Aerodynamic Characteristics Of Membrane Airfoil Compared To Rigid Naca 4412 Airfoil by Chan, Min Xhao

“…Membrane airfoil is said to have the flexibility to change its surface geometry to adapt to the airflow. …”
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Investigation Of Cavity Designs On Various Airfoils by Vasudevan, Yuvneesh

“…Aerodynamic efficiency loss in airfoils is primarily due to the increased drag caused by boundary layer separation, especially at low Reynolds number. …”
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Airfoil With Membrane At Low Reynolds Number by Roslan, Abdul Qayyum

“…In this project, an experiment was carried out to study the aerodynamic performance on NACA 2412. The airfoil is divided into two parts which are airfoil with flexible membrane and rigid airfoil. …”
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Aerodynamics Study Of Tubercle Effect On NACA4412 Airfoil by Enso, Ennelyn Novema

“…Aerodynamics Study of Tubercle Effect on NACA4412 Airfoil The purpose of this research is to study the aerodynamics characteristics of NACA4412 airfoil with tubercle effect on its leading edge. …”
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Effect Of Vibration Frequency On Naca 4412 Airfoil Aerodynamic Performance by Chan, Ze Yu

“…As vibration might lead to catastrophe, it is very important to understand the effect of vibration frequency on an airfoil aerodynamic performance. Thus, this project was designed to obtain the aerodynamic characteristics on NACA 4412 airfoil at different vibration frequencies and to study the aerodynamic characteristics on NACA 4412 airfoil at different Reynolds numbers. …”
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Analysis And Comparison Of Airfoil-Polar Prediction Methods For Vertical-Axis Turbines by Goh, Su Teng

“…Thus, full-range airfoil data is required to compute the turbine performance of VAT. …”
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Analisis Kitaran Melalui Kerajang Airfoil NACA (Lapisan Sempadan) Dan Kawasan Pusaran by Md. Ali, Affandy

“…Eksperimen ini adalah berdasarkan kepada tajuk; “Analisis kitaran melalui kerajang airfoil NACA(lapisan sempadan) dan kawasan pusaran”. …”
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Computational Fluid Dynamics (Cfd) Simulation Of Low Renolds Number Flow Over Airfoils For Unmanned Aerial Vehicle (Uav) by Chan, Quan Xin

“…Two cambered airfoils will be chosen for aerodynamic analysis with Re number lower than 100,000. …”
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Investigation And Design Optimization Of An Indoor Plane by Alias, Faiz Azizi Che

“…The aim of this project is to improve the performance of indoor plane that been used in the outreach program by the School of Aerospace Engineering and determine the performance of a thin camber airfoil against the flat plate airfoil to be utilised for the wing of the indoor plane. …”
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Study Of Aerodynamic Performances Of Gliders Using Computational Fluid Dynamics Analysis by Mustapa, Nabila

“…One of the important design phases of an aerodynamically efficient wing is the selection of an appropriate airfoil. The airfoil v selection of a wing design firstly requires performing aerodynamic performance analyses of different airfoils for the purpose of the design (Fukusato et al., 2018). …”
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Numerical Investigation On The Aerodynamics Of Vertical Axis Hydrokinetic Turbines With Semi-Empirical Data by Foong, Xipeng

“…Next, design methodology is prepared to aid the mathematical modelling process. The airfoil data is extracted from a previous study (s1210, NACA-0015 airfoil). …”
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Experimental Investigation On The Power Performance Of A Hybrid Turbine Blade For Hydrokinetic Application by Zamri, Siti Nuruljannah Mohamad

“…The proposed Darrieus turbine, on the other hand, would use a symmetrical airfoil rather than a cambered airfoil to overcome the resistive torque and begin rotating. …”
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Evaluation Of The Mechanisms For Inducing Leading Edge Vortex Using Ansys Fluent by Idris, Mohamed Nizam Mohamed

“…This thesis evaluates the mechanism for inducing leading edge vortex using synthetic jet utilising ansys fluent on an airfoil due to aerodynamic in the transitional Reynolds number regime. …”
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Unsteady Pressure Measurement Of NACA 0018 Undergoing Pure Pitching Motion At Different Pitch Amplitudes by Tong, Chee Kent

“…An experimental investigation of the unsteady pressure measurement of a 2D NACA 0018 airfoil oscillating in pitch motion was performed by using pressure transducers at open-circuit wind tunnel. …”
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Aerodynamics And Performance Of Variable Pitch Vertical Axis Turbines At Low Tip Speed Ratios by Suresh Raj, Aaron Basil Raj

“…The blade Blade Designer module with a NACA 0018 airfoil profile and experimentally tested extrapolated airfoil polar data to ensure realistic and accurate data. …”
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Determining Helicopter Blade Length Per Airworthiness Strength Requirement by Sariman, Nur Ika Farhana

“…To achieve this, stress analyses were performed on different blade length using SOLIDWORKS 2016 x64 Edition. The NACA 8-H-12 airfoil sections with a 5.25 inches uniform chord length was chosen; suitable as rotor-blade sections for helicopters and other rotary-wing aircraft due to previous investigation. …”
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The Numerical Comparison Study On The Effect Of The Anti-Icing Methods On Thermal Stress Distribution Of Nacelle Lip-Skin by Muhamad Yusli, Siti Rosyada

“…It ruins the smoothness flow of air, increasing drag, degrading control authority and decreasing the ability of an airfoil to lift. The worst situation would be when broken ice particles are absorbed, which ingestion of would break down the engine. …”
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Aerodynamic Optimization Of Medium Altitude Long Endurance Unmanned Aerial Vehicle by Ritzwan, Muhammad Rezza

“…Kata Kunci: Kenderaan Udara Tanpa Pemandu, Dinamik Cecair Komputasi, Sayap, Hujung Sayap, Airfoil…”
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Stress And Aeroelastic Analyses Of Ultralight Aircraft Wing by Kabbarah, Hussam Fatthi A

“…NACA 2412 is chosen as the baseline airfoil for wings. The spar-caps were used in the first model, but due to the academic edition of SolidWorks 2020, the number of elements was limited for any additional components. …”
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Investigation On Dynamics, Performance And Pitch Angle Optimization Of Vertical-Axis Turbines by Lim, Yew Hao

“…To conduct the investigation, a numerical simulation model of a Darrieus type straight-bladed vertical-axis turbine with 3 blades is completed using MATLAB with incorporation of NACA 0021 airfoil data. Blade Element Theory and various assumptions that represent physical turbine operating conditions are applied to create turbine simulation that can adequately predict turbine performance. …”
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