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Separated flow around an airfoil with a spoiler
Published 2009“…This thesis is devoted to a numerical study of the unsteady separated flow around an airfoil with a spoiler.…”
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Thesis -
84
B147 study on airfoil performance in gusts
Published 2014“…The dimensions of the existing airfoils were also changed to reduce the torque required to rotate the airfoils in attempt to produce sinusoidal wind gusts in the wind tunnel. …”
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Final Year Project (FYP) -
85
Effects of plasma actuator on flow over an airfoil
Published 2015“…Two features of flow control are investigated: delaying flow separation and controlling of lift generated. A NACA 0015 airfoil with plasma actuator installed at the surface was tested in an opened-loop wind tunnel at Re=106k and 212k and the aerodynamic forces were measured using a six-axis force/torque sensor. …”
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Final Year Project (FYP) -
86
On the flow behaviour of 2D flexible airfoils
Published 2018“…This thesis studies the on flow behaviour of the corrugated airfoil proposed by B. G Newman et al. [1]. Unlike previous studies by Flint et al. [2], this study put the flexibility and deformation of the airfoil into consideration. …”
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Final Year Project (FYP) -
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Aerodynamic performance of biomimicry snake-shaped airfoil
Published 2019“…In this study, the focus is placed on the snake-cross-section airfoil known as the S-airfoil. It is found that there is a lack of available researches on S-airfoil despite its important characteristics. …”
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Article -
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The effects of vortex shedding on the aerodynamic performance of airfoils
Published 2018“…This is a comparative study involving various National Advisory Committee for Aeronautics (NACA) airfoils NACA 0012, NACA 0024, NACA 4412 and NACA 4424. …”
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Article -
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Numerical simulation of turbulent flow around an airfoil with blunt trailing edge aerodynamic characteristics modification of this airfoil with base and aerodynamic cavity
Published 2013-03-01“…This paper is a computational study of the behavior of aerodynamics characteristics of an airfoil with blunt trailing edge and studies the effects aerodynamic performance caused by modifications made to the trailing edge. …”
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Numerical Study of Optimum Configuration of Unconventional Airfoil with Steps and Rotating Cylinder for Best Aerodynamics Performance
Published 2023-07-01Subjects: “…unconventional airfoil, airfoil with rotating cylinder, airfoil with upper steps.…”
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Analisis Airfoil Double-Slot Flap LS(01)-0417 MOD Dengan Airfoil Tanpa Flap Nasa SC(2) 0610
Published 2018-10-01“…Kestabilan pesawat terbang ditentukan oleh desain airfoil sayap dan ekor. Perbedaan kecepatan aliran udara antara permukaan atas dan bawah airfoil menghasilkan perbedaan tekanan sehingga akan memberikan gaya angkat (lift) pada sayap. …”
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Improvement of airfoil trailing edge bluntness noise model
Published 2016-02-01“…In this article, airfoil trailing edge bluntness noise is investigated using both computational aero-acoustic and semi-empirical approach. …”
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Article