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Look closer, the structure is really there.

First: one transient CFD solve, rendered at 2560×1440 with 840 axial cells dedicated to the plume.

Then: hot-fire footage from Launcher, showing the same kind of shock-cell structure forming in a real rocket exhaust.

The magnified CFD views focus on the nozzle-lip expansion fan, the shock crossing on the centerline, and the second shock cell. No sharpening, generative upscaling, or invented detail—everything shown exists in the solved field.

Mach number visualization. 2D axisymmetric transient. Inviscid cold start. Frozen-gamma CEA. Preliminary design output.

Detail views are approximately 2.5× magnifications using renderer interpolation only. Cell counts shown on screen come directly from the solve log.

#CFD #RocketEngine #ShockWaves #AerospaceEngineering #RocketPropulsion
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