Worked examples
Four worked examples
Ordered by the solver and DSL surface each example requires. Figures are quoted from committed output.txt files, except where an entry states otherwise.
01 Flight envelope placard
Feed a Mach–altitude test matrix in, get a gated placard table out.
A parameter sweep over a closed-form body, gated against stated limits. No grid, no march and no solver state.
sweepGatesread_table / write_tableFittedNormalShockwell under a second02 Nozzle operating map
Sweep back-pressure over a converging–diverging nozzle and get the operating map.
Six back-pressure ratios through a 1-D compressible duct march, producing exit Mach, shock station and thrust coefficient per row, checked against the analytic critical ratios.
duct_marchsweepGatesparallel fan-outunder a second03 VIV resonance margin
Sweep airspeed over a circular member and get the shedding-frequency margin table.
Four concurrent Navier–Stokes wake marches, Strouhal extracted from a wake probe, and a resonance margin gated against a structural mode.
DEC marchsweepGatesStrouhal extractionabout two and a half minutes04 Forecast horizon under precision
How far ahead can a chaotic flow be forecast before roundoff destroys it?
One Lorenz rate field written over the scalar bound and instantiated at f32, f64 and Float106, measuring the forecast horizon each precision supports. No flow solver is involved.
Arrow calculus (Rk4)causal monadprecision as a type parametersecondsNo committed output
Source for all of these:examples/avionics_examples/cfd/