Outputs (47)

Numerical investigation of the effect of tread pattern on rotating wheel aerodynamics (2020)
Journal Article
Soliman, M., El-Baz, A., Abdel-Aziz, M., Abdel-Aziz, N., & Sugar-Gabor, O. (2020). Numerical investigation of the effect of tread pattern on rotating wheel aerodynamics. International journal of automotive and mechanical engineering (Kuantan), 17(4), 8234-8245. https://doi.org/10.15282/IJAME.17.4.2020.01.0621

The present work investigates the dynamic effect of wheel rotation on the aerodynamic characteristics of slick type (ST) wheel of Formula One racing cars using a computational approach. The ST wheel model was compared to experimental results as a val... Read More about Numerical investigation of the effect of tread pattern on rotating wheel aerodynamics.

Parameterised non-intrusive reduced-order model for general unsteady flow problems using artificial neural networks (2020)
Journal Article
Sugar-Gabor, O. (2021). Parameterised non-intrusive reduced-order model for general unsteady flow problems using artificial neural networks. International Journal for Numerical Methods in Fluids, 93(5), 1309-1331. https://doi.org/10.1002/fld.4930

A non-intrusive reduced-order model for nonlinear parametric flow problems is developed. It
is based on extracting a reduced-order basis from high-order snapshots via proper orthogonal
decomposition and using multi-layered feedforward artificial ne... Read More about Parameterised non-intrusive reduced-order model for general unsteady flow problems using artificial neural networks.

Design of supercritical low-Reynolds number airfoils for fixed-wing flight on Mars (2020)
Journal Article
Sugar-Gabor, O., & Koreanschi, A. (2020). Design of supercritical low-Reynolds number airfoils for fixed-wing flight on Mars. Journal of Aerospace Engineering, 33(5), https://doi.org/10.1061/%28ASCE%29AS.1943-5525.0001166

Aerodynamic shape optimization for the high-subsonic low-Reynolds number flow regime represents an area of on-going research. The interaction between supercritical compressible flow and laminar boundary layer separation is not well understood due to... Read More about Design of supercritical low-Reynolds number airfoils for fixed-wing flight on Mars.

Nonlinear lifting-line model using a vector formulation of the unsteady Kutta-Joukowski theorem (2018)
Presentation / Conference
Sugar-Gabor, O. (2018, October). Nonlinear lifting-line model using a vector formulation of the unsteady Kutta-Joukowski theorem. Presented at Aerospatial 2018 : International Conference of Aerospace Sciences, Bucharest, Romania

In this paper, a vector form of the unsteady Kutta-Joukowski theorem is derived and then used in the formulation of a general Lifting-Line Model capable of analysing a wide range of engineering problems of interest. The model is applicable to investi... Read More about Nonlinear lifting-line model using a vector formulation of the unsteady Kutta-Joukowski theorem.

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.

Unsteady nonlinear lifting line model for applied aerodynamics studies (2018)
Presentation / Conference
Sugar-Gabor, O. (2018, May). Unsteady nonlinear lifting line model for applied aerodynamics studies. Presented at Advances in Aerospace Structures, Systems and Technology (AASST 2018), London, UK

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 Unsteady nonlinear lifting line model for applied 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.

Discrete adjoint-based simultaneous analysis and design approach for conceptual aerodynamic optimization (2017)
Journal Article
Sugar-Gabor, O. (2017). Discrete adjoint-based simultaneous analysis and design approach for conceptual aerodynamic optimization. Incas Bulletin, 9(3), 133-147. https://doi.org/10.13111/2066-8201.2017.9.3.11

In this paper, a simultaneous analysis and design method is derived and applied for a non-linear constrained aerodynamic optimization problem. The method is based on the approach of defining a Lagrange functional based on the objective function and t... Read More about Discrete adjoint-based simultaneous analysis and design approach for conceptual aerodynamic optimization.

Morphing wing application on Hydra Technologies UAS-S4 (2017)
Presentation / Conference
Segui, M., Sugar-Gabor, O., Koreanschi, A., & Botez, R. (2017, February). Morphing wing application on Hydra Technologies UAS-S4. Presented at IASTED Modelling, Identification and Control 2017 Conference, Innsbruck, Austria

This paper presents the aerodynamic results of a morphing wing study performed on the UAS S4 Éhecatl from Hydra Technologies. Only the cruise phase of the aircraft was considered (constant altitude and constant speed). The difference, from an aerodyn... Read More about Morphing wing application on Hydra Technologies UAS-S4.