Optimisation of the Helicopter Fuselage with Simulation of Main and Tail Rotor Influence. W Stalewski, J Zoltak 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: An International Journal 86 …, 2014 | 30 | 2014 |
Parametric Modelling of Aerodynamic Objects - The Key to Successful Design and Optimisation. W Stalewski Aerotecnica Missili & Spazio, 2012 | 27 | 2012 |
Parametric Modelling of Aerodynamic Objects-The Key to Successful Design and Optimisation. W Stalewski Proceedings of CEAS., 2011 | 27 | 2011 |
Multi-objective and multidisciplinary optimization of wing for small aircraft W Stalewski, J Żółtak Proceedings of the CEAS Congress on disc, 1483-1492, 2011 | 23 | 2011 |
Vortex Ring State Simulation Using Actuator Disc. W Stalewski, A Dziubiński Proceedings of 21st European Conference on Modelling and Simulation., 2007 | 18* | 2007 |
Development of new generation main and tail rotor blade airfoils W Kania, W Stalewski Proceedings of 22nd International Council of the Aeronautical Sciences …, 2000 | 18 | 2000 |
Aerodynamic design of modern gyroplane main rotors W StaleWSkI Prace Instytutu Lotnictwa, 2016 | 14 | 2016 |
Multi-Disciplinary Optimisation Of Forward-Swept Wing. J Rokicki, W Stalewski, J Zoltak Evolutionary Methods for Design, Optimization and Control., 2009 | 12 | 2009 |
Przykłady Zastosowania Pakietu FLUENT™ w Analizach Bezpieczeństwa Lotu Śmigłowców W Stalewski, J Żółtak, A Dziubiński Prace Instytutu Lotnictwa, 2008 | 11* | 2008 |
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 Zoltak Evolutionary and Deterministic Methods for Design, Optimization and Control …, 2011 | 10 | 2011 |
Flow Control on Helicopter-Rotor Blades via Active Gurney Flap W Stalewski 30th ICAS Congress of the International Council of the Aeronautical Sciences, 2016 | 8 | 2016 |
Aerodynamic Optimisation of Joined-Wing Aeroplane, W Stalewski Proceedings of 6th International Conference on Experiments/Process/System …, 2015 | 8 | 2015 |
Overview of the Inverted Joined Wing Scaled Demonstrator Programme C Galinski, W Stalewski, M Lis, J Hajduk 30th ICAS Congress of the International Council of the Aeronautical Sciences, 2016 | 7 | 2016 |
Designing the modern family of helicopters airfoils. W Kania, W Stalewski Wienczyslaw, B Zwierchanowska Transaction of the Institute of Aviation 4, 197, 2007 | 7* | 2007 |
Design and optimisation of exhaust system of light turboprop airplane W Stalewski Journal of KONES 23 (2), 341-348, 2016 | 6 | 2016 |
Modification of aerodynamic wing loads by fluidic devices W Stalewski, J Sznajder Journal of KONES 21 (3), 271--278, 2014 | 6 | 2014 |
Application of a panel method with viscous-in-viscid interaction for the determination of aerodynamic characteristics of Cesar Base-Line aircraft W Stalewski, J Sznajder Prace Instytutu Lotnictwa, 76-97, 2010 | 6 | 2010 |
Investigations of the vortex ring state on a helicopter main rotor using the URANS solver W Stalewski, K Surmacz Aircraft Engineering and Aerospace Technology 92 (9), 1327-1337, 2020 | 5 | 2020 |