Regime
Set by the shock's own feedback loop — a frequency the steady solution does not have
Every figure drawn under this hypothesis — 5 of them — with the essay each one belongs to and the generator that drew it.
5 figure placements state this regime. The strip along the foot of every figure names two things — the model that produced it and the regime it holds in — and this listing is read back out of the finished drawing rather than from what produced it.
- A shock that will not stand still — a shock at 0.6 of the chord, disturbances convected at 0.4 of the free stream · transonic · hero
- A shock that will not stand still — a shock at 0.6 of the chord, disturbances convected at 0.4 of the free stream · transonic
- A shock that will not stand still — a shock at 0.6 of the chord, disturbances convected at 0.4 of the free stream · transonic
- A shock that will not stand still — an eight per cent parabolic arc at zero lift — no boundary layer, no separation · transonic
- A shock that will not stand still — a shock at 0.6 of the chord · transonic