Fluid Mechanics and Machinery

Chapter 1
Fluid Mechanics Foundations and Fluid Properties

Bachelors Program in Machine Technology
Fluid Mechanics and Machinery   •   Bachelor

Fluid Mechanics Foundations and Fluid Properties

Introduction

Fluid mechanics is the branch of engineering science concerned with the behavior of liquids and gases at rest and in motion. It provides the foundation for analyzing pumps, turbines, compressors, hydraulic systems, lubrication systems, pipelines, engines, cooling systems, and many manufacturing processes. In machine technology, an understanding of fluid properties is essential because those properties determine pressure losses, power requirements, sealing performance, heat transfer, cavitation risk, and component life.

A fluid differs from a solid primarily in its response to shear. A solid can sustain a static shear stress, whereas a fluid deforms continuously when subjected to any nonzero shear stress. Liquids and gases are both fluids, but liquids are relatively difficult to compress and generally form a free surface, while gases expand to occupy the available volume.

This chapter develops the continuum model of fluids and introduces the principal properties used in engineering analysis: density, specific weight, specific gravity, pressure, viscosity, surface tension, capillarity, vapor pressure, compressibility, and rheological behavior. Thermodynamic properties such as temperature, specific volume, internal energy, enthalpy, and entropy are also related to fluid-mechanical analysis.

Learning Objectives

After studying this chapter, the reader should be able to:

  1. Explain the continuum assumption and distinguish intensive from extensive properties.
  2. Use dimensions and SI units consistently in fluid calculations.
  3. Define and calculate pressure, density, specific weight, specific volume, and specific gravity.
  4. Explain absolute, gauge, and vacuum pressure.
  5. Distinguish dynamic and kinematic viscosity and apply Newton’s law of viscosity.
  6. Describe surface tension, capillarity, vapor pressure, cavitation, and compressibility.
  7. Compare Newtonian, non-Newtonian, ideal, and real-fluid behavior.
  8. Relate important thermodynamic properties to fluid-mechanics problems.
  9. Select appropriate property data and recognize modeling limitations.

1. The Fluid Continuum

Matter is composed of molecules separated by microscopic distances. At molecular scale, properties such as density fluctuate strongly. Engineering equations, however, require properties that vary smoothly in space and time. The continuum assumption treats a fluid as continuously distributed matter and assigns a meaningful value of density, pressure, and temperature to every point.

A representative elementary volume must be large compared with molecular spacing but small compared with the dimensions over which the macroscopic property changes significantly. For ordinary engineering flows this requirement is satisfied. It may fail in highly rarefied gases, micro- and nanoscale devices, or flows with very large molecular mean free paths. A useful measure is the Knudsen number:

Kn = λ / L

where λ is the molecular mean free path and L is a characteristic length. The continuum approximation is generally reliable when Kn is much less than 1. When Kn becomes significant, molecular or kinetic theory is required.

A fluid at rest cannot sustain a tangential shear stress. It can, however, sustain a normal stress, which is identified as pressure when the stress is isotropic. Fluids may transmit shear while moving, and the relation between shear stress and deformation rate is a central topic of rheology.

System and control volume

A system is a specified quantity of matter whose mass remains constant. A control volume is a selected region in space through which mass may flow. Fluid machinery is usually analyzed using control volumes because fluid enters and leaves pumps, turbines, valves, nozzles, and compressors. The choice between system and control-volume descriptions does not change the physical laws, but it changes the mathematical form used to apply them.

2. Dimensions, Units, and Fluid Variables

A dimension describes the physical nature of a quantity; a unit gives the numerical scale used to measure it. In the SI system, the base dimensions include mass M, length L, time T, and temperature Θ. Important derived dimensions include:

QuantitySymbolSI unitDimensions
LengthLmetre (m)L
Massmkilogram (kg)M
Timetsecond (s)T
ForceFnewton (N)ML T⁻²
Pressureppascal (Pa)ML⁻¹T⁻²
Densityρkg/m³ML⁻³
Dynamic viscosityμPa·sML⁻¹T⁻¹
Kinematic viscosityνm²/sL²T⁻¹
EnergyEjoule (J)ML²T⁻²

The newton is defined as 1 N = 1 kg·m/s², and the pascal is 1 Pa = 1 N/m². Dimensional homogeneity requires all terms added or equated in a valid physical equation to have identical dimensions. Unit consistency is a powerful method for detecting errors, but dimensional consistency alone cannot prove that an equation is physically correct.

Intensive and extensive properties

An extensive property depends on the amount of matter. Mass, total volume, total energy, and total momentum are extensive. An intensive property is independent of system size. Pressure, temperature, density, and viscosity are intensive. Specific properties are extensive properties per unit mass, such as specific volume and specific internal energy.

3. Density and Related Mass Properties

Density is mass per unit volume:

ρ = m / V

where ρ is density in kg/m³, m is mass in kg, and V is volume in m³. Density may vary with temperature, pressure, and composition. For a uniform fluid, m = ρV. For a nonuniform fluid, density is defined locally as the limit of mass divided by an infinitesimal volume.

Specific volume is volume per unit mass:

v = V / m = 1 / ρ

Its SI unit is m³/kg. The symbol v for specific volume must be distinguished from velocity, which is commonly denoted by V or V.

Specific weight is weight per unit volume:

γ = ρg

where γ is specific weight in N/m³ and g is gravitational acceleration, approximately 9.81 m/s² near Earth’s surface. Specific gravity is the ratio of a substance’s density to the density of a reference substance:

SG = ρ / ρref

For liquids, water at a specified reference temperature is commonly used; for gases, dry air may be used. Specific gravity is dimensionless. The reference condition must be stated because water density changes with temperature.

Worked Example 1: Density and specific weight

A 0.75 m³ tank contains 600 kg of hydraulic oil. Determine its density, specific volume, and specific weight, taking g = 9.81 m/s².

Density:

ρ = m/V = 600/0.75 = 800 kg/m³.

Specific volume:

v = 1/ρ = 1/800 = 0.00125 m³/kg.

Specific weight:

γ = ρg = 800 × 9.81 = 7,848 N/m³ = 7.848 kN/m³.

The results assume the oil is uniformly mixed and that gravitational acceleration is constant throughout the tank.

4. Pressure and Its Measurement

Pressure is the normal force exerted per unit area:

p = Fn / A

where p is pressure in pascals, Fₙ is normal force in newtons, and A is area in square metres. The definition applies to an average pressure over an area. A point pressure is obtained by considering an infinitesimal area.

In a fluid at rest, pressure acts normal to every surface and, at a point, has the same magnitude in all directions. This isotropic character follows from the absence of shear stress in static equilibrium.

Absolute, gauge, and vacuum pressure

Absolute pressure is measured relative to a perfect vacuum. Gauge pressure is measured relative to the local atmospheric pressure:

pabs = pg + patm

where p_abs is absolute pressure, p_g is gauge pressure, and p_atm is atmospheric pressure. If the pressure is below atmospheric pressure, the gauge pressure is negative. Vacuum pressure is often reported as:

pvac = patm − pabs

Pressure must be identified as absolute or gauge when applying gas laws, vapor-pressure comparisons, or compressor calculations. Pressure differences, such as those measured by many differential pressure gauges, are independent of the selected zero reference.

Hydrostatic pressure variation

For a fluid at rest with z measured upward, force equilibrium gives:

dp/dz = −ρg

If density is constant:

p₂ − p₁ = −ρg(z₂ − z₁)

or, for a depth h below a free surface exposed to pressure p₀:

p = p₀ + ρgh

This equation applies to a stationary fluid of constant density and uniform gravitational field. For a compressible fluid, density must be treated as a function of pressure and temperature.

Pressure-measuring devices

A piezometer measures liquid pressure using the height of a liquid column and is unsuitable for gases or high pressures. A U-tube manometer balances pressure against a column of known density. Bourdon-tube gauges convert elastic deformation into a pressure indication. Strain-gauge and piezoelectric transducers provide electrical signals for monitoring and control. Calibration, temperature compensation, zero error, and installation orientation affect measurement quality.

5. Viscosity and the Mechanics of Shear

Viscosity is a fluid’s resistance to relative molecular motion. Consider two parallel plates separated by a small distance y. If the lower plate is stationary and the upper plate moves with velocity U, a velocity gradient develops. For a Newtonian fluid:

τ = μ (du/dy)

where τ is shear stress in Pa, μ is dynamic viscosity in Pa·s, u is velocity parallel to the plate, and y is the coordinate normal to the plate. The relation assumes a continuum fluid, a local linear velocity gradient, and Newtonian behavior. The sign depends on the coordinate convention; the resisting stress acts opposite the relative motion.

The rate of shear strain is du/dy, measured in s⁻¹. Dynamic viscosity may also be expressed in N·s/m². Kinematic viscosity is:

ν = μ / ρ

with units m²/s. It is useful in momentum-diffusion and Reynolds-number calculations.

Worked Example 2: Shear force between plates

Oil with μ = 0.25 Pa·s fills a 2 mm gap between a stationary plate and a plate of area 0.40 m² moving at 1.5 m/s. Assuming a linear velocity profile, determine the shear stress and force.

The velocity gradient is:

du/dy ≈ U/h = 1.5/0.002 = 750 s⁻¹

Therefore:

τ = μ(U/h) = 0.25 × 750 = 187.5 Pa.

The force is:

F = τA = 187.5 × 0.40 = 75 N.

The result neglects edge effects and assumes the gap is sufficiently small for a linear profile.

Factors affecting viscosity

For most liquids, viscosity decreases as temperature increases because molecular cohesion becomes less influential. For gases, viscosity generally increases with temperature because molecular momentum transfer becomes more effective. Pressure has a comparatively small effect on ordinary liquid viscosity at moderate pressures but may be important in high-pressure lubrication and elastohydrodynamic contacts.

Viscosity data must be reported with temperature and, when relevant, pressure. Values obtained from tables or software should be checked for the correct fluid grade and operating condition.

6. Surface Tension and Capillarity

Molecules within a liquid experience attractions from neighboring molecules in all directions. Molecules at a free surface experience an unbalanced inward attraction, causing the surface to behave as though it were under tension. Surface tension σ has units N/m.

For a liquid surface, the force along a line of length L is:

F = σL

For a soap film with two surfaces, the force is approximately 2σL. Surface tension depends strongly on temperature and contamination. Surfactants reduce surface tension and change wetting behavior.

Capillarity is the rise or depression of a liquid in a narrow tube. For a circular tube:

h = 4σ cosθ / (ρgd)

where h is capillary rise (positive) or depression (negative), θ is the contact angle measured through the liquid, d is tube diameter, and ρg is specific weight. The equation assumes a circular tube, static equilibrium, negligible meniscus-complexity effects, and a clean interface. Wetting liquids have θ < 90° and rise; non-wetting liquids have θ > 90° and may be depressed.

Capillary effects are important in small passages, seals, porous materials, ink delivery, lubrication films, and microfluidic devices. They are usually negligible in large hydraulic pipes compared with pressure forces.

7. Vapor Pressure and Cavitation

Vapor pressure is the equilibrium pressure of a vapor above its liquid at a specified temperature. It rises substantially with temperature. If the local absolute pressure in a liquid falls to or below the vapor pressure, vapor-filled cavities can form. This phenomenon is called cavitation.

Cavitation may occur at pump inlets, valve restrictions, propellers, hydraulic turbines, and rapidly accelerating flow regions. As vapor bubbles enter regions of higher pressure, they collapse, producing noise, vibration, material erosion, and performance loss. The comparison must use absolute pressure, not gauge pressure.

A common pump-related indicator is the net positive suction head available:

NPSHA = (pabs,suction − pv)/(ρg) + Vs²/(2g)

where p_abs,suction is an appropriate absolute pressure at the pump suction reference, p_v is vapor pressure, V_s is mean suction velocity, ρ is liquid density, and g is gravitational acceleration. The exact expression depends on the reference location and whether suction-line losses are included. Safe operation requires NPSH available to exceed the manufacturer’s required NPSH by an appropriate margin.

8. Compressibility and Bulk Modulus

Compressibility describes the change in volume caused by pressure change. Liquids are often treated as incompressible, but no real fluid is perfectly incompressible. The bulk modulus is:

K = −V(dp/dV)

where K is bulk modulus in Pa. The negative sign reflects the fact that volume decreases as pressure increases. For small changes, assuming constant K:

∆V/V ≈ −∆p/K

The compressibility coefficient is β = 1/K and has units Pa⁻¹. A large bulk modulus means small volume change for a given pressure change.

Gas compressibility is much more important. For an ideal gas:

pV = mR T

where p is absolute pressure, V is volume, m is mass, R is the specific gas constant, and T is absolute temperature in kelvin. The ideal-gas model is appropriate when intermolecular effects are relatively small, often at moderate pressure and sufficiently high temperature. Real-gas behavior may require a compressibility factor or a real-gas equation of state.

Compressibility affects hydraulic transients, water hammer, accumulator design, pneumatic control, compressor power, and sound propagation. Treating a liquid as incompressible is appropriate only when the resulting pressure and time scales make elastic effects negligible.

9. Rheology: Newtonian and Non-Newtonian Fluids

Rheology studies deformation and flow of materials. A Newtonian fluid has constant viscosity at a specified temperature and pressure, so shear stress is proportional to shear rate. Water, air, and many light oils are approximately Newtonian over common engineering ranges.

Non-Newtonian fluids do not obey a constant-viscosity linear relation. A useful model is the power-law equation:

τ = Kp (du/dy)n

where Kₚ is the consistency index and n is the flow-behavior index. For n = 1, the model reduces to Newtonian behavior with μ = Kₚ. For n < 1, the fluid is shear-thinning; its apparent viscosity decreases as shear rate increases. For n > 1, it is shear-thickening.

The apparent viscosity is defined by:

μapp = τ / (du/dy)

For materials requiring a minimum stress before flow begins, a yield-stress model such as the Bingham model is useful:

τ = τ₀ + μp(du/dy)

when τ exceeds yield stress τ₀. Here μₚ is plastic viscosity. Paints, drilling muds, cement slurries, polymer solutions, food products, blood, greases, and suspensions may exhibit non-Newtonian behavior.

A constitutive model is an approximation. Its parameters depend on temperature, concentration, shear history, and measurement method. Engineers should not use a single viscosity value for a non-Newtonian product without specifying the shear-rate range.

10. Thermodynamic Properties Relevant to Fluids

Fluid mechanics and thermodynamics are closely connected. Thermodynamic properties describe the state and energy of a fluid, while fluid mechanics describes forces, motion, and transport.

Temperature T indicates thermal state and must be expressed on an absolute scale in gas equations. Internal energy U is the microscopic energy stored within a system. Specific internal energy is u = U/m. Enthalpy is defined as:

H = U + pV

and specific enthalpy is:

h = u + pv

where p is pressure and v is specific volume. Enthalpy is especially useful in flowing systems because the term pv represents flow work.

Entropy is a thermodynamic state property associated with energy dispersal and irreversibility. For a reversible differential process:

dS = δQrev/T

where S is entropy and δQ_rev is reversible heat transfer. Real fluid machinery generates entropy because of friction, mixing, shocks, heat transfer across finite temperature differences, and other irreversible effects.

Specific heat at constant volume and constant pressure are defined as:

cv = (∂u/∂T)v
cp = (∂h/∂T)p

For an ideal gas, h and u depend primarily on temperature, and for a calorically perfect gas cₚ and cᵥ may be treated as constant over a limited temperature range. The ratio γ_g = cₚ/cᵥ is often used in compressible-flow analysis; it should not be confused with specific weight, also commonly denoted by γ.

Other important properties include thermal conductivity k, which governs conduction; diffusivity, which measures molecular transport; and speed of sound a, which measures the propagation speed of small pressure disturbances. For a fluid, the speed of sound is related to compressibility and density by:

a² = (∂p/∂ρ)s

where the derivative is taken at constant entropy. This relation is important in compressible flow and water-hammer analysis.

11. Dimensionless Property Ratios

Dimensionless numbers compare competing physical effects. The Reynolds number is:

Re = ρVL/μ = VL/ν

where V is characteristic velocity and L is characteristic length. It compares inertial effects with viscous effects and assists in identifying laminar or turbulent regimes. The precise transition value depends on geometry and disturbance conditions; for internal pipe flow, values below approximately 2,300 are commonly considered laminar and values above approximately 4,000 turbulent, with a transitional range between them.

The Weber number compares inertia with surface tension:

We = ρV²L/σ

The Mach number compares flow speed with sound speed:

Ma = V/a

The capillary number compares viscous effects with surface tension:

Ca = μV/σ

These numbers are not substitutes for physical reasoning. Their usefulness depends on selecting a characteristic length and velocity that represent the actual problem.

12. Illustrative Case: Cavitation in a Centrifugal Pump

Background

Consider an illustrative case involving a centrifugal pump transferring warm water from an open storage tank to a processing line. Operators observe rattling noise, vibration, unstable discharge pressure, and a gradual loss of capacity.

Problem

Inspection shows that the suction strainer is partially blocked and the liquid temperature has increased. Both conditions reduce the absolute pressure available at the pump inlet or increase the vapor pressure of the water.

Analysis

The relevant comparison is between the local absolute pressure and vapor pressure. A blocked strainer increases suction-line loss, reducing suction pressure. Higher temperature increases vapor pressure. Consequently, the difference between suction pressure and vapor pressure decreases, reducing NPSH available. If NPSH available becomes too close to or below the pump’s required value, vapor bubbles form near the impeller eye and collapse downstream.

The analysis must use absolute pressure. Substituting gauge pressure directly into an NPSH expression would produce an incorrect result because vapor pressure is an absolute pressure. The engineer should determine the operating flow rate, liquid temperature, suction-pipe losses, elevation difference, and pump performance data, then calculate NPSH available under the actual conditions.

Approach and solution

The maintenance team cleans or replaces the strainer, reduces unnecessary suction-line restrictions, checks the tank liquid level, and verifies that the pump operates near its recommended range. If process conditions permit, the liquid temperature is reduced. A pressure sensor is installed near the suction flange, and vibration monitoring is used to confirm improvement.

Outcome

After the restriction is removed, suction pressure rises and the pump operates without persistent cavitation symptoms. The case demonstrates that fluid properties and system design are interdependent: temperature changes vapor pressure, geometry changes losses, and pressure conditions determine phase stability.

Learning points

  1. Cavitation assessment requires absolute pressure and correct vapor-pressure data.
  2. A pump does not create useful suction pressure independently of the complete system.
  3. Temperature, elevation, fittings, strainers, and flow rate all influence cavitation margin.
  4. Vibration and noise are useful symptoms but should be confirmed with measurements.
  5. Preventive design should include adequate NPSH margin, clean suction passages, and appropriate operating control.

13. Practical Selection and Professional Practice

Engineers should identify the fluid, temperature range, pressure range, composition, and expected shear-rate range before selecting property values. Data should come from reliable standards, manufacturer data, calibrated laboratory measurements, or recognized property databases. Units must be converted before substitution into equations.

A good engineering workflow is to define the control volume or material system, list known and unknown variables, select a property model, state assumptions, perform a dimensional check, calculate, and compare the result with physical expectations. For example, a predicted negative absolute pressure or an implausibly large liquid compression should trigger a review of assumptions and units.

Fluid properties may change because of contamination, aging, oxidation, dissolved gas, temperature cycling, or concentration changes. In machine systems, filtration, sampling, viscosity monitoring, leak prevention, and scheduled calibration are therefore part of fluid-mechanical reliability.

Computer-aided simulation and AI-assisted property estimation can improve productivity, but they do not eliminate the need for validated input data and engineering judgment. Models should be checked against conservation laws, dimensional consistency, experimental data, and operating limits. In safety-critical systems, traceable calculations and documented assumptions are essential.

Chapter Summary

Fluid mechanics treats liquids and gases as continua when macroscopic properties can be defined smoothly. Density, specific volume, specific weight, and specific gravity describe mass and gravitational effects. Pressure is normal force per unit area; absolute, gauge, and vacuum references must be distinguished. Hydrostatic pressure increases with depth in a stationary constant-density fluid.

Viscosity measures resistance to deformation. Newtonian fluids obey a linear relation between shear stress and velocity gradient, while non-Newtonian fluids require constitutive models such as power-law or yield-stress models. Surface tension and capillarity dominate small-scale free-surface effects. Vapor pressure determines the possibility of phase change and cavitation. Compressibility is represented by bulk modulus for liquids and by equations of state for gases.

Thermodynamic properties—including temperature, internal energy, enthalpy, entropy, specific heats, and speed of sound—are essential in flowing systems and fluid machinery. Dimensionless numbers such as Reynolds, Weber, Mach, and capillary numbers help compare competing physical effects. Reliable engineering practice requires appropriate property data, clear assumptions, dimensional checks, and validation against actual operating conditions.

Key Terms

Continuum assumption: Representation of matter as continuously distributed with definable properties at every point.

Density: Mass per unit volume, ρ = m/V.

Specific volume: Volume per unit mass, v = 1/ρ.

Specific weight: Weight per unit volume, γ = ρg.

Specific gravity: Ratio of a substance’s density to a reference density.

Pressure: Normal force per unit area.

Absolute pressure: Pressure measured relative to a perfect vacuum.

Gauge pressure: Pressure measured relative to local atmospheric pressure.

Viscosity: Resistance of a fluid to relative motion and deformation.

Dynamic viscosity: Proportionality constant between shear stress and shear rate for a Newtonian fluid.

Kinematic viscosity: Dynamic viscosity divided by density.

Surface tension: Tensile force per unit length at a liquid interface.

Capillarity: Liquid rise or depression caused by surface tension in a narrow passage.

Vapor pressure: Equilibrium pressure of vapor above a liquid at a specified temperature.

Cavitation: Formation and collapse of vapor cavities when local pressure approaches vapor pressure.

Compressibility: Measure of volume change caused by pressure change.

Bulk modulus: Resistance of a material to volumetric compression.

Rheology: Study of deformation and flow behavior of materials.

Newtonian fluid: Fluid with shear stress proportional to shear rate at specified conditions.

Enthalpy: Thermodynamic property defined by H = U + pV.

Review Questions

Short Answer Questions

  1. What is the continuum assumption, and when might it become invalid?
  2. Distinguish absolute pressure from gauge pressure.
  3. Define dynamic viscosity and kinematic viscosity.
  4. What is vapor pressure, and why is it important in pump operation?
  5. State the difference between a Newtonian and a non-Newtonian fluid.

Long Answer Questions

  1. Explain density, specific volume, specific weight, and specific gravity, including their units and engineering uses.
  2. Derive the hydrostatic pressure relation for a constant-density fluid and state its assumptions.
  3. Explain Newton’s law of viscosity and discuss the effects of temperature on liquid and gas viscosity.
  4. Describe surface tension, contact angle, and capillary rise, including the conditions under which capillary effects matter.
  5. Discuss compressibility, bulk modulus, ideal-gas behavior, and their importance in hydraulic and pneumatic machinery.

Analytical / Application Questions

  1. A hydraulic oil has density 860 kg/m³ and occupies 0.20 m³. Calculate its mass, specific volume, and specific weight using g = 9.81 m/s².
  2. A 1.0 mm oil film separates two surfaces. The upper surface moves at 0.8 m/s, the area is 0.15 m², and the oil viscosity is 0.12 Pa·s. Assuming a linear velocity profile, determine the shear stress and drag force.
  3. A pump handling warm water develops noise and vibration after a suction strainer becomes partially blocked. Explain, using vapor pressure and NPSH concepts, why the symptoms occur and recommend two corrective actions.

Multiple Choice Questions with Answers

Question 1

Which statement best describes the continuum assumption?

A. Fluid molecules are assumed to be motionless.

B. Fluid properties are treated as smoothly distributed at macroscopic scales.

C. All fluids are assumed to have constant density.

D. Only gases are treated as continuous matter.

Correct Answer: B. Fluid properties are treated as smoothly distributed at macroscopic scales.

Question 2

A fluid has a mass of 400 kg and a volume of 0.50 m³. Its density is:

A. 200 kg/m³

B. 400 kg/m³

C. 800 kg/m³

D. 1,250 kg/m³

Correct Answer: C. 800 kg/m³

Question 3

Which pressure reference is required when comparing local pressure with vapor pressure for cavitation analysis?

A. Gauge pressure

B. Vacuum pressure only

C. Differential pressure

D. Absolute pressure

Correct Answer: D. Absolute pressure

Question 4

For a Newtonian fluid, shear stress is proportional to:

A. Pressure only

B. Density gradient

C. Velocity gradient normal to the flow direction

D. Surface tension

Correct Answer: C. Velocity gradient normal to the flow direction

Question 5

The SI unit of kinematic viscosity is:

A. Pa·s

B. N/m

C. m²/s

D. kg/(m·s²)

Correct Answer: C. m²/s

Question 6

If the temperature of a liquid increases, its vapor pressure generally:

A. Increases

B. Decreases to zero

C. Remains exactly constant

D. Becomes equal to atmospheric pressure in every case

Correct Answer: A. Increases

Question 7

For a constant-density fluid at rest, pressure increases with depth according to:

A. p = ρg/h

B. p = p₀ + ρgh

C. p = p₀ − ρgh for depth h

D. p = μ du/dy

Correct Answer: B. p = p₀ + ρgh

Question 8

A power-law fluid with flow-behavior index n less than 1 is generally:

A. Shear-thinning

B. Shear-thickening

C. Perfectly inviscid

D. An ideal gas

Correct Answer: A. Shear-thinning

Question 9

The bulk modulus primarily measures a fluid’s resistance to:

A. Shear deformation

B. Volumetric compression

C. Surface contamination

D. Thermal conduction

Correct Answer: B. Volumetric compression

Question 10

For μ = 0.20 Pa·s and ρ = 800 kg/m³, the kinematic viscosity is:

A. 4.0 × 10⁻⁴ m²/s

B. 1.6 × 10² m²/s

C. 4.0 × 10³ m²/s

D. 160 m²/s

Correct Answer: A. 4.0 × 10⁻⁴ m²/s

Fluid Mechanics and Machinery
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