Potential Flow Theory

Module 2

2.1 Flow Kinematics
2.2 Stream Function
2.3 Elemental Flow
2.4 Numerical Exercise
2.1 Flow Kinematics
Basic Fluid Properties
Density (ρ)

Mass per unit volume: ρ = m / V. Units: kg·m⁻³. Water (25°C) ≈ 1000 kg/m³, Air (25°C) ≈ 1.184 kg/m³.

Specific weight & specific gravity

Specific weight γ = ρ g (N/m³).
Specific gravity SG = ρ_fluid / ρ_water (dimensionless).

Viscosity (μ, ν)

Viscosity is internal resistance to shear. Dynamic μ relates shear stress to velocity gradient: τ = μ du/dy. Kinematic ν = μ/ρ. Liquids: μ ↓ with T; gases: μ ↑ with T.

Compressibility & Bulk Modulus

Bulk modulus K = −V dP/dV. Liquids have high K (low compressibility), gases low K. Speed of sound: a = √(K/ρ).

Vapor pressure & cavitation

Vapor pressure is the pressure at which liquid vaporizes. High vapor pressure → easier evaporation; important for cavitation in pumps and propellers.

Surface tension & capillarity

Surface tension σ causes liquids to minimize surface area; capillary rise formula:

h = (2 σ cos θ) / (ρ g r)

θ = contact angle, r = tube radius.

2.2 Stream Function
Fluid Flow
Newtonian Law of Viscosity
The Newtonian law of viscosity states that the shear stress between adjacent fluid layers is directly proportional to the velocity gradient (rate of shear strain). Formula: τ = μ (du/dy)
Non-Newtonian Fluids
  • Shear-Thinning: Paint, blood, ketchup
  • τ = k (du/dy)n, n < 1
  • Shear-Thickening: Cornflour mixture (oobleck)
  • τ = k (du/dy)n, n > 1
  • Bingham Plastic: Toothpaste
  • τ = τ₀ + μₚ (du/dy)
  • Thixotropic: Gels, yogurt
  • μ = μ(t)
  • Rheopectic: Gypsum paste
Newtonian vs Non-Newtonian Fluids
CategoryNewtonian FluidsNon-Newtonian Fluids
Nature / BehaviorViscosity remains constant, independent of shear rate.Viscosity changes with shear rate or time.
Mathematical Modelτ = μ (du/dy)τ = k (du/dy)n or τ = τ₀ + μₚ (du/dy)
Shear Stress vs Shear RateLinear relationshipNon-linear relationship
Viscosity DependenceDepends only on temperatureDepends on shear rate, time, and molecular structure
Flow CurveStraight lineCurved / non-linear
ExamplesWater, air, kerosene, alcohol, mercuryHoney, ketchup, blood, toothpaste, paints, oobleck
Types— (No types; simple behavior)Pseudoplastic, Dilatant, Bingham Plastic, Thixotropic, Rheopectic
ApplicationsAerodynamics, lubrication, pipelines, hydraulic systemsFood processing, cosmetics, drilling mud, biomedical fluids, paints
Industries UsedAviation, aerospace, chemical plants, HVACFMCG, oil & gas, biomedical, pharmaceuticals, construction
Behavior Under ForcePredictable, easy to modelComplex, may require rheometers for analysis
Temperature SensitivityModerateHigh (strong dependence on structure)
Fluid Flow
1. Steady & Unsteady Flow
Steady flow properties do not change with time.

Steady: ∂(property)/∂t = 0

Example (Steady): Water flowing through a constant pipe

Unsteady flow properties vary with time. ∂(property)/∂t ≠ 0
Example (Unsteady): Pump start-up flow

2. Uniform & Non-uniform Flow

Uniform: Velocity same at every point.

∂u/∂x = 0
Example: Long straight pipe flow

Non-uniform: Velocity varies along path.

∂u/∂x ≠ 0
Example: Flow through a nozzle

3. Laminar & Turbulent Flow
Re = (ρUD)/μ
Laminar: Smooth, orderly motion of fluid layers.E.g., Honey or oil flow (Re < 2000)
Turbulent:Chaotic, mixing flow. E.g., Water from a fast-open tap (Re > 4000)
4. Compressible & Incompressible Flow
Compressible: Density changes significantly, dρ/dt = 0
or, ∇·V = 0
Example: High-speed air flow.
Incompressible: Constant density, dρ/dt ≠ 0
Example: Water at low speeds.
5. Rotational & Irrotational Flow
ω = ∇ × V ≠ 0
Rotational: Vortex near drain
∇ × V = 0
Irrotational: Potential flow over airfoils
6. 1D, 2D & 3D Flow
V = V(x) 1D: Simple pipe flow
V = V(x, y) 2D: Flow over a flat plate
V = V(x, y, z) 3D: Turbulent flow in real world

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2.3 Elemental Flow
Cylinder Pressure Visualization

Circular Cylinder Pressure Visualization

Explore the symmetrical pressure distribution on a circular cylinder. The pressure pattern remains constant regardless of orientation in ideal flow.

Key Concepts

  • High Pressure: Stagnation points
  • Low Pressure: Maximum velocity zones
  • Symmetry: Zero lift generation
  • Ideal Flow: Inviscid assumption

Theory

Pressure is visualized using the theoretical pressure coefficient: Cp = 1 − 4 sin²θ. Blue indicates low pressure, red indicates high pressure.

2.4 Numerical Exercise

Numerical Problems


Developed by Dr. Aishwarya Dhara

Aerodynamics Notes by Dr Aishwarya Dhara
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