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Creation of educational experiment for Aerodynamics I course
Fenech, Daniel ; Navrátil, Jan (oponent) ; Popela, Robert (vedoucí práce)
The goal of this thesis is to create a semester-long project for students of the course Aerodynamics I to follow in order to understand better, and gain first-hand experience, how one can determine aerodynamic characteristics through computations and by the use of wind-tunnel. The procedure highlights are how to obtain the geometries of a model using 3-D scanning and manipulating the scanned item to get the required geometries, using XFOIL to obtain 2-D aerodynamic characteristics of aerofoils, using Glauert III alongside basic computations to obtain aerodynamic coefficients distributions along a whole surface and solving for total forces acting on the model. Finally, wind tunnel test of the model is carried out for validation of the computational part.
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Conceptual study of general aviation electric powered plane
Cervera, Iigo ; Jebáček, Ivo (oponent) ; Popela, Robert (vedoucí práce)
The design of electric aircraft represents an opportunity in the aviation field by offering promising advancements in terms of efficiency and sustainability. This project aims to explore the feasibility of designing a purely electric aircraft at a time when electric mobility is widespread in the automotive sector but not yet in the aviation industry. It will encompass the study of marketing and the market field, as well as the performance characteristics of the model, including the calculation of aircraft surfaces, with the goal of achieving the most realistic project possible.
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Creation of educational experiment for Aerodynamics I course
Fenech, Daniel ; Navrátil, Jan (oponent) ; Popela, Robert (vedoucí práce)
The goal of this thesis is to create a semester-long project for students of the course Aerodynamics I to follow in order to understand better, and gain first-hand experience, how one can determine aerodynamic characteristics through computations and by the use of wind-tunnel. The procedure highlights are how to obtain the geometries of a model using 3-D scanning and manipulating the scanned item to get the required geometries, using XFOIL to obtain 2-D aerodynamic characteristics of aerofoils, using Glauert III alongside basic computations to obtain aerodynamic coefficients distributions along a whole surface and solving for total forces acting on the model. Finally, wind tunnel test of the model is carried out for validation of the computational part.
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