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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The NACA 0015 profile is defined by its 15% thickness. As a symmetric airfoil, it produces zero lift at a 0∘0 raised to the composed with power angle of attack. 15% of the chord length. Camber: 0% (Symmetric). 3.2 Experimental Setup The NACA 0015 exhibits a "trailing edge stall,"