Airfoil experimental database

Version 1.1.0 (2,44 Mo) par engdancili
Get airfoil characteristics from an experimental database.
5.0
(2)
800 téléchargements
Mise à jour 29 avr. 2020
Afficher la licence sur GitHub

This app queries an aerodynamic database of NACA 4 digits, 5 digits, 6 series, and NASA supercritical airfoils. Data for the NACA sections has been derived from the book Theory of Wing Sections, by Abbott and Von Doenhoff. Data for NASA supercritical (cambered) airfoil is extracted from NASA TM 81912. The app reports airfoil characteristics, lift curve and drag polar with a few inputs. The user has only to select airfoil family and assign relative thickness and Reynolds number. The characteristics of the curves are reported in a table, which can be exported on a spreadsheet file. All data are at low Mach number, incompressible flow regime. Very useful in preliminary aircraft design, when the user needs a reliable source of data but has only few global parameters to play with.

Check the website for binaries: MATLAB app and Windows standalone executable.

The code should work with earlier versions of MATLAB, although I did not check it.

Citation pour cette source

engdancili (2024). Airfoil experimental database (https://github.com/dciliberti/experimentalAirfoilDatabase), GitHub. Extrait(e) le .

Compatibilité avec les versions de MATLAB
Créé avec R2018b
Compatible avec les versions R2018b et ultérieures
Plateformes compatibles
Windows macOS Linux

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Les versions qui utilisent la branche GitHub par défaut ne peuvent pas être téléchargées

Version Publié le Notes de version
1.1.0

Fixed Cd_min of supercritical airfoil. Updated description. New icons.
1.0.0

Pour consulter ou signaler des problèmes liés à ce module complémentaire GitHub, accédez au dépôt GitHub.
Pour consulter ou signaler des problèmes liés à ce module complémentaire GitHub, accédez au dépôt GitHub.