Analysis of location of laminar-turbulent transition on the FX 66-S-196 V1 airfoil
The transition location on the FX 66-S-196 V1 wing section was analyzed with the using interactive program XFOIL of Mark Drela, MIT. Calculated results of transition location were compared with published measurement data from a wind tunnel at Delft University of Technology (Netherlands). The airfoi...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
Vilnius Gediminas Technical University
2011-04-01
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| Series: | Mokslas: Lietuvos Ateitis |
| Subjects: | |
| Online Access: | https://www.jbem.vgtu.lt/index.php/MLA/article/view/10642 |