Examples

Original EasyCFD worked cases

The images and captions follow the organization and terminology of the original website.

01

Worked example

Laminar unsteady flow around a cylinder

Laminar flow around a cylinder at Re = 3.7 × 10³. The visualization illustrates the development of the von Kármán vortex street.

Problem definition for the cylinder-flow calculation.
Detail of the structured grid generated around the cylinder.
Instantaneous flow field showing vortex shedding downstream of the cylinder.

Tutorials and movies

Tutorial 1

Tutorial 2

Visualization movie

02

Worked example

Natural convection inside a cylindrical annulus

Laminar, steady natural convection in a concentric annulus for Pr = 0.7 and Gr = 5.0 × 10⁴. The original site notes two solutions associated with a bifurcation.

Problem definition and boundary temperatures for the concentric annulus.
Temperature contours and velocity-vector field for the second solution, showing two vortices.

Tutorials and movies

Tutorial movie

03

Worked example

Conjugate heat transfer

Laminar, unsteady conjugate heat transfer in which solid conduction and fluid convection are solved simultaneously. An air region is surrounded by copper and steel blocks.

Problem definition at the initial time: air, copper and steel regions with their dimensions and temperatures.
Temperature contours and velocity-vector field at t = 6.0 s.

Tutorials and movies

Tutorial 1

Tutorial 2

Visualization movie

04

Worked example

Turbulent flow around a vehicle

An example of external turbulent flow over a simplified vehicle shape.

Structured generalized mesh around the vehicle.
Streamlines and velocity contours for the flow over the vehicle.
05

Worked example

Pulsatile flow inside a symmetric channel with wavy walls

This example uses table functions to impose a time-dependent inlet and outlet velocity over a cycle that includes flow reversal.

Inlet Reynolds number as a function of time.
Main geometrical parameters of the symmetric channel with wavy walls.
06

Worked example

Turbulent flow around a NACA 2412 airfoil

Turbulent flow over a NACA 2412 airfoil at Re = 3.2 × 10⁶ using an unstructured mesh. The tutorials include importing profile coordinates and calculating aerodynamic forces.

Problem definition for the NACA 2412 airfoil calculation.
Unstructured mesh around the NACA 2412 airfoil.
Lift coefficient versus incidence angle: EasyCFD results and experimental data.

Tutorials and movies

Tutorial 1

Tutorial 2

Unstructured-mesh movie