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CFD EDUCATION · NUMERICAL RESEARCH PATH

CFD learning path for research and PhD applications

A structured research-oriented pathway for learning CFD: governing equations, finite volume method, mesh quality, boundary conditions, turbulence modelling, convergence, validation and OpenFOAM workflow.

Course progress0%

Mark each module complete after studying it.

01

CFD MINDSET

CFD is not just running software

CFD means converting a physical problem into a mathematical model, then a numerical model, and finally a defensible result. Colourful contours without checks on physics, mesh, boundary conditions and validation have little research value.

01Physics
→
02Assumptions
→
03Geometry
→
04Mesh
→
05Solver
→
06Validation
Research rule

A good CFD project must explain what was simplified, why it was acceptable, and how the numerical result was verified against physics, literature or experiment.

02

GOVERNING EQUATIONS

Three core principles: mass, momentum and energy

Continuity∂ρ/∂t + ∇·(ρu) = 0

Conservation of mass in the flow domain.

Momentumρ Du/Dt = −∇p + μ∇²u + S

Newton’s second law applied to a fluid element.

Energyρcp DT/Dt = k∇²T + Φ

Thermal transport through convection, diffusion and source terms.

Incompressible

Density is treated as constant; common for low-speed liquid flows.

Compressible

Density changes become important; pressure waves and Mach number matter.

Steady

Mean solution does not change with time.

Transient

Time history is required; essential for vortex shedding and VIV.

03

DISCRETIZATION

Finite Volume Method: from continuum domain to control volumes

In the finite volume method, the domain is divided into small control volumes. The integral form of conservation laws is applied to each cell, and fluxes are balanced across cell faces.

Flux in−Flux out+Source=Accumulation
01

Conservation

FVM is strong for conservation of mass, momentum and energy.

02

Schemes

Upwind, central and higher-order schemes change numerical diffusion and stability.

03

Pressure–velocity coupling

Algorithms such as SIMPLE and PISO coordinate pressure and velocity fields.

04

MESH QUALITY

A good mesh is the foundation of a reliable result

Skewness

High skewness can destabilize the solution and reduce accuracy.

Orthogonality

Non-orthogonal cells increase discretization error and correction cost.

Aspect Ratio

Large aspect ratios may be acceptable in boundary layers but must be controlled.

y+

Near-wall resolution must match the turbulence model and wall treatment.

Mesh independence logic

CoarseMediumFineResult change becomes small

Do not claim a CFD result is reliable before checking whether the main outputs change significantly with mesh refinement.

05

BOUNDARY CONDITIONS

Boundary conditions must represent the physics

Velocity Inlet
Pressure Outlet
No-Slip Wall
Symmetry / Far-field
Body / Cylinder
Velocity inlet

Use when incoming velocity or mass flow is known.

Pressure outlet

Use when downstream static pressure is known or assumed.

No-slip wall

Velocity at solid wall equals wall velocity; thermal condition must also be defined.

Symmetry / far-field

Useful only when the domain and physics justify it.

Common mistake

Changing boundary conditions until the solution “looks good” is not CFD. Every boundary condition must have a physical justification.

06

TURBULENCE

Turbulence model selection is a research decision

RANS

Practical engineering average

Cost-effective for many industrial flows; model choice matters.

URANS

Unsteady averaged flow

Useful for periodic or transient mean-flow behaviour.

LES

Large eddy simulation

Resolves large turbulent structures; much more expensive.

DNS

Direct simulation

Solves all scales; mainly research-level and extremely expensive.

Typical model questions

  • Is the flow attached or separated?
  • Is near-wall behaviour important?
  • Is the problem steady or inherently unsteady?
  • Is the computational budget compatible with the chosen model?
07

CONVERGENCE

Convergence is not only low residuals

Residuals

Residuals should decrease and stabilize at an acceptable level.

Mass balance

Inlet and outlet mass flow must be physically consistent.

Monitor values

Forces, pressure drop, heat transfer or other key outputs should stabilize.

Physics check

Contours, vectors and integral values must make physical sense.

08

VALIDATION + REPORTING

From software output to publishable result

Verification

Did you solve the equations correctly? Check mesh, timestep, residuals and numerical settings.

Validation

Did you solve the right physical problem? Compare with experiment, benchmark or reliable literature.

Uncertainty

Report assumptions, sensitivity, mesh dependence and limitations.

Reproducibility

Document geometry, mesh, boundary conditions, solver settings and post-processing method.

OPENFOAM MINI WORKFLOW

case → constant → system → solver → postProcess

For an academic portfolio, a small validated OpenFOAM case is stronger than only listing OpenFOAM as a skill.

Back to research track

CFD knowledge check

0 / 5

1. What makes a CFD result research-grade?

2. What does FVM balance across control-volume faces?

3. What does y+ mainly relate to?

4. Which item is not enough alone to prove convergence?

5. Validation means:

How this learning page supports my research profile

This CFD education section is designed to show not only that I use CFD software, but that I understand the numerical workflow behind publishable CFD research: modelling assumptions, discretization, mesh control, convergence, validation and reproducible reporting.