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May 8, 2021 - Python
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lift-coefficient
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Combined aerospace engineering project: NACA 0012 wind-tunnel aerodynamics (lift and drag polars, stall onset) plus heavy-lift transport aircraft conceptual sizing (W/S, T/W, Cn_beta).
matlab aerodynamics aerospace-engineering aircraft-design conceptual-design fluid-mechanics drag-coefficient experimental-methods lift-coefficient thrust-to-weight aircraft-sizing stability-derivatives wind-tunnel-testing naca-0012 directional-stability stall-analysis wing-loading vertical-tail
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Jun 6, 2026 - HTML
Visualisation of general XFOIL results
plotly numerical-integration xfoil trapezoidal-rule polar-plots lift-coefficient pressure-coefficient
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Apr 20, 2024 - Jupyter Notebook
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