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A Study on the Composite Blade Performance Variation by Attaching Erosion Shield for Hovercraft

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초록

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.

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.

참고문헌 (9)

  1. Yun-hae Kim, "A study on the durability of fiberreinforced composites using ANSYS", ICMDT2009, pp.15~ (2009)
  2. Yun-hae Kim, "The evaluation of mechanical properties and physical properties of the Hanji reinforced composites", ICMDT2009, pp.25~ (2009)
  3. Yong-Wook Cho, "Principle of a Flight", pp.54~59 (1995), Chungyeon Publishing Co
  4. Jeong-Hwan Kim, "A study on three dimensional flow characteristics of wells turbine for wave power conversion by CFD", 석사, pp.2000
  5. Bum-Suk Kim, "A basis study on optimum design of turbine for wind power generation", Proceedings of the KSME 2001 Spring Annual Meeting (2001)
  6. Computational evaluation of an airfoil with a Gurney flap, "Corys Jang", NASA, 1~19, pp.TM 4071 (1992)
  7. "FLUENT User Manuals, Fluent Inc", ~
  8. Neung-Su Yoo, "Effect of airfoil thickness on the optimum Gurney flap height", Proceedings of the KSME 2001 Autumn Annual Meeting B, pp.568~572 (2001)
  9. Thompson Joe. F., "Wayne Mastin, Numerical Grid Generation" (1985), Elsevier Science Publishing Co.

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