Fluid Mechanics Formula Sheet

Fluid Mechanics Formula Sheet

All Key Equations in One Place — For Quick Revision & Exam Preparation

Last Updated: March 2026

📌 How to Use This Sheet

  • Every important fluid mechanics formula organised by topic.
  • All variables defined with SI units.
  • Use for last-minute revision — not as a substitute for understanding concepts.
  • Click topic links for detailed explanations and worked examples.

1. Fluid Properties

Density: ρ = m/V (kg/m³)

Specific weight: γ = ρg (N/m³)

Specific gravity: SG = ρ/ρwater (dimensionless)

Specific volume: v = 1/ρ (m³/kg)

Viscosity

Newton’s law: τ = μ(du/dy)

Dynamic viscosity: μ (Pa·s)

Kinematic viscosity: ν = μ/ρ (m²/s)

Surface Tension & Compressibility

Droplet pressure: ΔP = 2σ/r (sphere), ΔP = 4σ/r (bubble)

Capillary rise: h = 4σcosθ/(ρgd)

Bulk modulus: K = −ΔP/(ΔV/V) (Pa)

2. Fluid Statics

Pressure

Hydrostatic: P = P₀ + ρgh

Pressure head: h = P/(ρg)

Gauge pressure: Pgauge = Pabs − Patm

Hydrostatic Force

Force on plane surface: F = ρgh̄A

Centre of pressure: hcp = h̄ + IG/(h̄A)

Curved surface: FH = force on vertical projection; FV = weight of fluid above

Buoyancy

Buoyant force: FB = ρfluidgVdisplaced

Floating body: Fraction submerged = ρbodyfluid

Metacentric height: GM = BM − BG, where BM = I/Vdisplaced

Manometers

U-tube: Start at known pressure, add ρgh going down, subtract going up

Differential: PA − PB = (ρm − ρfluid)gh

3. Continuity & Flow Rates

General: ρ₁A₁V₁ = ρ₂A₂V₂ (mass conservation)

Incompressible: A₁V₁ = A₂V₂ = Q (volume conservation)

Volume flow rate: Q = AV (m³/s)

Mass flow rate: ṁ = ρAV = ρQ (kg/s)

Circular pipe area: A = πD²/4

4. Bernoulli’s Equation

Standard Form

P₁ + ½ρV₁² + ρgz₁ = P₂ + ½ρV₂² + ρgz₂

Head Form

P/(ρg) + V²/(2g) + z = H (total head)

Modified (with losses & pump)

P₁/(ρg) + V₁²/(2g) + z₁ + hpump = P₂/(ρg) + V₂²/(2g) + z₂ + hL

Applications

Pitot tube: V = √[2(P₀ − P)/ρ]

Torricelli: V = √(2gh)

Venturi: Q = CdA₂√[2ΔP/(ρ(1 − (A₂/A₁)²))]

Stagnation pressure: P₀ = P + ½ρV²

5. Reynolds Number & Laminar Flow

Reynolds number: Re = ρVD/μ = VD/ν

Pipe flow: Re < 2,300 → Laminar; Re > 4,000 → Turbulent

Flat plate: Rex,crit ≈ 5 × 10⁵

Hydraulic diameter: Dh = 4A/Pwetted

Hagen-Poiseuille (Laminar Pipe Flow)

Velocity profile: u(r) = (ΔP/4μL)(R² − r²)

Vmax = 2Vavg

Flow rate: Q = πΔPD⁴/(128μL)

Pressure drop: ΔP = 32μLV/D²

Friction factor: f = 64/Re

Wall shear stress: τw = 8μV/D

6. Pipe Flow — Losses

Darcy-Weisbach (Major Losses)

hf = f(L/D)(V²/2g)

ΔP = f(L/D)(ρV²/2)

Laminar: f = 64/Re. Turbulent: Moody chart or Colebrook equation.

Colebrook Equation (Turbulent)

1/√f = −2log₁₀(ε/(3.7D) + 2.51/(Re√f))

Minor Losses

hm = KV²/(2g)

Sudden expansion: h = (V₁ − V₂)²/(2g)

Equivalent length: Leq = KD/f

Series & Parallel Pipes

Series: Q same, hL,total = ΣhLi

Parallel: hL same, Qtotal = ΣQi

7. Boundary Layer

Laminar BL (Blasius — Flat Plate)

δ = 5x/√Rex

δ* = 1.72x/√Rex

θ = 0.664x/√Rex

Cf,x = 0.664/√Rex

f = 1.328/√ReL

Turbulent BL (1/7th Power Law)

δ = 0.37x/Rex0.2

Cf,x = 0.0592/Rex0.2

f = 0.074/ReL0.2

Drag

FD = CD × ½ρV²A

Flat plate drag: FD = C̄f × ½ρV² × Awetted

8. Dimensionless Numbers

NumberFormulaForce Ratio
Reynolds (Re)ρVL/μInertia / Viscous
Froude (Fr)V/√(gL)Inertia / Gravity
Mach (Ma)V/cVelocity / Sound speed
Euler (Eu)ΔP/(ρV²)Pressure / Inertia
Weber (We)ρV²L/σInertia / Surface tension
Strouhal (St)fL/VOscillation / Flow

9. Important Constants & Properties

QuantityValueUnit
ρwater (20°C)998kg/m³
ρair (20°C, 1 atm)1.204kg/m³
ρmercury13,600kg/m³
μwater (20°C)1.002 × 10⁻³Pa·s
νwater (20°C)1.004 × 10⁻⁶m²/s
μair (20°C)1.81 × 10⁻⁵Pa·s
νair (20°C)1.51 × 10⁻⁵m²/s
σwater (20°C)0.0728N/m
g9.81m/s²
Patm101.325kPa