Penerapan Teori Klasik Airfoil Tipis Ber-camber pada Profil NACA 64-206
نویسندگان
چکیده
منابع مشابه
Aerodynamic Performance Enhancement of a NACA 66-206 Airfoil Using Supersonic Channel Airfoil Design
Supersonic channel airfoil design techniques have been shown to significantly reduce drag in high-speed flows over diamond shaped airfoils by Ruffin and colleagues. The effect of applying these techniques to a NACA 66-206 airfoil is presented. The design domain entails channel heights of 8-16.6% thickness-to-chord and speeds from Mach 1.5-3.0. Numerical simulations show an increase in the lift-...
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ژورنال
عنوان ژورنال: Buletin Profesi Insinyur
سال: 2019
ISSN: 2654-5926
DOI: 10.20527/bpi.v2i1.54