): Remains low at low AoA but increases exponentially as the airfoil approaches stall due to flow separation.
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) across varying angles of attack (AoA) to identify stall behavior and efficiency. 2. Introduction ): Remains low at low AoA but increases
The comparison between experimental and numerical data for the NACA 0015 shows high correlation, though CFD models often slightly under-predict drag at high angles of attack. This profile remains a robust choice for applications requiring predictable symmetric performance. The NACA 0015 exhibits a "trailing edge stall,"
The NACA 0015 exhibits a "trailing edge stall," where the flow separation begins at the rear and moves forward as the AoA increases. 5. Conclusion
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