Khani Solutions · Saved simulation results

Inspect the aircraft exhaust plume

Follow a hypothetical hot-gas release from startup through dispersion. Switch between gas temperature and speed, isolate a saved time, and inspect a local cell history.

Explore the saved solution

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Read the result, step by step

1 · Start with the boundary

The reconstructed aircraft center section bounds a 2D external gas domain. An assumed flush slot injects hot gas for 10 seconds; dispersion continues to 15 seconds.

2 · Follow heat and momentum

During the pulse, the jet drives gas motion and entrains surrounding air. After shutoff, buoyancy and mixing continue to redistribute heat. These are gas temperatures; the model does not solve the aircraft or ground solid temperature.

3 · Compare like with like

Keep one fixed color range while moving through saved times. Click a cell to see its local history, then compare it with the domain peak. A cooling peak can coexist with heat moving elsewhere in the domain.

Full model, mesh, solver settings and interpretation →Analysis & modeling gallery →

Data, CAD & traceability

These controls inspect retained numerical results. They do not rerun the solver when you move a control. The manifest records file sizes and SHA-256 hashes. All four studies remain preliminary and unvalidated.

Section CAD · STEP ↓Native FreeCAD ↓Run checks & limits ↓Domain histories ↓Geometry assumptions ↓Case setup source ↓Viewer data & sampling record ↓Displayed float32 fields ↓Asset manifest ↓Viewer & export source ↓

Field binary layout: little-endian float32, [saved state, stored quantity, displayed cell]. Geometry, units, fixed display ranges and times are declared in viewer.json. Battery detail color range reuses the same temperature field.