Physiscs

Chapter 14: Fluid Mechanics

Imron Rosyadi

Chapter 14.1: Fluids, Density, and Pressure

Learning Objectives

By the end of this section, you will be able to:

  • State the different phases of matter.
  • Describe the characteristics of the phases of matter at the molecular or atomic level.
  • Distinguish between compressible and incompressible materials.
  • Define density and its related SI units.
  • Compare and contrast the densities of various substances.
  • Define pressure and its related SI units.
  • Explain the relationship between pressure and force.
  • Calculate force given pressure and area.

Phases of Matter

Matter exists commonly as:

  • Solid: Rigid, specific shape, definite volume.
    • Atoms/molecules are in close proximity with strong forces, forming a lattice structure.
    • Resist shearing forces.
  • Liquid: Indefinite shape, definite volume.
    • Molecules bonded but can move past each other.
    • Yield to shearing forces; they flow.
    • Resist compression like solids.
  • Gas: Indefinite shape, indefinite volume.
    • Molecules far apart, weak forces.
    • Easily compressible; they flow and expand to fill containers.

Molecular Arrangement in Phases

Figure 14.2: (a) Solid (b) Liquid (c) Gas

  • Solid (a): Atoms are in close contact, held in fixed positions by strong forces (like springs).
    • Limited movement.
  • Liquid (b): Atoms are in close contact but can slide over one another.
    • Fewer bonds, allowing for flow.
  • Gas (c): Atoms move about freely and are separated by large distances.
    • Very weak forces; expands to fill container.

Compressible vs. Incompressible Fluids

  • Incompressible Fluid: Requires an extremely large force to change its volume.
    • Liquids (e.g., water) are generally considered incompressible.
    • Molecules are closely packed.
  • Compressible Fluid: Volume changes significantly with pressure.
    • Gases (e.g., air) are highly compressible.
    • Molecules are far apart, with weak interactions.

Note

In fluid mechanics, we often treat liquids as incompressible, which simplifies many calculations. Gases, however, are almost always treated as compressible.

Density (\(\rho\))

  • Definition: Mass per unit volume.

\[ \rho = \frac{m}{V} \]

  • SI Unit: Kilograms per cubic meter (\(\text{kg/m}^3\)).
    • Common cgs unit: \(\text{g/cm}^3\) (\(1 \text{ g/cm}^3 = 1000 \text{ kg/m}^3\)).
  • Density determines if an object floats or sinks.
    • Example: Wood floats in water because its density is less than water’s. Brass sinks because its density is greater.

Density and Floating

Figure 14.3: (a) Same mass, different volumes. (b) Brass sinks, wood floats.

  • Even if a block of brass and a block of wood have the same mass (and thus weight):
    • Brass has a smaller volume, meaning higher density.
    • Wood has a larger volume, meaning lower density.
  • When placed in water:
    • Brass (\(\rho_{brass} > \rho_{water}\)) sinks.
    • Wood (\(\rho_{wood} < \rho_{water}\)) floats.

Densities of Common Substances

Substance \(\rho (\text{kg/m}^3)\) Phase
Gold \(1.93 \times 10^4\) Solid
Lead \(1.13 \times 10^4\) Solid
Mercury \(1.36 \times 10^4\) Liquid
Water (\(4.0^\circ\text{C}\)) \(1.000 \times 10^3\) Liquid
Ice (\(0^\circ\text{C}\)) \(9.17 \times 10^2\) Solid
Oak \(7.10 \times 10^2\) Solid
Air (\(0^\circ\text{C}\)) \(1.29 \times 10^0\) Gas
Hydrogen (\(0^\circ\text{C}\)) \(9.00 \times 10^{-2}\) Gas

Tip

Densities of liquids and solids are roughly comparable and much greater than gases. Gases are highly dependent on temperature and pressure. Water has a unique density behavior, reaching maximum density at \(4.0^\circ\text{C}\), explaining why ice floats.

Homogeneous vs. Heterogeneous Substances

  • Homogeneous Substance: Density is constant throughout.
    • Example: A solid iron bar.
  • Heterogeneous Substance: Density varies within the substance.
    • Example: Swiss cheese (cheese + gas voids).
    • Local Density: \(\rho = \lim_{\Delta V \to 0} \frac{\Delta m}{\Delta V}\)

Figure 14.4: Local density in a heterogeneous mixture.

Specific Gravity

  • Definition: Ratio of a material’s density to the density of water at \(4.0^\circ\text{C}\) (\(1000 \text{ kg/m}^3\)). \[ \text{Specific gravity} = \frac{\text{Density of material}}{\text{Density of water}} \]
  • Dimensionless Quantity: Useful for comparing densities without units.
  • Example: Aluminum has a specific gravity of 2.7, meaning it’s 2.7 times denser than water.

Pressure (p)

  • Definition: Normal force F per unit area A over which the force is applied. \[ p = \frac{F}{A} \]
  • Pressure at a point: \(p = \frac{dF}{dA}\) for an infinitesimal area.
  • SI Unit: Pascal (Pa), where \(1 \text{ Pa} = 1 \text{ N/m}^2\).
  • Scalar Quantity: Pressure has no direction, but the force due to pressure is always perpendicular to the surface.

Pressure and Force

Figure 14.5: (a) Finger (b) Needle.

  • The effect of a force depends heavily on the area over which it’s applied.
  • Example:
    • A finger applies force over a large area, resulting in low pressure.
    • A needle applies the same force over a tiny area, resulting in very high pressure.

Pressure in a Fluid of Constant Density

  • Pressure in a static fluid increases with depth.
  • The pressure at a depth h below the surface of a fluid with constant density \(\rho\) is: \[ p = p_0 + \rho g h \]
    • \(p_0\): atmospheric pressure at the surface.
    • \(\rho\): fluid density.
    • \(g\): acceleration due to gravity.
    • \(h\): depth.

Figure 14.6: Pressure at the bottom of a container.

Example: Dam Force

A dam retaining a reservoir.

Problem: A dam is 500-m wide, and water is 80.0-m deep.

  1. What is the average pressure on the dam due to water?
  2. Calculate the force against the dam.

Solution:

  1. Average depth \(h = 40.0 \text{ m}\).

\(p = \rho g h = (10^3 \text{ kg/m}^3)(9.80 \text{ m/s}^2)(40.0 \text{ m}) = 3.92 \times 10^5 \text{ N/m}^2 = 392 \text{ kPa}\).

  1. Area \(A = (80.0 \text{ m})(500 \text{ m}) = 4.00 \times 10^4 \text{ m}^2\).

\(F = p A = (3.92 \times 10^5 \text{ N/m}^2)(4.00 \times 10^4 \text{ m}^2) = 1.57 \times 10^{10} \text{ N}\).

Pressure and Container Shape

Figure 14.9: Fluid levels in connected containers of different shapes.

  • The pressure in a fluid depends only on the depth from the surface, not on the shape of the container.
  • This is why liquids seek the same level in interconnected containers, regardless of their shape.

Atmospheric Pressure Variation with Height

  • Unlike liquids, air density changes significantly with height.
  • Assuming constant air temperature and ideal gas behavior, atmospheric pressure drops exponentially with height: \[ p(y) = p_0 \exp(-\alpha y) \]
    • \(p_0\): pressure at sea level.
    • \(\alpha = \frac{mg}{k_B T}\) is a constant.
    • \(1/\alpha\) is the pressure scale height (approx. 8800 m for Earth’s atmosphere).

Caution

This exponential drop is an approximation assuming constant temperature and gravity, which isn’t perfectly true over large distances.

Pressure Direction in Fluids

Figure 14.10: (a) Tire pressure (b) Swimmer.

  • Fluid pressure is a scalar, but the forces due to pressure are always exerted perpendicular to any surface.
  • Fluids cannot withstand shearing forces.
  • This is evident in:
    • Tire walls (air pushes outwards perpendicularly).
    • Swimmers (water pushes inward perpendicularly from all directions, with greater force from below due to depth).

Chapter 14.2: Measuring Pressure

Learning Objectives

By the end of this section, you will be able to:

  • Define gauge pressure and absolute pressure.
  • Explain various methods for measuring pressure.
  • Understand the working of open-tube barometers.
  • Describe in detail how manometers and barometers operate.

Gauge Pressure vs. Absolute Pressure

  • Gauge Pressure (\(p_g\)): Pressure relative to atmospheric pressure.
    • Most common pressure gauges (e.g., tire pressure, scuba tanks) read zero at atmospheric pressure.
    • Can be positive (above atmospheric) or negative (below atmospheric, like in a vacuum chamber).
  • Absolute Pressure (\(p_{abs}\)): Total pressure, including atmospheric pressure. \[ p_{abs} = p_g + p_{atm} \]
    • Cannot be negative for fluids (fluids push, not pull). Minimum absolute pressure is zero (perfect vacuum).

Important

Always be clear whether a pressure value refers to gauge or absolute pressure, especially in problem-solving. Unless stated otherwise, assume gauge pressure in everyday contexts.

Pressure Measuring Devices

Figure 14.11: (a) Gas cylinder gauge (b) Tire gauge (c) Ionization gauge.

Various devices measure pressure:

  • Mechanical gauges: (a) Gas cylinder gauges, (b) tire gauges.
  • Strain gauges: Measure material shape change due to pressure.
  • Capacitance pressure gauges: Measure capacitance change due to shape.
  • Piezoelectric pressure gauges: Generate voltage from pressure difference.
  • Ion gauges: Measure pressure by ionizing molecules in vacuum systems (c).

Manometers

Figure 14.12: Open-tube manometers.

  • U-shaped tube filled with a fluid (often mercury).
  • Measures gauge pressure by comparing fluid levels.
  • One side open to atmosphere (\(p_{atm}\)).
  • Gauge pressure: \(p_g = h \rho g\).
      1. If \(p_{abs} > p_{atm}\), \(p_g\) is positive.
      1. If \(p_{abs} < p_{atm}\), \(p_g\) is negative.
    • The difference in height, \(h\), indicates the pressure difference.

Barometers

Figure 14.13: A mercury barometer.

  • Invented by Torricelli in 1643.
  • Measures atmospheric pressure.
  • A glass tube, closed at one end and filled with mercury, inverted into a pool of mercury.
  • A near-perfect vacuum exists above the mercury column in the tube.
  • Atmospheric pressure supports the column of mercury: \(h \rho g = p_{atm}\).
  • Used by meteorologists for weather forecasting (rising mercury = improving weather).

Fluid Heights in an Open U-Tube Example

Figure 14.14: Two liquids in a U-tube.

Problem: Two immiscible liquids of densities \(\rho_1\) and \(\rho_2\) (\(\rho_2 < \rho_1\)) are in an open U-tube. Derive a formula for the height difference \(h_2 - h_1\).

Solution: Equate pressures at the interface level in both arms: \(p_0 + \rho_1 g h_1 = p_0 + \rho_2 g h_2\) \(\rho_1 h_1 = \rho_2 h_2\) \(h_1 = \frac{\rho_2}{\rho_1} h_2\) Height difference: \(h_2 - h_1 = h_2 - \frac{\rho_2}{\rho_1} h_2 = (1 - \frac{\rho_2}{\rho_1}) h_2\).

Units of Pressure

Unit Definition
Pascal (Pa) \(1 \text{ N/m}^2\)
pounds per square inch (psi) \(1 \text{ psi} = 6.895 \times 10^3 \text{ Pa}\)
Atmosphere (atm) \(1 \text{ atm} = 1.013 \times 10^5 \text{ Pa} = 760 \text{ mm Hg} = 14.7 \text{ psi}\)
Millibar (mbar) \(1 \text{ mbar} = 100 \text{ Pa}\) (\(1000 \text{ mbar} = 1 \times 10^5 \text{ Pa}\))
Torr \(1 \text{ torr} = 1 \text{ mm Hg} = 133.3 \text{ Pa}\)
Bar \(1 \text{ bar} = 10^5 \text{ Pa}\)

Chapter 14.3: Pascal’s Principle and Hydraulics

Learning Objectives

By the end of this section, you will be able to:

  • State Pascal’s principle.
  • Describe applications of Pascal’s principle.
  • Derive relationships between forces in a hydraulic system.

Pascal’s Principle

  • Statement: When a change in pressure is applied to an enclosed fluid, it is transmitted undiminished to all portions of the fluid and to the walls of its container.
  • This principle applies to the change in pressure, not necessarily the absolute pressure being the same everywhere (as pressure still varies with depth).

Figure 14.15: Pressure change in a fluid with a piston.

  • If you add a weight \(Mg\) to a piston of area \(A\), the pressure at the top increases by \(\Delta p = \frac{Mg}{A}\).
  • According to Pascal’s principle, this \(\Delta p\) is transmitted throughout the entire fluid.
    • \(\Delta p_{top} = \Delta p_{bottom} = \Delta p_{everywhere}\).

Applications of Pascal’s Principle: Hydraulic Systems

Figure 14.16: A typical hydraulic system.

  • Hydraulic systems use Pascal’s principle to multiply forces.
  • An input force \(F_1\) on a small area \(A_1\) creates a pressure \(p_1 = F_1/A_1\).
  • This pressure is transmitted to a larger area \(A_2\), creating a larger output force \(F_2\).
  • Since \(p_1 = p_2\) (assuming same height, negligible friction): \[ \frac{F_1}{A_1} = \frac{F_2}{A_2} \]
    • If \(A_2 > A_1\), then \(F_2 > F_1\).

Hydraulic Jack

Figure 14.17: (a) Hydraulic jack principle (b) Car on a hydraulic jack.

  • A small input force (\(F_1\)) over a small piston area (\(A_1\)) lifts a large load (\(F_2\)) on a large piston area (\(A_2\)).
  • The ratio of forces is directly proportional to the ratio of areas: \[ F_2 = F_1 \frac{A_2}{A_1} \]
  • Commonly used to lift heavy objects like cars.

Example: Calculating Force on Wheel Cylinders (Automobile Brakes)

Figure 14.18: Hydraulic brake system.

Problem: A 500 N force is exerted on a pedal cylinder (master cylinder) with diameter 0.500 cm. Each wheel cylinder has a diameter of 2.50 cm. Calculate the force \(F_2\) at each wheel cylinder.

Solution:

\(F_1 = 500 \text{ N}\)

\(d_1 = 0.500 \text{ cm} \Rightarrow r_1 = 0.250 \text{ cm}\)

\(d_2 = 2.50 \text{ cm} \Rightarrow r_2 = 1.25 \text{ cm}\)

Using \(\frac{F_1}{A_1} = \frac{F_2}{A_2}\):

\(F_2 = F_1 \frac{A_2}{A_1} = F_1 \frac{\pi r_2^2}{\pi r_1^2} = F_1 \frac{r_2^2}{r_1^2}\)

\(F_2 = (500 \text{ N}) \frac{(1.25 \text{ cm})^2}{(0.250 \text{ cm})^2} = (500 \text{ N}) \frac{1.5625}{0.0625} = 1.25 \times 10^4 \text{ N}\).

Chapter 14.4: Archimedes’ Principle and Buoyancy

Learning Objectives

By the end of this section, you will be able to:

  • Define buoyant force.
  • State Archimedes’ principle.
  • Describe the relationship between density and Archimedes’ principle.

Buoyant Force (\(F_B\))

  • Definition: The upward force on any object in any fluid.
  • Arises because pressure increases with depth.
    • Upward force on the bottom of an object is greater than the downward force on the top.
  • Result: Net upward force on the object.
  • Present whether an object floats, sinks, or is suspended.

Figure 14.20: Net buoyant force on an object.

Archimedes’ Principle

  • Statement: The buoyant force on an object equals the weight of the fluid it displaces.

\[ F_B = w_{fl} \]

-   $F_B$: buoyant force.
-   $w_{fl}$: weight of the fluid displaced by the object.

Figure 14.21: Buoyant force equals weight of displaced fluid.

  • Named after Archimedes of Syracuse.
  • When an object is submerged, it pushes aside, or displaces, a certain volume of fluid. The weight of that displaced fluid is exactly the buoyant force acting on the object.

Density and Archimedes’ Principle

  • An object’s average density determines if it floats:
    • If \(\rho_{obj} < \rho_{fl}\): Object floats.
    • If \(\rho_{obj} > \rho_{fl}\): Object sinks.
    • If \(\rho_{obj} = \rho_{fl}\): Object remains suspended (neutrally buoyant).
  • Fraction submerged: For a floating object, the fraction of its volume submerged is: \[ \text{fraction submerged} = \frac{V_{sub}}{V_{obj}} = \frac{\rho_{obj}}{\rho_{fl}} \]

Figure 14.22: Unloaded vs. loaded ship.

Example: Calculating Average Density

Problem: A 60.0-kg woman floats in fresh water with 97.0% of her volume submerged when her lungs are full of air. What is her average density?

Given:

\(m_{person} = 60.0 \text{ kg}\)

Fraction submerged = 0.970

\(\rho_{water} = 1.000 \times 10^3 \text{ kg/m}^3\)

Solution:

Using the formula for fraction submerged:

\(\text{fraction submerged} = \frac{\rho_{obj}}{\rho_{fl}}\)

\(\rho_{person} = (\text{fraction submerged}) \times \rho_{water}\)

\(\rho_{person} = (0.970) \times (1.000 \times 10^3 \text{ kg/m}^3) = 970 \text{ kg/m}^3\).

Significance: Her average density is indeed less than water, which is why she floats.

Measuring Density with Apparent Weight

Figure 14.23: Weighing a coin in air and water.

  • An object’s apparent weight when submerged is less than its actual weight in air.
  • Apparent weight loss = Weight of fluid displaced = Buoyant force.
  • By weighing an object in air (\(W_{air}\)) and then submerged in a fluid (\(W_{app}\)): \(F_B = W_{air} - W_{app}\) Since \(F_B = \rho_{fl} g V_{obj}\) and \(W_{air} = \rho_{obj} g V_{obj}\): \(\rho_{obj} = \rho_{fl} \frac{W_{air}}{W_{air} - W_{app}}\)
  • This technique can be used to find either \(\rho_{obj}\) (if \(\rho_{fl}\) is known) or \(\rho_{fl}\) (if \(\rho_{obj}\) is known).

Chapter 14.5: Fluid Dynamics

Learning Objectives

By the end of this section, you will be able to:

  • Describe the characteristics of flow.
  • Calculate flow rate.
  • Describe the relationship between flow rate and velocity.
  • Explain the consequences of the equation of continuity to the conservation of mass.

Characteristics of Flow: Streamlines

  • Streamline: Represents the path of a small volume of fluid as it flows.
    • The velocity vector is always tangential to the streamline.
  • Laminar Flow (Steady Flow): Smooth, parallel streamlines.
    • Layers flow without mixing.
    • Velocity may vary across the flow (e.g., faster in the center of a pipe due to viscosity).
  • Turbulent Flow: Irregular, chaotic streamlines that change over time.
    • Fluid mixes, forming eddies and whirlpools.
    • Occurs at high speeds or due to obstructions.

Figure 14.25: (a) Laminar flow (b) Turbulent flow.

Flow Rate (\(Q\))

  • Volume Flow Rate: Volume of fluid passing a given location through an area per unit time. \[ Q = \frac{V}{t} \]
  • Relationship to Velocity: \[ Q = Av \]
    • \(A\): cross-sectional area of flow.
    • \(v\): average speed of the fluid.
  • SI Unit: \(\text{m}^3/\text{s}\). (Liters/minute are also common).

Figure 14.26: Volume flow rate.

The Equation of Continuity

  • For an incompressible fluid (constant density) in steady flow, the flow rate is constant throughout the pipe.
    • No fluid is created or destroyed.
    • Mass conservation implies volume flow rate conservation. \[ Q_1 = Q_2 \] \[ A_1 v_1 = A_2 v_2 \]
    • If the cross-sectional area decreases, the fluid speed must increase (and vice versa).

Figure 14.27: Fluid speed increases when a tube narrows.

Example: Calculating Fluid Speed through a Nozzle

Problem: A nozzle with diameter 0.500 cm is attached to a hose with radius 0.900 cm. The flow rate is 0.500 L/s. Calculate the speed of water (a) in the hose and (b) in the nozzle.

Given:

\(Q = 0.500 \text{ L/s} = 0.500 \times 10^{-3} \text{ m}^3/\text{s}\)

Hose: \(r_1 = 0.900 \text{ cm} = 0.00900 \text{ m}\)

Nozzle: \(d_2 = 0.500 \text{ cm} \Rightarrow r_2 = 0.250 \text{ cm} = 0.00250 \text{ m}\)

Solution:

  1. Speed in the hose (\(v_1\)):

\(A_1 = \pi r_1^2 = \pi (0.00900 \text{ m})^2\)

\(v_1 = \frac{Q}{A_1} = \frac{0.500 \times 10^{-3} \text{ m}^3/\text{s}}{\pi (0.00900 \text{ m})^2} = 1.96 \text{ m/s}\).

  1. Speed in the nozzle (\(v_2\)):

Using the equation of continuity \(A_1 v_1 = A_2 v_2\):

\(v_2 = v_1 \frac{A_1}{A_2} = v_1 \frac{\pi r_1^2}{\pi r_2^2} = v_1 \left(\frac{r_1}{r_2}\right)^2\)

\(v_2 = (1.96 \text{ m/s}) \left(\frac{0.900 \text{ cm}}{0.250 \text{ cm}}\right)^2 = (1.96 \text{ m/s}) (3.6)^2 = 25.5 \text{ m/s}\).

Mass Flow Rate and General Continuity Equation

  • Mass Flow Rate (\(\frac{dm}{dt}\)): The rate at which mass of fluid moves past a point.

    \[ \frac{dm}{dt} = \rho A v \]

  • General Continuity Equation: For any fluid (compressible or incompressible), mass flow rate is conserved:

    \[ \left(\frac{dm}{dt}\right)_1 = \left(\frac{dm}{dt}\right)_2 \]

    \[ \rho_1 A_1 v_1 = \rho_2 A_2 v_2 \]

  • If the fluid is incompressible (\(\rho_1 = \rho_2\)), then \(\rho\) cancels, returning \(A_1 v_1 = A_2 v_2\).

Chapter 14.6: Bernoulli’s Equation

Learning Objectives

By the end of this section, you will be able to:

  • Explain the terms in Bernoulli’s equation.
  • Explain how Bernoulli’s equation is related to the conservation of energy.
  • Describe how to derive Bernoulli’s principle from Bernoulli’s equation.
  • Perform calculations using Bernoulli’s principle.
  • Describe some applications of Bernoulli’s principle.

Bernoulli’s Equation

  • Based on the conservation of energy for an incompressible, frictionless fluid in laminar flow.
  • It states that along a streamline, the sum of pressure, kinetic energy density, and potential energy density is constant: \[ p + \frac{1}{2} \rho v^2 + \rho g y = \text{constant} \]
    • \(p\): absolute pressure.
    • \(\frac{1}{2} \rho v^2\): kinetic energy density (dynamic pressure).
    • \(\rho g y\): potential energy density (hydrostatic pressure).

Figure 14.30: Geometry for deriving Bernoulli’s equation.

Analyzing Bernoulli’s Equation

  • Energy Transformation: Pressure, kinetic energy density, and potential energy density can interconvert, but their sum remains constant.
  • Pressure Drop with Speed: As fluid speed (v) increases, the pressure (p) tends to decrease (assuming constant height), to keep the sum constant.
    • Examples: Shower curtain bulging inward, cars pulling towards trucks on a highway.

Figure 14.29: Pressure drop between passing vehicles.

Special Cases of Bernoulli’s Equation

  1. Static Fluids (\(v_1 = v_2 = 0\)):

    \[ p_1 + \rho g y_1 = p_2 + \rho g y_2 \]

    If \(y_2 = 0\), then \(p_2 = p_1 + \rho g y_1\). This confirms pressure increases with depth, as seen in fluid statics.

  2. Bernoulli’s Principle (Constant Depth, \(y_1 = y_2\)):

    \[ p_1 + \frac{1}{2} \rho v_1^2 = p_2 + \frac{1}{2} \rho v_2^2 \]

    This clearly shows that if \(v_2 > v_1\), then \(p_2 < p_1\). Pressure drops as speed increases.

Example: Calculating Pressure in a Hose

Problem: Water speed in a hose increases from 1.96 m/s to 25.5 m/s in a nozzle. Absolute pressure in the nozzle is \(1.01 \times 10^5 \text{ N/m}^2\) (atmospheric). Assuming level, frictionless flow, calculate the pressure in the hose.

Given:

\(v_1 = 1.96 \text{ m/s}\) (hose)

\(v_2 = 25.5 \text{ m/s}\) (nozzle)

\(p_2 = 1.01 \times 10^5 \text{ Pa}\) (nozzle pressure)

\(\rho_{water} = 1000 \text{ kg/m}^3\)

Level flow implies \(y_1 = y_2\).

Solution:

Using Bernoulli’s principle: \(p_1 + \frac{1}{2} \rho v_1^2 = p_2 + \frac{1}{2} \rho v_2^2\)

Solving for \(p_1\):

\(p_1 = p_2 + \frac{1}{2} \rho v_2^2 - \frac{1}{2} \rho v_1^2 = p_2 + \frac{1}{2} \rho (v_2^2 - v_1^2)\)

\(p_1 = 1.01 \times 10^5 \text{ Pa} + \frac{1}{2} (1000 \text{ kg/m}^3) [(25.5 \text{ m/s})^2 - (1.96 \text{ m/s})^2]\)

\(p_1 = 1.01 \times 10^5 \text{ Pa} + 500 \text{ kg/m}^3 [650.25 \text{ m}^2/\text{s}^2 - 3.84 \text{ m}^2/\text{s}^2]\)

\(p_1 = 1.01 \times 10^5 \text{ Pa} + 500 \text{ kg/m}^3 (646.41 \text{ m}^2/\text{s}^2)\)

\(p_1 = 1.01 \times 10^5 \text{ Pa} + 3.23 \times 10^5 \text{ Pa} = 4.24 \times 10^5 \text{ Pa}\).

Applications of Bernoulli’s Principle

  1. Entrainment: Using high-velocity fluid to create low pressure, which pulls other fluids into the stream.
    • Bunsen burners entrain air for combustion.
    • Atomizers entrain perfume drops.
    • Aspirators use water to create suction.
    • Chimneys entrain air to draw smoke up.

Figure 14.31: Entrainment devices.

Applications: Velocity Measurement

  • Devices like the Pitot tube use Bernoulli’s principle to measure fluid velocity.
  • By creating a “dead spot” (zero velocity) at one opening and measuring pressure at a point of flow, the pressure difference can be related to fluid speed. \[ p_1 = p_2 + \frac{1}{2} \rho v_2^2 \implies \frac{1}{2} \rho v_2^2 = p_1 - p_2 \] \[ v_2 = \sqrt{\frac{2(p_1 - p_2)}{\rho}} \]
  • Commonly used as air-speed indicators in aircraft.

Figure 14.32: Pitot tube for velocity measurement.

Chapter 14.7: Viscosity and Turbulence

Learning Objectives

By the end of this section, you will be able to:

  • Explain what viscosity is.
  • Calculate flow and resistance with Poiseuille’s law.
  • Explain how pressure drops due to resistance.
  • Calculate the Reynolds number for an object moving through a fluid.
  • Use the Reynolds number for a system to determine whether it is laminar or turbulent.
  • Describe the conditions under which an object has a terminal speed.

Viscosity and Laminar Flow

  • Viscosity (\(\eta\)): A measure of internal friction within a fluid and between fluid and surroundings.
    • Juice has low viscosity; maple syrup has high viscosity.
  • Laminar Flow: Fluid layers slide smoothly past each other without mixing.
  • Turbulence: Chaotic fluid flow with eddies and swirls, layers mix.
    • Caused by obstructions or high fluid speeds.

Figure 14.34: (a) Laminar flow (b) Turbulent flow.

Measuring Viscosity

  • Viscosity (\(\eta\)) is defined by applying a force \(F\) to move a top plate over a stationary bottom plate, with fluid in between. \[ F = \eta \frac{Av}{L} \]
    • \(A\): area of the plates.
    • \(v\): velocity of the top plate.
    • \(L\): distance between plates.
  • Solving for viscosity: \[ \eta = \frac{FL}{Av} \]
  • SI Unit: \(\text{Pa} \cdot \text{s}\) (Pascal-second).

Figure 14.36: Setup for measuring viscosity.

Poiseuille’s Law for Laminar Flow in Tubes

  • Flow rate (\(Q\)) in a horizontal tube is driven by a pressure difference (\(\Delta p = p_2 - p_1\)) and opposed by resistance (\(R\)). \[ Q = \frac{\Delta p}{R} \]
  • For laminar flow in a uniform tube of radius \(r\) and length \(l\) with fluid viscosity \(\eta\), the resistance (\(R\)) is: \[ R = \frac{8 \eta l}{\pi r^4} \]
  • Combining these gives Poiseuille’s Law for flow rate: \[ Q = \frac{(p_2 - p_1) \pi r^4}{8 \eta l} \]

Figure 14.38: Laminar flow in a pipe.

Example: Air Conditioning System Flow Rate

Problem: An AC system delivers air at gauge pressure 0.054 Pa (\(20^\circ\text{C}\)). Conduit: \(D = 18.00 \text{ cm}\), \(L = 20 \text{ m}\). Room: \(12 \text{ m} \times 6 \text{ m} \times 3 \text{ m}\).

  1. Volume flow rate assuming laminar flow?
  2. Time to replace air in the room?
  3. New flow rate if conduit \(D = 9.00 \text{ cm}\)?

Given:

\(\Delta p = 0.054 \text{ Pa}\)

\(\eta_{air} = 0.0181 \times 10^{-3} \text{ Pa} \cdot \text{s}\) (from Table 14.4)

Solution (a):

\(r = D/2 = 9.00 \text{ cm} = 0.09 \text{ m}\)

\(Q = \frac{\Delta p \pi r^4}{8 \eta l} = \frac{(0.054 \text{ Pa}) \pi (0.09 \text{ m})^4}{8 (0.0181 \times 10^{-3} \text{ Pa} \cdot \text{s}) (20 \text{ m})} = 3.84 \times 10^{-3} \text{ m}^3/\text{s}\).

Solution (b):

\(V_{room} = (12 \text{ m})(6 \text{ m})(3 \text{ m}) = 216 \text{ m}^3\)

\(\Delta t = \frac{V_{room}}{Q} = \frac{216 \text{ m}^3}{3.84 \times 10^{-3} \text{ m}^3/\text{s}} = 5.63 \times 10^4 \text{ s} \approx 15.6 \text{ hours}\).

Solution (c):

New radius \(r' = 4.50 \text{ cm} = 0.045 \text{ m}\) (half the original).

Since \(Q \propto r^4\), the new flow rate will be \(\left(\frac{r'}{r}\right)^4 Q = \left(\frac{0.045}{0.09}\right)^4 Q = \left(\frac{1}{2}\right)^4 Q = \frac{1}{16} Q\).

\(Q' = \frac{1}{16} (3.84 \times 10^{-3} \text{ m}^3/\text{s}) = 2.40 \times 10^{-4} \text{ m}^3/\text{s}\).

Flow and Resistance as Causes of Pressure Drops

  • Pressure drops occur due to fluid flow encountering resistance. \[ p_2 - p_1 = R Q \]
  • This equation is valid for both laminar and turbulent flows.
  • Consequences:
    • During heavy use (high \(Q\)), the pressure drop (\(p_2 - p_1\)) is large, leading to lower pressure (\(p_1\)) for users.
    • Resistance (\(R\)) is much greater in narrow sections, causing larger pressure drops there.
    • Turbulence greatly increases \(R\), leading to significant pressure reduction downstream.

Figure 14.39: Pressure drop in a water main.

Measuring Turbulence: The Reynolds Number

  • Reynolds Number (\(N_R\)): A dimensionless quantity that indicates whether flow is laminar or turbulent. \[ N_R = \frac{2 \rho v r}{\eta} \quad (\text{for flow in a tube}) \]
    • \(\rho\): fluid density.
    • \(v\): fluid speed.
    • \(r\): tube radius.
    • \(\eta\): fluid viscosity.
  • Turbulence Thresholds:
    • \(N_R < 2000\): Laminar flow.
    • \(N_R > 3000\): Turbulent flow.
    • \(2000 < N_R < 3000\): Unstable flow (can be laminar but easily becomes turbulent).

Note

Turbulence leads to increased energy dissipation (lost as heat and eddies), making flow less efficient.

Example: Turbulent Flow or Laminar Flow?

Problem: For the AC system (conduit \(D = 18.00 \text{ cm}\)) from Example 14.8, we found \(Q = 3.84 \times 10^{-3} \text{ m}^3/\text{s}\).

  1. Was the assumption of laminar flow valid?
  2. At what velocity would the flow become turbulent?

Given:

\(Q = 3.84 \times 10^{-3} \text{ m}^3/\text{s}\)

\(r = 0.09 \text{ m}\)

\(\rho_{air} = 1.23 \text{ kg/m}^3\) (from Table 14.1 at \(0^\circ\text{C}\), but usually taken as \(1.29 \text{ kg/m}^3\) for air, use \(1.23 \text{ kg/m}^3\) as given in prompt)

\(\eta_{air} = 0.0181 \times 10^{-3} \text{ Pa} \cdot \text{s}\)

Solution (a):

First, find velocity \(v = \frac{Q}{\pi r^2} = \frac{3.84 \times 10^{-3} \text{ m}^3/\text{s}}{\pi (0.09 \text{ m})^2} = 0.15 \text{ m/s}\).

Now, calculate Reynolds number:

\(N_R = \frac{2 \rho v r}{\eta} = \frac{2 (1.23 \text{ kg/m}^3) (0.15 \text{ m/s}) (0.09 \text{ m})}{0.0181 \times 10^{-3} \text{ Pa} \cdot \text{s}} = 1835\).

Since \(N_R = 1835 < 2000\), the flow is laminar. The assumption was valid.

Solution (b):

Flow becomes turbulent when \(N_R \approx 2000\).

\(v = \frac{N_R \eta}{2 \rho r} = \frac{2000 (0.0181 \times 10^{-3} \text{ Pa} \cdot \text{s})}{2 (1.23 \text{ kg/m}^3) (0.09 \text{ m})} = 0.16 \text{ m/s}\).

Key Takeaways

  • Phases of Matter: Solids are rigid, liquids flow and maintain volume, gases expand and are compressible.
  • Density (\(\rho = m/V\)): Mass per unit volume; determines floating/sinking. Pressure always pushes perpendicular to surfaces.
  • Pressure (\(p = F/A\)): Force per unit area. \(p = p_0 + \rho g h\) for static fluids of constant density.
  • Pascal’s Principle: Pressure changes in enclosed fluids transmit undiminished; basis for hydraulics (\(F_1/A_1 = F_2/A_2\)).
  • Archimedes’ Principle: Buoyant force equals weight of fluid displaced (\(F_B = w_{fl}\)).
  • Flow Rate (\(Q = Av\)): Volume of fluid per unit time.
  • Equation of Continuity (\(A_1 v_1 = A_2 v_2\)): For incompressible fluids, speed increases as area decreases.
  • Bernoulli’s Equation (\(p + \frac{1}{2} \rho v^2 + \rho g y = \text{constant}\)): Conservation of energy for ideal fluids, linking pressure, velocity, and height.
  • Viscosity (\(\eta\)): Fluid friction; higher viscosity means slower flow.
  • Poiseuille’s Law (\(Q = \frac{\Delta p \pi r^4}{8 \eta l}\)): Describes laminar flow rate in tubes; flow is highly sensitive to radius (\(r^4\)).
  • Reynolds Number (\(N_R = \frac{2 \rho v r}{\eta}\)): Predicts laminar (\(<2000\)) vs. turbulent (\(>3000\)) flow.

Key Equations

Equation Description
\(\rho = \frac{m}{V}\) Definition of density
\(p = \frac{F}{A}\) Definition of pressure
\(p = p_0 + \rho g h\) Pressure at a depth h in a fluid of constant density
\(p_{abs} = p_g + p_{atm}\) Relationship between absolute and gauge pressure
\(\frac{F_1}{A_1} = \frac{F_2}{A_2}\) Pascal’s principle in a hydraulic system
\(F_B = w_{fl}\) Archimedes’ principle (buoyant force)
\(\text{fraction submerged} = \frac{\rho_{obj}}{\rho_{fl}}\) Fraction of a floating object submerged
\(Q = Av\) Volume flow rate
\(A_1 v_1 = A_2 v_2\) Equation of continuity (for incompressible fluids)
\(p + \frac{1}{2} \rho v^2 + \rho g y = \text{constant}\) Bernoulli’s equation
\(Q = \frac{(p_2 - p_1) \pi r^4}{8 \eta l}\) Poiseuille’s law for laminar flow
\(N_R = \frac{2 \rho v r}{\eta}\) Reynolds number (for flow in a tube)

Key Terms

Term Definition
Absolute Pressure The sum of gauge pressure and atmospheric pressure.
Archimedes’ Principle The buoyant force on an object equals the weight of the fluid it displaces.
Bernoulli’s Equation States that the sum of pressure, kinetic energy density, and potential energy density is constant along a streamline for an ideal fluid.
Buoyant Force The upward force on an object in a fluid.
Density (\(\rho\)) Mass per unit volume.
Fluid Dynamics The study of fluids in motion.
Flow Rate (\(Q\)) Volume of fluid passing a point per unit time.
Gauge Pressure Pressure relative to atmospheric pressure.
Incompressible Fluid A fluid whose volume changes negligibly with pressure.
Laminar Flow Smooth, orderly fluid flow in layers without mixing.
Manometer A device for measuring pressure using a column of fluid.
Pascal’s Principle A change in pressure applied to an enclosed fluid is transmitted undiminished throughout the fluid.
Poiseuille’s Law Describes the laminar flow rate of a viscous fluid through a tube.
Pressure (\(p\)) Force per unit area.
Reynolds Number (\(N_R\)) A dimensionless quantity that predicts the onset of turbulence.
Specific Gravity Ratio of a substance’s density to water’s density at \(4.0^\circ\text{C}\).
Streamline The path followed by a small element of fluid.
Turbulence Chaotic, irregular fluid flow with eddies and swirls.
Viscosity (\(\eta\)) A measure of a fluid’s internal friction or resistance to flow.