Airfoil Geometry Converter
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F70883521%3A28140%2F16%3A43874366" target="_blank" >RIV/70883521:28140/16:43874366 - isvavai.cz</a>
Result on the web
<a href="https://github.com/vogeltanz/AirfoilGeometryConverter/releases/download/v0.5.0/Airfoil.Geometry.Converter.zip" target="_blank" >https://github.com/vogeltanz/AirfoilGeometryConverter/releases/download/v0.5.0/Airfoil.Geometry.Converter.zip</a>
DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
Airfoil Geometry Converter
Original language description
The application accelerates the preparation for aerodynamic analysis and optimization of airfoil in CFD software and simplifies deployment of optimized airfoil into a real aircraft design. Airfoil Geometry Converter is a console application, which converts files with coordinates from/to formats commonly used for airfoils (such as Selig, Lednicer, and NASA/OpenVSP). The application can be used as a mesh file generator of airfoils for aerodynamic analysis in CFD software; e.g., in SU2, OpenFOAM, etc. The files may be also converted back from the mesh file to the geometry file, for example, when an optimization of an airfoil was performed and it is necessary to apply the airfoil on a wing in the real design of an aircraft. Then, the optimized airfoil can be used in CAD and parametric software, specialized on the aircraft engineering; e.g. in OpenVSP. Input formats with airfoil geometry: Selig (dat), Lednicer (dat), NASA/OpenVSP (af). Output formats for mesh: su2, msh, msh1, unv, vrml, ply2, stl, mesh, bdf, diff, med, ... (see Gmsh). Input formats with mesh: su2, msh (ASCII v2). Output formats for airfoil geometry: Selig (dat), Lednicer (dat), geo.
Czech name
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Czech description
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Classification
Type
R - Software
CEP classification
IN - Informatics
OECD FORD branch
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Result continuities
Project
<a href="/en/project/LO1303" target="_blank" >LO1303: Promoting sustainability and development of the Centre for Security, Information and Advanced Technologies (CEBIA-Tech)</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)<br>S - Specificky vyzkum na vysokych skolach
Others
Publication year
2016
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Internal product ID
R/FAI/ÚIUI/2016/AirfoilConverter
Technical parameters
Konzolová aplikace naprogramovaná v C++ pro operační systém Windows (verze pro Linux je také možná). Využívá aplikaci Gmsh verze }=2.11.0 pro meshování geometrie.
Economical parameters
Aplikace přispívá ke snížení finančních nákladů na vývoj a nasazení nových vylepšených profilů křídel, které mohou pozitivně ovlivnit aerodynamiku a spotřebu paliva letounu využívající tyto profily.
Owner IČO
70883521
Owner name
Univerzita Tomáše Bati ve Zlíně