Fortran program utilizing panel method on arbitrary lifting airfoil in two-dimensional incompressible flow to obtain Cl, Cd & Cm / Abdul Rahman Abdullah by Abdullah, Abdul Rahman

“…NACA 0009 Symmetrical Airfoil and NACA 23018 Cambered Airfoil configuration is used as a comparable results with the one obtained from Abbot and Von Doenhoff Airfoil Data. …”
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Flight performance analysis of a radio controlled airplane / Luthffi Idzhar Ismail by Ismail, Luthffi Idzhar

“…Computational Fluid Dynamics simulation is performed to obtain the important parameters such as lift coefficient, drag coefficient and moment coefficient for the airfoil as well as for the whole wing itself. This research focus on the analysis of the range performance, endurance performance, as well as the maximum velocity performance. …”
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CAD modelling using Gielis Superformula / Azimah Abdul Aziz by Abdul Aziz, Azimah

“…In this study, an impeller, airfoil and propeller blade were generated using Gielis Superformula with the aid from Solidworks features. …”
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Aerodynamics performance of optimal wing profile on MAV wings / Siti Khatijah Hamdan by Hamdan, Siti Khatijah

“…The optimum design for Micro Air Vehicle (MAV) fixed wing is Zimmerman based on the optimal efficiency, however, the effect of camber to aerodynamics performance on the Zimmerman design are not fully discovered by previous researchers due to wide range of airfoil profile. Thus, the objectives of this research are to compare the aerodynamics performance of Zimmerman wing design with different percentage of camber.Three types of Zimmerman wing design known as Profile 1, Profile 2 and Profile 3 with 3%, 6% and 12% of camber, respectively which has different polynomial equation are used for ANSYS-CFX simulations. …”
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