1 · Hold the operating point
The public-reference, unpowered aircraft remains fixed at 20° and 100 mph. Unlike the earlier steady angle sweep, these snapshots evolve in physical time within one full-domain URANS calculation.
Khani Solutions · Saved simulation results
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.
Explore the saved solution
Loading numerical results…
Drag to pan, scroll or pinch to zoom. Reset view restores the full section. Click a cell for its saved-time profile; select a plotted metric to return to a domain history.
Time history
Click the plot to select the nearest available field snapshot. Playback advances stored states at a constant display cadence; it is not real-time motion or a new solve.
Read the result, step by step
2 · Inspect one saved state
The field panel retains the original fixed-camera view. Surface colors show signed local lift traction; translucent Q surfaces show selected rotating/strain-dominated flow structures. Instantaneous streamlines are not particle tracks.
3 · Compare with the histories
Move the time control or click a plot. Read forces from their nearest retained record and circulation from its own saved times. The short record and contour omissions do not support a validated shedding frequency or aircraft performance claim.
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.
Original high-rate loads · CSV ↓Fixed-loop circulation ↓Solver & operating inputs ↓Execution record ↓Contour limits ↓Viewer data & sampling record ↓Asset manifest ↓Viewer & export source ↓
The fixed-camera images retain their exact physical-time index; load and circulation data retain their own recorded timestamps.