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Pavel Hospodár, Jan Klesa, Daniel Demovic and Nikola ?i?kovský
In this paper, an aerodynamic and structural computation framework was produced to develop a more efficient aircraft configuration considering a wing with a distributed electric propulsion and its use in different flight missions. For that reason, a mode...
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Svatomir Slavik, Jan Klesa and Jiri Brabec
Selection process of the propeller for short take-off and landing (STOL) category aircraft is described. The aim is to achieve the highest possible performance with fixed propeller, i.e., high maximal horizontal and cruise speed, short take-off and high ...
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