ANALISA AERODINAMIKA AIRFOIL NACA 0021 DENGAN ANSYS FLUENT
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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Numerical investigation was performed on NACA 0015 which is a symmetric airfoil. Pressure distribution and then lift and drag forces are verified. Changing of ground clearance was a considerable point. Also the angle of attack was changed from 0° to 10°. Pressure coefficient reaches its higher amounts on the wing lower surface when the ground clearance diminishes. Increment of the angle of atta...
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ژورنال
عنوان ژورنال: JURNAL KAJIAN TEKNIK MESIN
سال: 2016
ISSN: 2406-9671,2502-843X
DOI: 10.52447/jktm.v1i1.332