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A general numerical unsteady nonlinear lifting line model for engineering aerodynamics studies (2018)
Journal Article
Sugar-Gabor, O. (2018). A general numerical unsteady nonlinear lifting line model for engineering aerodynamics studies. Aeronautical Journal, 122(1254), 1199-1228. https://doi.org/10.1017/aer.2018.57

The lifting line theory is widely used for obtaining aerodynamic performance results in various engineering fields, from aircraft conceptual design to wind power generation. Many different models were proposed, each tailored for a specific purpose, t... Read More about A general numerical unsteady nonlinear lifting line model for engineering aerodynamics studies.

Numerical and experimental transition results evaluation for a morphing wing and aileron system (2018)
Journal Article
Botez, R., Koreanschi, A., Sugar-Gabor, O., Mebarki, Y., Mamou, M., Tondji, Y., …Concilio, A. (2018). Numerical and experimental transition results evaluation for a morphing wing and aileron system. Aeronautical Journal, 122(1251), 747-784. https://doi.org/10.1017/aer.2018.15

A new wing-tip concept with morphing upper surface and interchangeable conventional and morphing ailerons was designed, manufactured, bench and wind tunnel tested. The development of this wing tip model was performed in the frame of an international... Read More about Numerical and experimental transition results evaluation for a morphing wing and aileron system.

Numerical study of the circular cylinder in supersonic ground effect conditions (2018)
Journal Article
Sugar-Gabor, O. (2018). Numerical study of the circular cylinder in supersonic ground effect conditions. International review of aerospace engineering (CD-ROM), 11(1), https://doi.org/10.15866/irease.v11i1.13696

A numerical study of the aerodynamics of a circular cylinder section in proximity to the ground surface was performed, for Mach numbers of 1.5 and 2.9 and ground clearances between 2 and 0.125, non-dimensional with respect to the cylinder diameter. T... Read More about Numerical study of the circular cylinder in supersonic ground effect conditions.