Model incompressible flow using practical numerical inputs. Compare boundary conditions, viscosity, and convergence trends clearly. See solved values above instantly after every calculation submission.
The form uses a responsive three-column layout on large screens, two columns on smaller screens, and one column on mobile devices.
These sample values show a practical setup for a lid-driven cavity style estimate.
| Parameter | Example Value | Meaning |
|---|---|---|
| Flow Model | Lid-Driven Cavity | Moving top wall, closed box |
| Grid Points X | 21 | Horizontal discretization count |
| Grid Points Y | 21 | Vertical discretization count |
| Time Steps | 80 | Solution advancement count |
| Pressure Iterations | 50 | Poisson correction loop count |
| Density | 1.0 | Fluid density |
| Kinematic Viscosity | 0.10 | Momentum diffusion strength |
| Time Step | 0.001 | Explicit update size |
| Lid Velocity | 1.0 | Top wall speed |
| Residual Tolerance | 0.00001 | Pressure convergence target |
For incompressible flow, the divergence of velocity is zero:
∂u/∂x + ∂v/∂y = 0
∂u/∂t + u∂u/∂x + v∂u/∂y = -(1/ρ)∂p/∂x + ν(∂²u/∂x² + ∂²u/∂y²) + Fx
∂v/∂t + u∂v/∂x + v∂v/∂y = -(1/ρ)∂p/∂y + ν(∂²v/∂x² + ∂²v/∂y²) + Fy
∇²p = b
The source term b is built from local velocity gradients to enforce incompressibility during iteration.
This calculator applies central finite differences for spatial derivatives and forward stepping in time. It is a practical numerical solver for educational and planning use, not a certified CFD package.
It solves a practical 2D incompressible flow approximation using iterative finite differences for velocity and pressure fields under selected boundary conditions.
No. It is an educational and planning-oriented solver that demonstrates Navier Stokes behavior numerically, but it is not a replacement for industrial CFD software.
More grid points capture gradients better and usually improve field detail. They also increase runtime and may require smaller time steps for stability.
It gives a quick sense of flow regime behavior by relating inertia to viscous effects. Higher values often indicate stronger convective influence.
Residual tolerance controls how tightly the pressure correction loop must settle before the solver treats the iterative pressure update as sufficiently converged.
A large time step can make explicit numerical updates unstable. Smaller steps often improve stability, especially when velocity gradients are strong.
Yes. Negative values can represent acceleration or forcing in the opposite coordinate direction, depending on your chosen physical interpretation.
The chart shows a heatmap of speed magnitude across the grid. Higher values indicate stronger local flow velocity within the computed domain.
Important Note: All the Calculators listed in this site are for educational purpose only and we do not guarentee the accuracy of results. Please do consult with other sources as well.