Computational Study of Aerodynamic Flow over NACA 4412 Airfoil
نویسندگان
چکیده
منابع مشابه
Flying-Hot-Wire Study of Flow Past an NACA 4412 Airfoil at Maximum Lift
Hot-wire measurements have been made in the boundary layer, the separated region, and the near wake for flow past an NACA 4412 airfoil at mad mum lift. The Reynolds number based on chord was about 1,500,000. Special care was taken to achieve a two-dimensional mean flow. The main instrumentation was a flying hot wire; that is, a hot-wire probe mounted on the end of a rotating arm. The probe velo...
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ژورنال
عنوان ژورنال: British Journal of Applied Science & Technology
سال: 2017
ISSN: 2231-0843
DOI: 10.9734/bjast/2017/31893