| Hybrid upwind methods for the simulation of unsteady shock-wave diffraction over a cylinder J Zółtak, D Drikakis Computer Methods in Applied Mechanics and Engineering 162 (1-4), 165-185, 1998 | 104 | 1998 |
| Multi-disciplinary optimisation approach for a light turboprop aircraft-engine integration and improvement A Iwaniuk, W Wiśniowski, J Żółtak Aircraft Engineering and Aerospace Technology: An International Journal 88 …, 2016 | 42 | 2016 |
| Optimisation of the helicopter fuselage with simulation of main and tail rotor influence W Stalewski, J Żółtak Proceedings of the 28th ICAS Congress of the International Council of the …, 2012 | 35 | 2012 |
| The Preliminary Design of the Air-Intake System and the Nacelle in the Small Aircraft-Engine Integration Process W Stalewski, J Żółtak Aircraft Engineering and Aerospace Technology 86 (3), 250 - 258, 2014 | 29 | 2014 |
| Multi-objective and multidisciplinary optimization of wing for small aircraft W Stalewski, J Żóltak Proceedings of the CEAS 2011 3rd CEAS Air & Space Conference, 21st AIDAA …, 2011 | 21 | 2011 |
| Investigation of blending-function-based overlapping-grid technique for compressible flows D Drikakis, J Majewski, J Rokicki, J Żółtak Computer Methods in Applied Mechanics and Engineering 190 (39), 5173-5195, 2001 | 15 | 2001 |
| Multi-Disciplinary Optimisation Of Forward-Swept Wing J Rokicki, W Stalewski, J Żółtak, T Burczynski, J Périaux Evolutionary Methods for Design, Optimization and Control, 2009 | 12 | 2009 |
| Przykłady zastosowania pakietu Fluent w analizach bezpieczeństwa lotu śmigłowców A Dziubiński, W Stalewski, J Żółtak Prace Instytutu Lotnictwa 194, 2008 | 11 | 2008 |
| Parallel performance of overlapping mesh technique for compressible flows J Rokicki, J Żółtak, D Drikakis, J Majewski Future Generation Computer Systems 18 (1), 3-15, 2001 | 11 | 2001 |
| Design of a turbulent wing for small aircraft using multidisciplinary optimisation W Stalewski, J Żółtak Archives of Mechanics 66 (3), 185 - 201, 2014 | 10 | 2014 |
| Multicriteria design and optimisation of helicopter fuselage W Stalewski, J Żółtak, C Poloni, D Quagliarella, J Périaux, N Gauger, ... Evolutionary and Deterministic Methods for Design, Optimization and Control, 2011 | 9 | 2011 |
| CFD Analysis of External Armour Influence on a Helicopter Aerodynamic Characteristics A Dziubiński, K Grzegorczyk, J Żółtak Prace Instytutu Lotnictwa 218, 20-27, 2011 | 7 | 2011 |
| Multi-objective surrogate model-based optimization of a small aircraft engine air-intake duct PS Drężek, S Kubacki, J Żółtak Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2022 | 5 | 2022 |
| Time-accurate Simulation of Flow Past PZL W-3A "Sokół" (FALCON) Helicopter Main Rotor in Forward Flght O Szulc, P Doerffer, J Żółtak, J Małecki Task Quarterly 17 (1), 43-61, 2013 | 5 | 2013 |
| Multi-objective and multi-disciplinary design using evolutionary methods applied to aerospace design problems J Żółtak Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2018 | 3 | 2018 |
| NUMERICAL ANALYSIS OF HIGH-SPEED IMPULSIVE (HSI) NOISE OF PZL W3-A “SOKÓŁ”(FALCON) HELICOPTER MAIN ROTOR IN FORWARD FLIGHT O SZULC, P DOERFFER, F TEJERO, J ŻÓŁTAK, J MAŁECKI TASK QUARTERLY 19 (2), 181-196, 2014 | 3 | 2014 |
| The Joined Wing Scaled Demonstrator Results of CFD A Dziubiński, S Kuprianowicz, K Surmacz, C Galiński, J Żółtak | 3 | 2014 |
| Flying Object Armour Concept Analysis Based On Helicopter. W Gnarowski, J Zóltak, R Kajka ECMS, 126-129, 2010 | 3 | 2010 |
| Wing Design And Analysis Report AC1, Turbulent Wing, AFT, HLT W Stalewski, J Zoltak CESAR Project (6FP), Deliverable Report D 1, 2.3-7, 2009 | 3 | 2009 |
| Kriging-based framework applied to a multi-point, multi-objective engine air-intake duct aerodynamic optimization problem PS Drężek, S Kubacki, J Żółtak Aerospace 10 (3), 266, 2023 | 2 | 2023 |
Dimitris DrikakisProfessor, University of Nicosia, Cyprus, Vice President for Global PartnershipsVerified email at unic.ac.cy
