Aerodynamic-structural analysis of a hybrid VTOL transition wing - NACA 0012/2415/4412 spanwise layout, XFLR5 panel method, 9-module Python performance model
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May 2, 2026 - Python
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naca-airfoil
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Automated workflow for NACA 4-digit airfoil analysis and 3D CAD geometry (SolidWorks/CATIA) generation using Python and Bash.
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Mar 26, 2026 - Python
2D turbine blade thermal & stress simulator using finite difference methods.
python aerospace mechanical-engineering finite-difference heat-transfer aerospace-engineering streamlit aerospace-structures naca-airfoil
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May 29, 2026 - Python
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