A Comprehensive Interactive Reference

The Science of Fluid Motion

From molecular viscosity to turbulent eddies — an interactive deep‑dive into the principles, mathematics, and applications governing every substance that flows.

Explore below
Ch 01

The Continuum Hypothesis

The foundational assumption in fluid mechanics treats a fluid as a continuous medium rather than a discrete collection of molecules. At the microscopic level, all fluids consist of molecules in constant, random translational, rotational, and vibrational motion. In air at sea level, molecules travel an average distance called the mean free path between successive collisions.

The continuum viewpoint holds that every point in the fluid possesses well-defined macroscopic properties: density, velocity, and pressure. This is valid when the system's characteristic length scale $L$ is vastly larger than the mean free path $\lambda$.

Knudsen Number
$$\mathrm{Kn} = \frac{\lambda}{L}$$
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When $\mathrm{Kn} \ll 1$, the fluid behaves as a continuum and the Navier–Stokes equations apply with the no-slip boundary condition. When $\mathrm{Kn} \gg 1$, individual molecular interactions dominate and kinetic theory must be used.

Flow Regimes by Knudsen Number

Kn RangeRegimeApplicable Model
Kn < 0.001Continuum FlowNavier-Stokes with No-Slip Condition
0.001 – 0.1Slip FlowContinuum + Velocity Slip Boundary Conditions
0.1 – 10Transition FlowStatistical Mechanics / Boltzmann Equations
Kn > 10Free Molecular FlowKinetic Theory of Gases
Ch 02

Intrinsic Physical Properties

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Density
ρ = m / V

Mass per unit volume. Water ≈ 1000 kg/m³; Air ≈ 1.2 kg/m³ at STP.

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Viscosity
μ = τ / (du/dy)

Internal friction resisting deformation under shear stress.

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Surface Tension
σ ≈ 0.073 N/m (water)

Net inward force at the liquid-air interface forming a stretched membrane.

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Vapor Pressure
p_v at equilibrium

If local pressure falls below p_v, cavitation occurs — dangerous in pumps.

Newtonian Viscosity Relation

For a Newtonian fluid, the shear stress $\tau$ between fluid layers is directly proportional to the velocity gradient $du/dy$ — the rate of deformation:

Newton's Law of Viscosity
$$\tau = \mu \frac{du}{dy}$$

Non-Newtonian Behaviour Explorer

Many real fluids deviate from this simple linear relationship. Click each fluid type to learn more:

Newtonian Fluids

Viscosity $\mu$ remains constant regardless of shear rate. The stress–strain curve is a straight line through the origin. Examples: water, air, light oils, glycerin.

$\tau = \mu \dot{\gamma}$ — a perfectly linear relationship.

Pseudoplastic / Shear-Thinning

Viscosity decreases as the shear rate increases. At high shear, the fluid becomes easier to deform. Examples: blood, paint, polymer solutions, ketchup.

$\tau = K \dot{\gamma}^n$ with $n < 1$ (Power-Law model). Blood's shear-thinning allows red blood cells to align with flow in narrow arteries.

Dilatant / Shear-Thickening

Viscosity increases with shear rate. The faster you deform it, the stiffer it becomes. Examples: cornstarch in water (oobleck), quicksand, certain ceramic slurries.

$\tau = K \dot{\gamma}^n$ with $n > 1$. This counterintuitive behaviour arises from particle jamming at high deformation rates.

Bingham Plastic

Behaves as a rigid solid until a yield stress $\tau_0$ is exceeded, then flows like a viscous fluid. Examples: toothpaste, mayonnaise, mud, lava.

$\tau = \tau_0 + \mu_p \dot{\gamma}$ for $\tau > \tau_0$, and $\dot{\gamma} = 0$ otherwise. This is why toothpaste holds its shape on a brush until squeezed.

Capillary Rise

Adhesive forces between liquid and solid compete with cohesive forces within the liquid, driving fluid up narrow tubes — a phenomenon critical in plant vascular systems and soil moisture transport:

Jurin's Law — Capillary Height
$$h = \frac{2\sigma \cos\theta}{\rho g r}$$

where $\sigma$ = surface tension, $\theta$ = contact angle, $\rho$ = fluid density, $g$ = gravity, $r$ = tube radius

Ch 03

Fluid Statics & Equilibrium

When a fluid is at rest, no shear stresses act — only normal (pressure) forces. Pressure at any point is isotropic: it acts equally in all directions regardless of surface orientation.

Hydrostatic Pressure Distribution

Hydrostatic Pressure
$$p = p_0 + \rho g h$$

$p_0$ = surface pressure, $h$ = depth below surface. Pressure depends only on depth — not the container's shape.

Pascal's Law & Hydraulic Amplification

Any pressure change applied to an enclosed incompressible fluid is transmitted undiminished everywhere. Connecting two pistons of different areas creates a mechanical force multiplier:

Pascal's Principle — Hydraulic Force
$$\frac{F_1}{A_1} = \frac{F_2}{A_2} \implies F_2 = F_1 \cdot \frac{A_2}{A_1}$$

While force is amplified, work is conserved: $F_1 d_1 = F_2 d_2$. The smaller piston must travel proportionally farther.

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Hydraulic brakes, car jacks, and industrial presses all exploit Pascal's Law. A modest 50 N force on a 1 cm² piston can generate 50,000 N on a 1,000 cm² piston — enough to lift a car.

Archimedes' Principle

Buoyant Force
$$F_B = \rho_{\text{fluid}}\, g\, V_{\text{displaced}}$$

Acts upward through the centroid of the displaced volume (the centre of buoyancy).

A steel ship floats because it displaces a volume of water whose weight equals the ship's total mass. Fish exploit this by adjusting the volume of gas-filled swim bladders to achieve neutral buoyancy at any depth.

Ch 04

Governing Equations of Motion

Continuity — Conservation of Mass

Mass is neither created nor destroyed. In differential form, relating the rate of density change to the divergence of mass flux:

General Continuity Equation
$$\frac{\partial \rho}{\partial t} + \nabla \cdot (\rho \mathbf{u}) = 0$$

For incompressible flows ($\rho$ = const), this simplifies to the divergence-free constraint — every parcel of volume entering a region must leave it:

Incompressible Continuity
$$\nabla \cdot \mathbf{u} = 0 \implies A_1 V_1 = A_2 V_2$$

Navier–Stokes Equations

Newton's second law applied to a continuous viscous fluid. For an incompressible Newtonian fluid with constant viscosity $\mu$:

Incompressible Navier–Stokes (Momentum)
$$\rho\left(\underbrace{\frac{\partial \mathbf{u}}{\partial t}}_{\text{local accel.}} + \underbrace{(\mathbf{u} \cdot \nabla)\mathbf{u}}_{\text{convective accel.}}\right) = \underbrace{-\nabla p}_{\text{pressure}} + \underbrace{\mu \nabla^2 \mathbf{u}}_{\text{viscous diffusion}} + \underbrace{\rho\mathbf{g}}_{\text{body force}}$$
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The non-linear convective term $(\mathbf{u} \cdot \nabla)\mathbf{u}$ is the source of turbulence and chaos. Whether smooth closed-form solutions exist for all initial conditions is one of the Clay Millennium Prize Problems.

Bernoulli's Principle — Inviscid Streamlines

For steady, incompressible, inviscid flow along a streamline, energy is conserved in the form of pressure, kinetic, and potential contributions:

Bernoulli's Equation
$$p + \frac{1}{2}\rho v^2 + \rho g z = \text{constant along a streamline}$$

When velocity increases (e.g. flow through a constriction or over a wing), pressure must drop to conserve energy — this pressure difference generates lift in aircraft.

Interactive Bernoulli Visualiser

Bernoulli — Pipe Constriction

Real Pipe Flow — Head Loss

Real fluids lose mechanical energy to friction. The modified Bernoulli equation for engineering calculations adds a head-loss term:

Extended Bernoulli (Real Flow)
$$\frac{p_1}{\rho g} + \frac{v_1^2}{2g} + z_1 = \frac{p_2}{\rho g} + \frac{v_2^2}{2g} + z_2 + h_L$$

$h_L$ is calculated via the Darcy-Weisbach equation: $h_L = f \dfrac{L}{D} \dfrac{v^2}{2g}$

Ch 05

Turbulence & the Reynolds Number

The Reynolds number is the single most important dimensionless parameter in fluid mechanics, representing the balance between inertial and viscous forces:

Reynolds Number
$$Re = \frac{\rho V L}{\mu} = \frac{VL}{\nu}$$

$\nu = \mu/\rho$ is the kinematic viscosity. $L$ is the characteristic length (e.g. pipe diameter, chord length).

RegimeRe Range (pipe)Physical Character
LaminarRe < 2300Smooth parallel streamlines; momentum transfer only by viscosity; analytically solvable.
Transitional2300 – 4000Intermittent turbulent bursts; erratic, unstable, sensitive to perturbations.
TurbulentRe > 4000Chaotic 3D eddies; rapid mixing; inertial forces dominate; high energy dissipation.

Interactive Reynolds Number Calculator

Reynolds Number Calculator
Reynolds Number
50,000
Turbulent

Flow Pattern Visualiser

Live Streamline Simulation
Low Re — Laminar
Ch 06

Biological Fluid Mechanics

Hemodynamics — Blood Flow Physics

The cardiovascular system is a complex hydraulic network. For steady laminar flow in a cylindrical vessel, the flow rate is governed by the Hagen–Poiseuille law:

Hagen–Poiseuille Flow Rate
$$Q = \frac{\pi r^4 \Delta p}{8 \mu L}$$

The fourth-power dependence on radius is the most clinically critical insight: halving the vessel radius reduces flow by a factor of 16.

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A plaque narrowing an artery from radius $r$ to $r/2$ (50% reduction) increases vascular resistance by 16×, severely starving downstream tissue of oxygen — the mechanism behind ischaemia and heart attacks.

Interactive Vessel Narrowing Simulator

Poiseuille Flow — Vessel Stenosis
0% — Normal
Relative Flow Rate
100%
Resistance Factor
1.0×

Alveolar Stability & Pulmonary Surfactant

Breathing is a pressure-driven process governed by Boyle's Law: $pV = \text{const}$ at fixed temperature. Diaphragm contraction expands thoracic volume, dropping alveolar pressure below atmospheric, drawing air inward.

Young–Laplace Equation (Alveolar Pressure)
$$\Delta p = \frac{4\sigma}{r}$$

The excess internal pressure in a spherical bubble of radius $r$ with surface tension $\sigma$. Without surfactant, small alveoli would collapse into large ones — a catastrophic cascade.

Pulmonary surfactant reduces surface tension from ~70 dyn/cm to ~25 dyn/cm, dramatically lowering the work of breathing. Its absence in premature infants causes neonatal respiratory distress syndrome.

Ch 07

Engineering & Everyday Applications

The Drinking Straw — Atmospheric Pressure at Work

When you "suck" through a straw, you are not pulling liquid upward — you expand your oral cavity, reducing the pressure inside the straw. The higher atmospheric pressure acting on the liquid's surface in the glass pushes the fluid upward to equalise the pressure difference.

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At sea level, $p_{atm} \approx 101.3\,\text{kPa}$, which can support a water column of at most $h = p/(\rho g) \approx 10.3\,\text{m}$. No straw longer than 10.3 m can ever deliver water to your mouth — regardless of how hard you suck.

Centrifugal Pumps

The most ubiquitous fluid machine. An impeller spins fluid outward by centrifugal action. The high-velocity fluid enters a volute casing of increasing cross-section, trading velocity head for pressure head via the continuity principle and Bernoulli's equation.

Euler Turbomachinery Equation
$$H = \frac{1}{g}(u_2 V_{t2} - u_1 V_{t1})$$

$u$ = blade tip speed, $V_t$ = tangential velocity component, $H$ = specific energy head delivered to fluid

Aerodynamic Lift & Airfoil Theory

Aircraft wings generate lift by creating asymmetric flow: the curved upper surface forces air to travel faster than air under the flatter lower surface. By Bernoulli's principle, faster flow means lower pressure, and the resulting pressure difference produces lift:

Kutta–Joukowski Lift Theorem
$$L = \rho V_\infty \Gamma \cdot b$$

$\Gamma$ = circulation around the airfoil, $b$ = wingspan. Lift is directly proportional to both flight speed and circulation (related to angle of attack and camber).

Dimensional Analysis & the Art of Scaling

Buckingham's $\Pi$ theorem allows complex problems to be expressed as relationships between dimensionless groups. This is the foundation of scale-model testing — ensuring a wind-tunnel model and a full aircraft experience identical flow physics by matching key dimensionless parameters.

Reynolds Number
$Re = \rho V L / \mu$
Inertia / Viscous forces. Governs laminar-turbulent transition. Critical for pipe flow, aerodynamics, and microfluidics.
Range: 10⁻³ (capillary) → 10⁸ (aircraft)
Mach Number
$Ma = V / c$
Flow velocity / Speed of sound. Above Ma = 0.3, compressibility effects become significant; above Ma = 1, shock waves form.
Subsonic < 0.8; Transonic 0.8–1.2; Supersonic > 1.2
Froude Number
$Fr = V / \sqrt{gL}$
Inertia / Gravity forces. Essential for open-channel hydraulics, ship wave resistance, and dam spillways.
Fr < 1 = subcritical; Fr > 1 = supercritical
Weber Number
$We = \rho V^2 L / \sigma$
Inertia / Surface Tension. Controls droplet formation, spray break-up, and ink-jet printing.
Low We → spherical drops; High We → droplet breakup
Prandtl Number
$Pr = \nu / \alpha$
Momentum diffusivity / Thermal diffusivity. Links the velocity boundary layer thickness to the thermal boundary layer.
Liquid metals Pr ≪ 1; Oils Pr ≫ 1