Lift Force of Airfoil (NACA 0012, NACA 4612, NACA 6612) With Variation of Angle of Attack and Camber: Computational Fluid Dynamics Study
Airfoil is a cross section from air plane wings can affect aerodynamic performance to lift force (FL). The lift force generated by airfoil has different values due to several external and internal factors, including angle of attack, flow rate and camber. To find the lift force of airfoils with diffe...
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| Format: | EJournal Article |
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Physics Department, Faculty of Mathematics and Natural Sciences, University of Jember,
2021-11-24.
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A1234.567 |
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