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

Abstract


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

Full Text: PDF pdf

Science – Future of Lithuania / Mokslas – Lietuvos Ateitis ISSN 2029-2341, eISSN 2029-2252
This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 License.