2.11) is applied using the specific weight of mercury as 13.6γ water:

image

We could have converted meters of mercury to feet of mercury and then multi- plied by 13.6 to obtain feet of water.

2.2 Manometers

A manometer is an instrument that uses a column of a liquid to measure pressure. A typical U-tube manometer containing mercury is attached to a water pipe, as shown in Fig. 2.3. There are several ways to analyze a manometer. One way is to identify two points that have the same pressure, i.e., they are at the same elevation in the same liquid, such as points 2 and 3. Then we write

image

Since point 4 is shown to be open to the atmosphere, p4 = 0. Thus, the manometer would measure the pressure p1 in the pipe to be

image

image

Figure 2.3 A U-tube manometer using water and mercury.

Some manometers will have several fluids with several interfaces. Each interface should be located with a point when analyzing a manometer.

EXAMPLE 2.2

A manometer connects an oil pipeline and a water pipeline, as shown. Determine the difference in pressure between the two pipelines using the readings on the manometer. Use Soil = 0.86 and SHg = 13.6.

imageSolution

The points of interest have been positioned on the manometer shown. The pres- sure at point 2 is equal to the pressure at point 3:

image 

Observe that the heights must be in meters. The pressure at point 4 is essentially the same as that at point 5 since the specific weight of air is negligible compared to that of the oil. So,

image

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Fluid Statics : Pressure Variation and Manometers

Fluid Statics

In fluid statics there is no relative motion between fluid particles so there are no shear stresses present (a shear results from a velocity gradient). This does not mean that the fluid particles are not moving, only that they are not moving relative to one another. If they are moving, as in a can of water rotating about its axis, they move as a solid body. The only stress involved in fluid statics is the normal stress, the pressure. It is the pressure acting over an area that gives rise to the force. Three types of problems are presented in this chapter: fluids at rest, as in the design of a dam; flu- ids undergoing linear acceleration, as in a rocket; and fluids that are rotating about an axis.

2.1 Pressure Variation

Pressure is a quantity that acts at a point. But, does it have the same magnitude in all directions at the point? To answer this question, consider Fig. 2.1. A pressure p is assumed to act on the hypotenuse and different pressures p and p on the other two sides of the infinitesimal element which has a uniform depth dz into the paper.

image

Figure 2.1 Pressure acting on an infinitesimal element.

The fluid particle occupying the fluid element could be accelerating so we apply Newton’s second law in both the x- and y-directions:

image

Here we see that the quantities on the right-hand sides of the equations are infinitesimal (multiplied by dx and dy), and can be neglected2 so that Since the angle b is arbitrary, this holds for all angles. We could have selected dimensions dx and dz and arrived at px = pz = p. So, in our applications to fluid statics, the pressure is a scalar function that acts equally in all directions at a point.

In the preceding discussion, pressure at a point was considered. But, how does pressure vary from point to point? The fluid element of depth dy in Fig. 2.2 is assumed to be accelerating. Newton’s second law provides

image

If the element were shown in the y-direction also, the y-component equation would be

imageFigure 2.2 Forces acting on an element of fluid.

Finally, the pressure differential can be written as

image

This can be integrated to give the desired difference in pressure between specified points in a fluid.

In a fluid at rest, there is no acceleration so the pressure variation from Eq. (2.8) is

imageThis implies that as the elevation z increases, the pressure decreases, a fact that we are aware of in nature; the pressure increases with depth in the ocean and decreases with height in the atmosphere.

If g is constant, Eq. (2.9) allows us to write

imagewhere Δp is the pressure change over the elevation change Δz. If we desire an expression for the pressure, a distance h below a free surface (the pressure is zero on a free surface), it would be

p = γ h                                    2.11)

where h = −Δz. Equation (2.11) is used to convert pressure to an equivalent height of a liquid; atmospheric pressure is often expressed as millimeters of mercury (the pressure at the bottom of a 30-in column of mercury is the same as the pressure at the earth’s surface due to the entire atmosphere).

If the pressure variation in the atmosphere is desired, Eq. (2.9) would be used with the ideal-gas law p = ρRT to give

imagewhere p0 is the pressure at z = 0. If the temperature could be assumed constant over the elevation change, this could be integrated to obtain

image

In the troposphere (between the earth’s surface and an elevation of about 10 km), the temperature in kelvins is T = 288 − 0.0065z; Eq. (2.12) can be integrated to give the pressure variation.

EXAMPLE 2.1

Convert 230 kPa to millimeters of mercury, inches of mercury, and feet of water.

Solution

Equation (2.11) is applied using the specific weight of mercury as 13.6γ water:

image

We could have converted meters of mercury to feet of mercury and then multi- plied by 13.6 to obtain feet of water.

2.2 Manometers

A manometer is an instrument that uses a column of a liquid to measure pressure. A typical U-tube manometer containing mercury is attached to a water pipe, as shown in Fig. 2.3. There are several ways to analyze a manometer. One way is to identify two points that have the same pressure, i.e., they are at the same elevation in the same liquid, such as points 2 and 3. Then we write

image

Since point 4 is shown to be open to the atmosphere, p4 = 0. Thus, the manometer would measure the pressure p1 in the pipe to be

image

image

Figure 2.3 A U-tube manometer using water and mercury.

Some manometers will have several fluids with several interfaces. Each interface should be located with a point when analyzing a manometer.

EXAMPLE 2.2

A manometer connects an oil pipeline and a water pipeline, as shown. Determine the difference in pressure between the two pipelines using the readings on the manometer. Use Soil = 0.86 and SHg = 13.6.

imageSolution

The points of interest have been positioned on the manometer shown. The pres- sure at point 2 is equal to the pressure at point 3:

image 

Observe that the heights must be in meters. The pressure at point 4 is essentially the same as that at point 5 since the specific weight of air is negligible compared to that of the oil. So,

image

Leave a comment

Your email address will not be published. Required fields are marked *