Saved results · plume
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.
Khani Solutions · Interactive simulation library
Go inside the saved results.
Inspect a time, a material or a field. Each explorer connects numerical outputs to the model, assumptions and technical evidence.
Saved results · battery
Inspect cooling through a battery module
Explore the real finite-element temperature section alongside the full-module and coolant histories. Separate internal heat storage from heat removed by the series circuit.
Saved results · lunar
Inspect propellant through the mission windows
Choose one of 35 phases, inspect exact saved liquid fields, and compare inventory, outlet acquisition and the separately calculated ullage pressure.
Saved results · wake
Inspect the transient aircraft wake
Step through retained native-field renders at fixed 20° incidence and compare the same physical time with aerodynamic loads and fixed-loop circulation.
Independent work · Native saved fields
Icepak PCB thermal explorer
Corrected steady smartphone assembly: selectable native contour images, component maxima and vertex averages, mesh evidence, analytical cooling controls and report downloads.
Inspect the Icepak results →Existing interactive study
PCB & battery thermal learning stages
Seven connected stages: heat input, PCB/enclosure coupling, thermal pad, graphite size and adhesive thickness. Existing controls and results retained.
Start Stage 01 → · Latest comparison →Existing interactive study
Aircraft angle sweep
Eleven steady screening cases, 0°–20°, with signed surface loading and native streamlines. The angle controls remain unchanged. All eleven cases missed the full convergence targets.
Inspect the angle sweep →What can be made interactive?
A spatial field viewer needs geometry, numerical values, variable definitions and saved times. A video alone cannot supply those fields reliably.
Video archive: original numerical exports not located
The six older LinkedIn demonstrations—dynamic mesh waves, nonlinear tank waves, cryogenic slosh, compressible throttle flow, particle focusing and electronics cooling—remain in the gallery. Their original case directories or numerical exports were not located in this pass, so their videos have been retained. Each can gain a result explorer once its matching geometry, fields/time histories and run metadata are recovered.
The public rocket assembly is a separate CAD and analysis plan; the new lunar tank study has its own solved data. Unsolved battery-vent CAD has no assigned temperature or flow field.
Return to the complete gallery →