xflrpy is a python enabled version of xflr5 for scripting and design optimization.

xflr5の解析結果をもとに、Cl_Alpha、Cl_Cdグラフの近似モデルを作成し、xrotorのaeroファイルを出力するプログラム

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

XFLR5 flying wing design and analysis on XFLR5

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.

Comparative CFD analysis: NACA 2412 vs NLF airfoils · ~44% L/D improvement at cruise

A simple routine calculator for aerodynamic calculations. Was originally made for aeromodellers, but also usable for simple real plane research.

Comparative analysis of NACA airfoils using XFLR5 and Excel.

Scientific analysis comparing XFLR5 simulations with wind tunnel experiments for NACA airfoils — computes lift/drag coefficients and generates publication-quality visualizations

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.

Генерация профиля крыла из пластиковой трубы для исследования в xflr⁵

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

Sub-5kg MTOW surveillance UAV · airframe + propulsion + payload integration

Airfoil design for a straight-bladed VAWT at Re=4e5. Report + XFLR5 project with validation against literature.