Separasi Aliran pada Permukaan Atas Airfoil Kumbang Kelapa dengan Metoda China Clay



DOI: https://doi.org/10.25077/metal.4.2.99-105.2020

Author(s)

Benny Dwika Leonanda (Jurusan Teknik Mesin Universitas Andalas, Padang)

Abstract


This study is aimed at identifying airfoils by mimicking the curved shape of the wings of a flying animal. This interferes with what people did in ancient times to obtain objects capable of flying. The animal profile selected was the Coconut Beetle (Rhinkoporus Rhigidoporus). The wings were divided into nine pieces and made a wing model with a chord size of 15 cm, a length of 45 cm and tested in a subsonic force draft wind tunnel with a test section measuring 45 x 45 x 100 cm3. Tests are carried out to measure the length of flow separation on the upper surface of the airfoil at Reynolds and the different angles of attack of the airfoil. The China Clay method was used to determine the separation point on the airfoil surface, and the test results obtained various separation points for different angles of attack and Reynolds number.


Keywords


Airfoil; Kumbang kelapa; China clay; Separasi

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References


History of Airfoil Development, 2004, www.airfoil.com

J.D. Anderson, Fundamental of Aerodynamics, 2nd edition, Mc. Graw-Hill, 1984.

T.H. Luth, Airfoil Design and Optimization, Institute for Aerodynamics and Gas Dynamics, University of Stuttgart

P. Giguere, M.S. Selig, Blade design Trade-off Using law-lift Airfoil for stall regulated HAWTs, University of Illinois, 1999

G. De Bothezat, An Introduction to The Law of Air Resistance of Aerofoil, NACA Report No. 28.

P. K. Chang, Control of Flow Separation, Mc Graw-Hill, 1976.

G. Casale, M. Onorato, Qughotti, Flow Visualization Methods for Vertical Flow Studies, Polithecnico di Torino, Torino, Itali.

H. Mc Mahon, J. Jagoda, N.Komerath, dan J. Seitzman, Flow visualization, School of Aerospace engineering, 1999.

I. W. Newton, Flow Visualization, Aerospace and Ocean Engineering Dept, Virginia Polytechnic Institute and State University Blacksburg, Virginia, 27 Januari 2002.

M.D. Maughmer, T.S. Swan, dan S.M. Willets, The Design and Testing of a Winglet Airfoil for low-speed aircraft. The Pennsylvania State University, Pennsylvania, 2002.

Eppler Airfoil Design and Analysis Code, 4-5-2004, www.airfoil.com

Subsonik Airfoil Design, 4-5-2004, www.airfoil.com


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