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O Sugar-Gabor

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My Most Viewed
My Latest

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Contact

Name:

O Sugar-Gabor

Email:

O.Sugar-Gabor@salford.ac.uk

Department:

School of Science, Engineering & Environment

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My Most Viewed

#	Item title
1.	Flutter analysis of a morphing wing technology demonstrator : numerical simulation and wind tunnel testing	251	853
2.	Numerical and experimental validation of a morphed wing geometry using Price-Païdoussis wind-tunnel testing	220
3.	Application of a morphing wing technology on Hydra Technologies unmanned aerial system UAS-S4	218
4.	Morphing wing application on Hydra Technologies UAS-S4	204	360
5.	Numerical and experimental transition results evaluation for a morphing wing and aileron system	182	171
6.	Nonlinear lifting-line model using a vector formulation of the unsteady Kutta-Joukowski theorem	172	175
7.	Numerical simulation and wind tunnel tests investigation and validation of a morphing wing-tip demonstrator aerodynamic performance	161	2
8.	Analysis of UAS-S4 Éhecatl aerodynamic performance improvement using several configurations of a morphing wing technology	160	2
9.	Unmanned aerial system hydra technologies éhecatl wing optimization using a morphing approach	160
10.	Drag optimisation of a wing equipped with a morphing upper surface	154	2

My Latest

Ali, U, Chadwick, EA ORCID: https://orcid.org/0000-0002-3743-8589 and Sugar-Gabor, O ORCID: https://orcid.org/0000-0001-6366-9623 2022, 'An optimisation of a chordwise slot to enhance lateral flow control on a UCAV' , INCAS Bulletin, 14 (4) , pp. 3-17.
Sugar-Gabor, O ORCID: https://orcid.org/0000-0001-6366-9623 2022, Active flux scheme for time-dependent, viscous, compressible flows , in: International Conference of Aerospace Sciences AEROSPATIAL 2022, 13-14 October 2022, INCAS, Bucharest, Romania.
Sugar-Gabor, O ORCID: https://orcid.org/0000-0001-6366-9623 and Fairchild, D 2022, Non-intrusive reduced-order model for unsteady fluid flow and fluid-structure interaction problems , in: International Conference of Aerospace Sciences AEROSPATIAL 2022, 13-14 October 2022, INCAS, Bucharest, Romania.
Sugar-Gabor, O ORCID: https://orcid.org/0000-0001-6366-9623 2021, Improving the efficiency of unmanned aerial systems through wing morphing: a case study for the Hydra Technologies S4 Éhecatl UAS , in: International Symposium on Electric Aircraft and Autonomous Systems, 16-18 December 2021, Eskisehir University, Eskisehir, Turkey.
Sugar-Gabor, O ORCID: https://orcid.org/0000-0001-6366-9623 2021, 'Reduced-order modelling of parameterised incompressible and compressible unsteady flow problems using deep neural networks' , International Journal of Computer Applications in Technology (IJCAT), 66 (1) , pp. 36-50.
Sugar-Gabor, O ORCID: https://orcid.org/0000-0001-6366-9623 and Koreanschi, A ORCID: https://orcid.org/0000-0002-7637-0783 2021, 'Recent developments in quasi-3D aerodynamic methods for multidisciplinary aircraft conceptual design studies' , in: Multiphysics Simulations in Automotive and Aerospace Applications , Multiphysics: Advances and Applications, 1 , Elsevier, pp. 155-186.
Sugar-Gabor, O ORCID: https://orcid.org/0000-0001-6366-9623 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) , pp. 1309-1331.
Sugar-Gabor, O ORCID: https://orcid.org/0000-0001-6366-9623 and Koreanschi, A ORCID: https://orcid.org/0000-0002-7637-0783 2021, 'Fast and accurate quasi-3D aerodynamic methods for aircraft conceptual design studies' , The Aeronautical Journal, 125 (1286) , pp. 593-617.
Soliman, MZ, El-Baz, AR, Abdel-Aziz, MA, Abdel-Aziz, N and Sugar-Gabor, O ORCID: https://orcid.org/0000-0001-6366-9623 2020, 'Numerical investigation of the effect of tread pattern on rotating wheel aerodynamics' , International Journal of Automotive and Mechanical Engineering, 17 (4) , pp. 8234-8245.
Sugar-Gabor, O ORCID: https://orcid.org/0000-0001-6366-9623 and Koreanschi, A ORCID: https://orcid.org/0000-0002-7637-0783 2020, 'Design of supercritical low-Reynolds number airfoils for fixed-wing flight on Mars' , Journal of Aerospace Engineering, 33 (5) .