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aero-dynamic-stall-sam
aero-dynamic-stall-sam PublicDynamic-stall prediction on a helicopter retreating blade (NACA 0012) using UNISTALL — a reduced-order Unified Indicial–Beddoes State-Space (UIBS) solver — validated against NASA static and dynamic…
Python
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aero-shockwave-boundarylayer-sam
aero-shockwave-boundarylayer-sam PublicMach-4 supersonic-intake shock-wave / boundary-layer transition case study computed with the UniSTAR-CFD solver, validated against three real experimental benchmarks.
Python
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