An analysis on Aerodynamics Performance Simulation of NACA 23018 Airfoil Wings on Cant Angles
Winglet attached on the tip of aircraft wings to increase lift. Mainly, winglet used for increasing aerodynamic efficiency, it decreases induced drag caused by vortex on wings tip. The phenomenon of vortex is collision of high-pressured air below the wings meet the low-pressured air above it that ca...
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| Format: | Article |
| Language: | English |
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University of Muhammadiyah Malang
2017-05-01
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| Series: | JEMMME (Journal of Energy, Mechanical, Material, and Manufacturing Engineering) |
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| Online Access: | http://ejournal.umm.ac.id/index.php/JEMMME/article/view/4905/5013 |