xflrpy is a python enabled version of xflr5 for scripting and design optimization.
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Updated
Oct 4, 2025 - C++
xflrpy is a python enabled version of xflr5 for scripting and design optimization.
Focused on the development of a simulator that simplifies and simulates the behaviour of an AeroSail system
Repo for some modelling and simulation work relating to my thesis
This is an application to convert exported polars from XFLR5 to Excel, automatically
Aerodynamic-structural analysis of a hybrid VTOL transition wing - NACA 0012/2415/4412 spanwise layout, XFLR5 panel method, 9-module Python performance model
Parametric modeling, aerodynamic analysis, and design evolution of classical NACA airfoil families.
Aerodynamic performance analysis of NACA 6-series airfoils using XFLR5 compared to NACA TN-2502 experimental data.
Comparative analysis of NACA airfoils using XFLR5 and Excel.
A simple routine calculator for aerodynamic calculations. Was originally made for aeromodellers, but also usable for simple real plane research.
Comparative CFD analysis: NACA 2412 vs NLF airfoils · ~44% L/D improvement at cruise
The Drafting Table // Aircraft Sizing A browser-based preliminary aircraft sizing tool for homebuilders, students, and experimental aviation enthusiasts. No installation, no account, no backend — one self-contained HTML file.
AI-driven aircraft design with flow5. MCP server + CLI for low-Reynolds-number aircraft — human-powered aircraft, RC gliders, small UAVs.
Scientific analysis comparing XFLR5 simulations with wind tunnel experiments for NACA airfoils — computes lift/drag coefficients and generates publication-quality visualizations
Генерация профиля крыла из пластиковой трубы для исследования в xflr5
Extract airfoil sections and planform data (Selig .dat + planform.csv) from STEP files, with an analytic validation harness, CLI and GUI
Airfoil design for a straight-bladed VAWT at Re=4e5. Report + XFLR5 project with validation against literature.
An aerodynamic course project which employed python to automate the process of filtering and downloading suitable airfoils.
PEL-TC is a tool which can be used in parallel with XFLR5 to creat a wing which approximates an elliptical lift distribution through twisting cross-sections
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