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Wieńczysław Stalewski
Wieńczysław Stalewski
Instytut Lotnictwa, Institute of Aviation
Verified email at ilot.edu.pl
Title
Cited by
Cited by
Year
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
352012
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
292014
Parametric Modelling of Aerodynamic Objects - The Key to Successful Design and Optimisation.
W Stalewski
Aerotecnica Missili & Spazio, 2012
272012
Parametric Modelling of Aerodynamic Objects-The Key to Successful Design and Optimisation.
W Stalewski
Proceedings of CEAS., 2011
272011
Multi-objective and multidisciplinary optimization of wing for small aircraft
W Stalewski, J Żółtak
Proceedings of the CEAS Congress on disc, 1483-1492, 2011
212011
Development of new generation main and tail rotor blade airfoils
W Kania, W Stalewski
Proceedings of 22nd International Council of the Aeronautical Sciences …, 2000
182000
Vortex Ring State Simulation Using Actuator Disc.
W Stalewski, A Dziubiński
Proceedings of 21st European Conference on Modelling and Simulation., 2007
17*2007
Aerodynamic design of modern gyroplane main rotors
W StaleWSkI
Prace Instytutu Lotnictwa, 2016
142016
Multi-Disciplinary Optimisation Of Forward-Swept Wing.
J Rokicki, W Stalewski, J Zoltak
Evolutionary Methods for Design, Optimization and Control., 2009
122009
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
102014
Multicriteria Design and Optimisation of Helicopter Fuselage.
W Stalewski, J Zoltak
Evolutionary and Deterministic Methods for Design, Optimization and Control …, 2011
92011
Aerodynamic Optimisation of Joined-Wing Aeroplane,
W Stalewski
Proceedings of 6th International Conference on Experiments/Process/System …, 2015
82015
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
72016
Flow Control on Helicopter-Rotor Blades via Active Gurney Flap
W Stalewski
30th ICAS Congress of the International Council of the Aeronautical Sciences, 2016
72016
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
62016
Modification of aerodynamic wing loads by fluidic devices
W Stalewski, J Sznajder
Journal of KONES 21 (3), 271--278, 2014
62014
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
62010
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
52020
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