fluid mechanics

Overview of Fluid Mechanics

  • Fluid Mechanics is divided into two primary sub-topics:
    • Fluid Statics: Deals with fluids at rest. In this course, it has a smaller quantum (volume of content).
    • Fluid Dynamics: Deals with fluids in motion. This topic carries a higher quantum in the syllabus.
  • Significance and Syllabus:
    • In the National Book Foundation (Federal Board) textbook, this is titled "Fluid Mechanics."
    • In most other boards (except Sindh), it is titled "Fluid Dynamics," with the Statics portion typically taught in grades 9 and 10.
    • For Sindh Board, Statics and Dynamics are separate chapters.
    • Current MD-CAT and NUMS syllabi do not include this chapter, though it is part of the Aga Khan University syllabus.

Definition and Properties of Fluids

  • Definition: A fluid is a combination of liquids and gases. Technically, it is anything that flows.
  • Flow Property: If you leave a liquid or gas in one corner of a room, it will flow to the other side (e.g., perfume scent or water on a slope).
  • Key Properties Comparison:
    • Shape:
      • Fluids: Conform to the shape of their container.
      • Gases: Occupy the entire available volume of a closed container. If moved from a 3dm33\,dm^3 container to a 300dm3300\,dm^3 container, gas will expand to fill the entire 300dm3300\,dm^3. This is due to minimal intermolecular forces of attraction.
      • Liquids: Maintain a fixed volume but occupy the shape of the container at the bottom level.
      • Solids: Have fixed shapes and volumes.
    • Compressibility:
      • Gases: Highly compressible because molecules are far apart.
      • Liquids: Slightly compressible. In this chapter, we focus on Ideal Liquids, which are considered completely incompressible.
    • Density (ρ\rho):
      • Defined as mass per unit volume: ρ=mV\rho = \frac{m}{V}.
      • Gases have low density because they occupy large volumes for a small mass.
    • Viscosity:
      • Known as Fluid Friction. It is the resistance to flow.
      • Fluids slide through layers. When the top layer moves forward, the bottom layer (in contact with a surface) remains at rest due to inertia.
      • Relative motion between layers creates friction: the bottom layer pulls the top layer back, and the top layer pulls the bottom layer forward. This opposition is viscosity.
    • Surface Tension:
      • Molecules at the surface of a liquid are stretched like a membrane.
      • Gases do not have a defined surface and thus lack surface tension, whereas liquids do.

Pascal's Law

  • Statement: Pressure applied to any point of an enclosed static fluid is transmitted perfectly and equally to all portions of the fluid and the walls of the container.
  • Ideal Fluid Assumptions:
    • Zero fluid friction (non-viscous).
    • Incompressible (does not compress under pressure).
  • Pressure Calculation: P=FAP = \frac{F}{A}. If 10N/m210\,N/m^2 of pressure is applied at one piston, the same 10N/m210\,N/m^2 is transmitted everywhere.

Application: The Hydraulic Lift

  • Principle: Uses unequal cross-sectional areas to amplify force.
  • Mechanism:
    • Applying a small force (F1F_1) on a small area (A1A_1) creates a pressure P1P_1.
    • This pressure transmits as P2P_2 to a larger area (A2A_2).
    • Since P1=P2P_1 = P_2, then F1A1=F2A2\frac{F_1}{A_1} = \frac{F_2}{A_2}.
    • Because A2A_2 is much larger than A1A_1, the output force F2F_2 is much larger than F1F_1.
  • Mechanical Advantage (MAMA):
    • MA=F2F1MA = \frac{F_2}{F_1}.
    • It defines how many times the machine multiplies the input force.
  • Numerical Case Study:
    • Cylinder A (r1=5cmr_1 = 5\,cm) and Cylinder B (r2=10cmr_2 = 10\,cm).
    • Input force F1=200NF_1 = 200\,N applied to Cylinder A.
    • A1=π×(5×102)2=25×104πm2A_1 = \pi \times (5 \times 10^{-2})^2 = 25 \times 10^{-4} \pi\,m^2.
    • A2=π×(10×102)2=100×104πm2A_2 = \pi \times (10 \times 10^{-2})^2 = 100 \times 10^{-4} \pi\,m^2.
    • Result: F2=F1×A2A1=200×100π×10425π×104=200×4=800NF_2 = F_1 \times \frac{A_2}{A_1} = 200 \times \frac{100 \pi \times 10^{-4}}{25 \pi \times 10^{-4}} = 200 \times 4 = 800\,N.

Upthrust and Archimedes' Principle

  • Upthrust (Buoyant Force): An upward force exerted by a fluid on an object immersed in it.
  • Cause: When an object enters a fluid, it displaces fluid to make space. The displaced fluid molecules push back.
  • Magnitude: Equal to the weight of the liquid displaced.
    • Fup=mliquid×gF_{up} = m_{liquid} \times g
    • Since m=ρ×Vm = \rho \times V, then Fup=ρfluid×Vdisplaced×gF_{up} = \rho_{fluid} \times V_{displaced} \times g.
  • Archimedes' Principle: When an object is immersed in a liquid, it experiences an upward thrust equal to the weight of the fluid it displaces.
  • Apparent Weight: Objects feel lighter in water.
    • Apparent Weight=Actual WeightUpthrust\text{Apparent Weight} = \text{Actual Weight} - \text{Upthrust}.
  • Principles of Flotation:
    1. Weight > Max Upthrust: The object sinks (e.g., a stone). This happens when ρobject>ρfluid\rho_{object} > \rho_{fluid}.
    2. Weight = Max Upthrust: The object floats completely submerged at any level (like a fish).
    3. Weight < Max Upthrust: The object rises to the surface and floats partially submerged (like a ship). It sinks only until the weight of the displaced water equals the weight of the ship and cargo.

Surface Tension Details

  • Molecular Basis: Interior molecules are pulled in all directions (net force zero). Surface molecules have no molecules above them; they are pulled sideways and downwards, creating a "stretched membrane."
  • Mathematical Definition: Force per unit length (γ\gamma) acting on an imaginary line on the liquid surface.
    • γ=FL\gamma = \frac{F}{L}.
  • Direction: Tangential to the surface and perpendicular to the imaginary line.
  • Units and Dimensions:
    • Units: N/mN/m or dynes/cmdynes/cm.
    • Dimensions: [MLT2]/[L]=[MT2][M L T^{-2}] / [L] = [M T^{-2}] or [M1L0T2][M^1 L^0 T^{-2}].
  • Applications: Causes raindrops to be spherical (minimal surface area for a given volume) and allows small needles to float on water surfaces.

Fluid Dynamics: Drag Force and Stokes' Law

  • Drag Force (FdF_d): A retarding force experienced by an object moving through a fluid. It is a type of fluid friction.
  • Stokes' Law: For a sphere of radius rr moving slowly at speed vv through a fluid with viscosity η\eta:
    • Fd=6πηrvF_d = 6\pi \eta r v.
  • Viscosity Dimensional Analysis (η\eta):
    • From F/(6πrv)F / (6\pi r v), dimensions are: [MLT2]/([L][LT1])=[ML1T1][M L T^{-2}] / ([L][L T^{-1}]) = [M L^{-1} T^{-1}].
    • Units: kgm1s1kg\,m^{-1}\,s^{-1}.

Terminal Velocity (vtv_t)

  • Concept: When a sphere falls through a fluid, its velocity increases due to gravity, causing the drag force (FdF_d) to increase (FdvF_d \propto v).
  • Condition for Terminal Velocity: When Drag Force equals Weight (Fd=WF_d = W), the net force is zero (a=0a = 0), and the object falls with constant speed.
  • Derivation:
    • 6πηrvt=mg6\pi \eta r v_t = m g
    • m=ρ×V=ρ×(43πr3)m = \rho \times V = \rho \times (\frac{4}{3}\pi r^3)
    • 6πηrvt=(ρ×43πr3)g6\pi \eta r v_t = (\rho \times \frac{4}{3}\pi r^3) g
    • vt=2gr2ρ9ηv_t = \frac{2gr^2\rho}{9\eta}.
  • Example Problem: A water droplet (r=0.01cm=104mr = 0.01\,cm = 10^{-4}\,m) in air (η=19×106kgm1s1\eta = 19 \times 10^{-6}\,kg\,m^{-1}\,s^{-1}, ρ=1000kg/m3\rho = 1000\,kg/m^3).
    • Calculated result is approximately 1.1m/s1.1\,m/s.
  • Paratrooper Example: Opening a parachute increases the surface area, significantly increasing drag force to reach a low, safe terminal velocity (Dynamic Equilibrium).

Types of Fluid Flow

  • Streamline (Laminar) Flow: Steady flow where every particle passing a point follows the exact same path/velocity as the previous particle. Streamlines never cross.
  • Turbulent Flow: Irregular, unsteady flow with varying velocities and cross-paths.
  • Reynolds Number (ReRe): A dimensionless number used to predict flow patterns.
    • Re<2300Re < 2300: Laminar flow.
    • 2300<Re<40002300 < Re < 4000: Transition phase.
    • Re>4000Re > 4000: Turbulent flow.

Equation of Continuity

  • Basis: Law of Conservation of Mass.
  • Statement: The mass flow rate remains constant throughout a pipe.
  • Mass Flow Rate: ΔmΔt=ρAv\frac{\Delta m}{\Delta t} = \rho A v.
  • Incompressible Fluids: Since ρ\rho is constant, the volume flow rate (AvAv) must be constant.
    • A1v1=A2v2A_1 v_1 = A_2 v_2.
  • Implication: Velocity is inversely proportional to cross-sectional area. Where a pipe narrows, the fluid speeds up (e.g., putting a thumb over a garden hose or blood moving from the aorta to narrower arteries).

Bernoulli's Principle

  • Basis: Law of Conservation of Energy applied to fluids.
  • Statement: For an ideal fluid, the sum of pressure energy, gravitational potential energy, and kinetic energy per unit volume is constant.
  • Equation: P+ρgh+12ρv2=constantP + \rho g h + \frac{1}{2} \rho v^2 = \text{constant}.
  • Horizontal Pipe Case: If hh is constant, P+12ρv2=constantP + \frac{1}{2} \rho v^2 = \text{constant}. This means where velocity increases, pressure decreases.

Applications of Bernoulli's Principle

  • Torricelli's Theorem (Velocity of Efflux): Calculating speed of water leaking from a hole in a tank.
    • Applying Bernoulli at the top (1) and orifice (2):
    • P1=P2=Atmospheric PressureP_1 = P_2 = \text{Atmospheric Pressure}.
    • v10v_1 \approx 0 (Top surface area is huge compared to the hole).
    • ρgh1=ρgh2+12ρv22\rho g h_1 = \rho g h_2 + \frac{1}{2} \rho v_2^2
    • v2=2g(h1h2)v_2 = \sqrt{2g(h_1 - h_2)}.
  • Venturi Meter: Measures speed by creating a constriction. High speed in the constriction creates low pressure, and the pressure difference identifies the flow rate.

Physics of Blood Flow

  • Blood Pressure Definition: Force per unit area exerted by blood against the walls of blood vessels (arteries/aorta).
  • Heart Cycles:
    • Systole (High Side): Left ventricle contracts, pushing blood into the aorta. High pressure 120mmHg\approx 120\,mmHg.
    • Diastole (Low Side): Left ventricle relaxes and fills. Low pressure 80mmHg\approx 80\,mmHg.
  • Measurement (Sphygmomanometer):
    • An external cuff is inflated until pressure exceeds 120mmHg120\,mmHg, collapsing the artery and stopping flow (no sound in stethoscope).
    • Pressure is released; when external pressure match systolic, blood shoots through (turbulent flow), creating a "gurgling sound."
    • Pressure is released further; sounds vanish when flow becomes laminar (laminar flow occurs when external pressure drops below the diastolic level, and the artery never collapses).