Calculation accuracy of wing aerodynamic parameters for a low speed aircraft
The article presents the analysis results of calculation error for a swept wing of NACA4415 airfoil. Coefficients of aerodynamic forces for this wing were calculated by means of a vortex step method including special algorithm to account non-linear characteristics of an airfoil. Calculation error o...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
Vilnius Gediminas Technical University
2012-08-01
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| Series: | Geodesy and Cartography |
| Subjects: | |
| Online Access: | https://btp.vgtu.lt/index.php/GAC/article/view/10979 |