General description
XFLR5 is an analysis tool for airfoils, wings and planes operating at low Reynolds Numbers. It includes:
- XFoil's Direct and Inverse analysis capabilities
- Wing design and analysis capabilities based on the Lifiting Line Theory, on the Vortex Lattice Method, and on a 3D Panel Method
flow5 is version 7 of xflr5. It has been released to open source on January 1st , 2026.
Documentation
General
Radio Controlled Soaring Digest 2008-02 : Francesco's great article to get started with XFLR5
Results_vs_Prediction.pdf: A comparison of performance measurements to XFLR5 results
XFLR5_Mode_Measurements.pdf: A comparison of stability measurements to XFLR5 results
Point_Out_Of_Flight_Envelope.pdf : The detailed explanation and fix for the error message "Point is out of the flight envelope"
XFLR5_and_Stability_analysis.pdf : My very personal view of stability analysis
Theoretical background
Part I: Theoretical overview
Part II: The inviscid problem_rev1.1
Part III: The viscous flow_rev1.2
Part IV: Limitations and shortcomings
French documentation
Survol_Bases_Aero_et_XFLR5.pdf : Bases aérodynamiques pour l'utilisation de XFLR5
Guide théorique pour XFLR5 : Traduction française des Guidelines
Tutoriel pour effectuer ses premiers pas dans XFLR5 : 4ème version, décembre 2013
Point_Out_Of_Flight_Envelope.pdf : Explication détaillée et méthode de résolution du problème
Chinese documentation
Ch_XFLR5_and_Stability_analysis_Rev_2.1.pdf
Japanese documentation
ja_XFLR5_and_Stability_analysis.pdf
ja_Results_vs_prediction.pdf
ja_Point_Out_Of_Flight_Envelope.pdf
Italian documentation
Lo studio dei modelli con XFLR5
Analisi della stabilità con XFLR5
Passo dopo Passo in XFLR5_6 10 03
Usare XFLR5 V6 e scoprire un sacco di cose da imparare (translated from RC Soaring Digest April 2016)
Spanish documentation
Video Tutorial
xflr5 tutorial: My first attempt at a video tutorial. This is intended for newcomers, but may also be of help to more experienced users.
Links
flow5: The next version of both xflr5 and sail7.
http://raphael.mit.edu/xfoil/: Original XFoil code as provided by M. Drela and H. Youngren, and of which the present application is derived.
http://perso.wanadoo.fr/scherrer/matthieu/aero/miarex.html : Calculation method for multi-airfoil wings based on XFoil or Experimental Results.
sail7: A derivative for the analysis of sails.
Disclaimer
- As with the original XFoil, the current software is released under the GNU General Public License , with all the associated rights and restrictions.
- The code has been developped exclusively for the design and analysis of model aircraft. Please consider using flow5 for all other applications.
- XFLR5 is released free, without any guarantee of any kind. Design of all products with the use of the code will be at the user's entire risk.
- XFLR5 is by no means a professional product, and does not offer the same guarantees of robustness, reliability, precision or product support than commercial softwares.