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- The Zenithair CH-750 airfoil has the highest maximum lift coefficient (approximately 1.70) as well as the largest lift coefficient at an angle of attack of zero degrees (0.40)1. Airfoil S1223 has the highest maximum lift coefficient among all the airfoils2. To achieve maximum airfoil lift, the best recovery location is chosen and the airfoil is made very thin so that the lower surface produces maximum lift as well3.Learn more:✕This summary was generated using AI based on multiple online sources. To view the original source information, use the "Learn more" links.
Each airfoil produces a differing lift coefficient for a given angle of attack. The Zenithair CH-750 airfoil has both the highest maximum lift coefficient (approximately 1.70) as well as the largest lift coefficient at an angle of attack of zero degrees (0.40).
aerotoolbox.com/intro-airfoil-aerodynamics/Selig and Guglielmo followed the footprints of Eppler and designed airfoil S1223 (Fig. 1), which has the highest maximum lift coefficient among all the airfoils that are presented here.www.witpress.com/Secure/elibrary/papers/AFM18/…The thickest section at Re = 10 millionis 57% thick, but of course, it will separate suddenly with any angle of attack. For maximum airfoil lift, the best recovery location is chosen and the airfoil is made verythin so that the lower surface produces maximum lift as well.aero-comlab.stanford.edu/aa200b/lect_notes/Airfoil… - People also ask
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