HomeCFD & NumericsFVM Time-Step Estimator

📐 FVM Solver Time Step Estimator

Determine maximum allowable time step based on local convection and diffusion limits in Finite Volume grids.

⚡ Fortran 90 Engine Double Precision (IEEE 754) ✓ ISO / ASME Validated
FVM Solver Time Step Estimator Cfd
📊 Solver Telemetry ● ACTIVE
👁️ Views 31
⚡ Solves 28
💾 Downloads 423 📦 Fortran Code 4.4 KB
📅 Released Jun 2026
⏱️ Latency < 1 ms
⚡ TOOLS & REPORTS:
💾 Download Fortran 90
CFD Regimes: Transonic Airfoil Euler Mesh (Convection-Dominated) Microchannel Liquid Conduction & Advection Gas Turbine Combustor High-Diffusion Zone

📥 Cell Geometry & Diffusivity

Face Normal Velocities & Geometry

📖 FVM Stability Bounds (Versteeg §5): $$\Delta t_{\text{conv}} \le \frac{V}{\sum_f |v_{n,f} S_f|} \times \text{CFL}_{\text{safe}}$$ $$\Delta t_{\text{diff}} \le \frac{V}{2\alpha \sum_f (S_f / d_f)} \times \text{CFL}_{\text{safe}}$$ $$\Delta t = \min(\Delta t_{\text{conv}}, \Delta t_{\text{diff}})$$
3.289e-6 s
Combined Stable $\Delta t$
3.289e-6 s
Convective Limit ($\Delta t_{\text{conv}}$)
4.167e-4 s
Diffusive Limit ($\Delta t_{\text{diff}}$)
Convection Limited (CFL)
Active Bottleneck
💡 Time-Stepping Diagnostic: Convection Limited (CFL)
With a safety factor of 0.5, the maximum stable physical time-step for this cell is 3.289e-6 seconds. Total outgoing convective flux across all faces is 1.82e-1 m³/s.

📊 Individual Face Convective & Geometric Fluxes

Face # Area $S_f$ [$\text{m}^2$] Velocity $v_{n,f}$ [m/s] Distance $d_f$ [m] Flux $|v_n| S_f$ [$\text{m}^3/\text{s}$]
Face 1 2.00e-3 45.00 2.00e-3 9.00e-2
Face 2 2.00e-3 42.00 2.00e-3 8.40e-2
Face 3 6.00e-4 8.00 6.00e-4 4.80e-3
Face 4 6.00e-4 6.00 6.00e-4 3.60e-3
🔍 View Raw GNU Fortran Double-Precision Solver Output
MODE= 4
MODE_NAME=Combined (Multi-Face)
CELL_VOLUME= 1.20000000E-06
ALPHA= 1.80000000E-04
SAFETY= 5.00000000E-01
NFACES=  4
FACES_START
  1, 2.00000000E-03, 4.50000000E+01, 2.00000000E-03, 9.00000000E-02
  2, 2.00000000E-03, 4.20000000E+01, 2.00000000E-03, 8.40000000E-02
  3, 6.00000000E-04, 8.00000000E+00, 6.00000000E-04, 4.80000000E-03
  4, 6.00000000E-04, 6.00000000E+00, 6.00000000E-04, 3.60000000E-03
FACES_END
SUM_FLUX= 1.82400000E-01
SUM_DIFF_RATIO= 4.00000000E+00
DT_CONV= 3.28947368E-06
DT_DIFF= 4.16666667E-04
DT_RESULT= 3.28947368E-06
LIMITING=convective
💾 Download .f90 Code

📘 Calculation Methodology: FVM Explicit Time-Step & Courant Number (CFL)

Mathematical Model & Theory

Explicit time integration of the Navier-Stokes equations requires the CFL condition to be satisfied so that physical wave propagation is bounded within adjacent control volumes:

$$CFL = \frac{(|u| + c)\Delta t}{\Delta x} \le CFL_{max}$$
$$\Delta t_{max} = CFL_{max} \cdot \min_i \left( \frac{\Delta x_i}{|u_i| + c_i} \right)$$

Assumptions

  • Explicit Runge-Kutta / Euler time discretization.
  • Acoustic wave speed $c = \sqrt{\gamma R T}$.

Academic References

  1. Courant, R., Friedrichs, K., & Lewy, H. (1928): Mathematische Annalen.
  2. Toro, E. F.: Riemann Solvers and Numerical Methods, Springer.

Worked Engineering Example

Problem Statement:
In a nozzle cell with $\Delta x = 0.5\text{ mm}$, $u = 600\text{ m/s}$, $c = 340\text{ m/s}$, calculate stable $\Delta t$ at $CFL = 0.8$.

Step-by-step Solution:
1. $\lambda_{max} = 600 + 340 = 940\text{ m/s}$.
2. $\Delta t = 0.8 \times 0.0005 / 940 \approx 0.426\ \mu\text{s}$.
Final Result:
Maximum stable time step is $\mathbf{0.426\ \mu s}$.