The preliminary design of the air-intake system and the nacelle in the small aircraft-engine integration process
Purpose–The purpose of this paper is to present the results of the preliminary design and
optimization of the air-intake system and the engine nacelle. The work was conducted as …
optimization of the air-intake system and the engine nacelle. The work was conducted as …
[PDF][PDF] Optimisation of the helicopter fuselage with simulation of main and tail rotor influence
The paper presents the methodology of parametric design and optimisation, which was
applied to a redesign of a helicopter fuselage. The purpose of the presented study was to …
applied to a redesign of a helicopter fuselage. The purpose of the presented study was to …
[PDF][PDF] Parametric modelling of aerodynamic objects-the key to successful design and optimisation
W Stalewski - Aerotecnica Missili e Spazio, 2012 - Citeseer
In the paper, the methodology of parametric modelling of complex objects has been
presented. The methodology is especially directed towards aerospace engineering …
presented. The methodology is especially directed towards aerospace engineering …
Aerodynamic optimisation of flat-upper-surface wing
Purpose The paper aims to optimise several concepts of the flat-upper-surface wing that
could install the largest possible number of photovoltaic cells and test them in flight. A wing …
could install the largest possible number of photovoltaic cells and test them in flight. A wing …
Shape optimisation method based on the surrogate models in the parallel asynchronous environment
This paper proposes a new optimisation method, the Parallel Asynchronous Surrogate
Model (PASM) method, which is based on the surrogate models approximation and takes …
Model (PASM) method, which is based on the surrogate models approximation and takes …
A surrogate-based integrated framework for the aerodynamic design optimization of a subsonic wing planform shape
A Benaouali, S Kachel - Proceedings of the Institution of …, 2018 - journals.sagepub.com
Due to the development in computer technology, computational simulations have become
indispensable for most engineering system design processes, particularly in aerospace …
indispensable for most engineering system design processes, particularly in aerospace …
Design of a turbulent wing for small aircraft using multidisciplinary optimisation
Abstract Design process of a turbulent wing for small aircraft, using multidisciplinary and
multi-objective optimisation, based on a genetic algorithm was presented. A generic …
multi-objective optimisation, based on a genetic algorithm was presented. A generic …
[PDF][PDF] Design and optimisation of exhaust system of light turboprop airplane
W Stalewski - Journal of KONES, 2016 - bibliotekanauki.pl
Innovative exhaust system for light turboprop airplane has been developed and optimised.
Apart from the basic function of removing exhaust from turboprop engine, the system …
Apart from the basic function of removing exhaust from turboprop engine, the system …
Performance improvement of helicopter rotors through blade redesigning
Purpose The purpose of this paper is to determine dependencies between a rotor-blade
shape and a rotor performance as well as to search for optimal shapes of blades dedicated …
shape and a rotor performance as well as to search for optimal shapes of blades dedicated …
Simulation and optimization of control of selected phases of gyroplane flight
W Stalewski - Computation, 2018 - mdpi.com
Optimization methods are increasingly used to solve problems in aeronautical engineering.
Typically, optimization methods are utilized in the design of an aircraft airframe or its …
Typically, optimization methods are utilized in the design of an aircraft airframe or its …