Return to search

Parametrická tvarová optimalizace letounu z aerodynamického hlediska / Aerodynamics Parametric Shape Aircraft Optimization

The work deals with the use of geometric parameterization for shape description of some parts of the airplane. Geometric parametrization is used for creating a parametric model airfoil. This parametric model allows local deformations pobrchu profile and can easily be applied to generate the geometry of the wing or other parts letoumu. Some properties of the parametric model were tested applications in aerodynamic optimization. Furthermore, the work deals with the parametric description of the blades, the aerodynamic optimization and noise analysis. For propeller blade were created distribution function of the control parameters that can be used in aerodynamic optimization of the blades. Geometric parameterization is used for identifying the location and other characteristics of noise sources.

Identiferoai:union.ndltd.org:nusl.cz/oai:invenio.nusl.cz:234201
Date January 2014
CreatorsDofek, Ivan
ContributorsSalga, Jaroslav, Brož,, Václav, Fiľakovský, Karol
PublisherVysoké učení technické v Brně. Fakulta strojního inženýrství
Source SetsCzech ETDs
LanguageCzech
Detected LanguageEnglish
Typeinfo:eu-repo/semantics/doctoralThesis
Rightsinfo:eu-repo/semantics/restrictedAccess

Page generated in 0.0018 seconds