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boundary-layer-transition

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aero-shockwave-boundarylayer-sam

samuelakosaonyejekwe / aero-shockwave-boundarylayer-sam

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Mach-4 supersonic-intake shock-wave / boundary-layer transition case study computed with the UniSTAR-CFD solver, validated against three real experimental benchmarks.

python validation scientific-computing cfd computational-fluid-dynamics supersonic aerospace-engineering hypersonic rans shock-waves aerothermodynamics turbulence-modeling shock-wave-boundary-layer-interaction swbli boundary-layer-transition supersonic-intake
  • Updated Jun 30, 2026
  • Python
aero-turbulence-transition-sam

samuelakosaonyejekwe / aero-turbulence-transition-sam

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Industrial aerodynamics case study predicting laminar-to-turbulent boundary-layer transition over a 3-D natural-laminar-flow aircraft wing (AETHER-NLF 25), using the UTSS multi-mechanism transition solver — includes geometry, mesh, solver outputs, figures, experimental validation, and the full report.

python validation cfd aircraft turbulence fluid-dynamics computational-fluid-dynamics case-study aerodynamics aerospace-engineering boundary-layer panel-method wing-design drag-reduction natural-laminar-flow boundary-layer-transition laminar-turbulent-transition skin-friction-drag transition-modeling
  • Updated Jun 30, 2026

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