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• W2044397931 abstract "This study intends to study about the blade performance loss occurred due to the variation in the shape of airfoil from the attachment/non-attachment of blade erosion shield for hovercraft. This study model has used NACA 4412, has designed NACA 4412 by using Auto CAD and designed the shape that has attached an erosion shield to this model according to the thickness and length. By using these models, we have generated a grid by using GAMBIT and calculated the lift coefficient (Cl) and drag coefficient (Cd) by using the FLUENT code for flow analysis. Through this, we have calculated and compared the lift-to-drag ratio that is an indicator of airfoil performance according to the shape and attachment/non-attachment of erosion shield." @default.
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• W2044397931 date "2009-11-30" @default.
• W2044397931 modified "2023-10-14" @default.
• W2044397931 title "A Study on the Composite Blade Performance Variation by Attaching Erosion Shield for Hovercraft" @default.
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• W2044397931 doi "https://doi.org/10.5916/jkosme.2009.33.7.1017" @default.
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