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Aerodynamic Impact of Slats on NACA 4415 by 2110311018 is a document available to read on EtoBox.
What is Aerodynamic Impact of Slats on NACA 4415 about?
This study uses CFD to analyze the effect of single and double slats on the aerodynamic performance of the NACA 4415 airfoil. Slat additions are found to increase lift and delay stall. A single slat provides better lift-to-drag performance than a double slat, but the double slat has a slightly higher optimum angle of attack.
- Author
- 2110311018
- Language
- EN