ARTES

ARTES is a browser-based computational fluid dynamics workspace. This presentation shows engineering model preparation and the visualization of simulation results.

ARTES product walkthrwough showing model preparation and flow-result views.

[00]

Leverage Our Expertise for Your Strategic Growth

Move from design through simulation and analysis to optimized results in one connected CFD workflow.

NSMB Solver

Connect your ARTES workflow with CFSE's NSMB flow solver, from case setup to simulation results.

Seamless Browser-Based Integration

Prepare, run, and review CFD work in one browser-based workspace, with a smooth handoff between steps.

  1. Design
  2. Mesh
  3. Simulate
  4. Analyze
  5. Optimize
ARTES

Made for Aerospace Applications

Build and study demanding aerospace cases, from vehicle geometry and meshes to re-entry flow fields.

Integrated Post-Processing

Explore physical fields and simulation results directly in ARTES, without leaving your workflow.

[01]

Define your geometry

Shape your model and organize its parts into a simulation-ready setup.

[02]

Mesh

Inspect the CARINA computational grid and its three-dimensional block structure.

ARV-2 to CARINA capsule family viewport

Scrolling rotates the ARV-2 capsule into profile view, then changes its shape to CARINA.

[03]

Simulate

Set up the case and run a high-fidelity flow simulation.

[01]

Easy Setup

Define free stream conditions from a planetary atmosphere, or enter the values yourself.

Physical Input Parameters
Thermodynamic State
Planetatkm
Free stream density.
Free stream pressure.
Free stream temperature.
Gas constant (287.0 for air, set to 1 if variables are non-dimensionalized).
Reynolds number per meter. Depending on the viscosity model, may be ignored since it is computed from free stream conditions.

[02]

Run simulations on a sustainable cloud

Swiss-hosted infrastructure supports digital sovereignty and keeps simulation data under your control.

Infomaniak

[04]

Post-Processing

Access physical fields during re-entry. Examine the bow shock, stagnation line, and high-temperature regions around the vehicle.

Temperature contour around an ARV-1 capsule, with a color scale beside it.

Bow-shock

Trace the shock front.

Inspect the Mach field ahead of the vehicle.

Bow-shock diagram ahead of a re-entry capsule, labelled Original Grid and Adapted Grid, with incoming flow arrows.

Stagnation-line

Follow the centerline flow.

Study heat flux near the vehicle nose as the incoming flow slows.

Heat-flux contour on an ARV-1 capsule, with a color scale beside it.