EXPERIMENTAL INVESTIGATION OF INCOMPRESSIBLE FLOW AROUND THREE-ELEMENT AIRFOIL AT HIGH ANGLE OF ATTACK

Authors

  • Ashraf A. Omar Department of Mechanical Engineering Faculty of Engineering International Islamic University Malaysia
  • Tang Chun Chong Department of Aerospace Engineering Faculty of Engineering University Putra Malaysia
  • Tan Sao Min Department of Aerospace Engineering Faculty of Engineering University Putra Malaysia

Keywords:

Three element airfoil, wind tunnel, coefficient of pressure, angle of attack, Reynolds number

Abstract

The experimental investigation of the incompressible flow around a three element airfoil was
carried out to study the effect of angle of attack and Reynolds number. The work started with designing, fabricating and testing the multi-element airfoil in the UPM low speed wind tunnel. The results of the experiment were studied in terms of the coefficient of pressure. The results show delay in flow separation and continuity in pressure distr ibution for studied angles of attack and Reynolds numbers. The performance of multi-element airfoil was compared to a single element airfoil.

References

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Lim, J. C. and Dominik, C. J., "Parametric Investigation of a High-lift Airfoil at High Reynolds numbers", NASA Langley Research Center, Hampton, USA

Rumsey, C. L. and Gatski, T. B., August 2000, "Recent Turbulence Model Advances Applied to Multielement Airfoil Computations", 18th Applied Aerodynamics Meeting, NASA Langley Research Center, Hampton, USA, .

James, H. A. and Maki, R. L., July 1957, "Wind-tunnel test of the static longitudinal characteristic at low-speed of a swept-wing airplane with blowing flaps and leading edge slats", Research Memorandum, Langley Aeronautical Laboratory Library, NACA

Anderson, J. D., ''Navier-Stokes Computations & Experimental Comparisons for Multielement Airfoil Conf igurations", NASA Langley Research Center Hampton, USA .

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Klausmeyer, S. M., and Lin J. c, May 1997, "Comparative results from a CFD challenge over a 2D Three-element High-lift Airfoil", NASA Technical Memorandom 112858.

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Published

2018-05-02

How to Cite

Omar, A. A., Chun Chong, T., & Sao Min, T. (2018). EXPERIMENTAL INVESTIGATION OF INCOMPRESSIBLE FLOW AROUND THREE-ELEMENT AIRFOIL AT HIGH ANGLE OF ATTACK. Jurnal Mekanikal, 16(2). Retrieved from https://jurnalmekanikal.utm.my/index.php/jurnalmekanikal/article/view/223

Issue

Section

Mechanical

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