Science – Future of Lithuania / Mokslas – Lietuvos Ateitis, Vol 1, No 6 (2009)

Analysis of Location of Laminar-Turbulent Transition on the FX 66-S-196 V1 Airfoil

Laurynas Naujokaitis
Eduardas Lasauskas


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 airfoil was analyzed at the Reynolds number Re = 0,5·106 and Re = 1,5·106

Article in Lithuanian

Article in: English

Article published: 2011-04-15

Keyword(s): wing section; calculation; laminar-turbulent transition; comparison with experiment

DOI: 10.3846/mla.2009.6.25

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Science – Future of Lithuania / Mokslas – Lietuvos Ateitis ISSN 2029-2341, eISSN 2029-2252
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