. "Theiner, Robert" . . . . "2"^^ . "Zpr\u00E1va se zab\u00FDv\u00E1 sestaven\u00EDm aerodynamick\u00FDch charakteristik letounu UL-39. Ve zpr\u00E1v\u011B je provedeno shrnut\u00ED aerodynamick\u00FDch charakteristik profilu v konfiguraci se vztlakovou klapkou vych\u00FDlenou do t\u0159\u00ED poloh (0\u02DA,15\u02DA a 35\u02DA). Na z\u00E1klad\u011B profilov\u00FDch hodnot je provedeno sestaven\u00ED vztlakov\u00FDch, momentov\u00FDch a odporov\u00FDch \u010Dar k\u0159\u00EDdla a letounu jako celku. Aerodynamick\u00E9 charakteristiky letounu jsou ur\u010Deny pro letoun ve vyv\u00E1\u017Een\u00E9m stavu (pro dv\u011B hmotov\u00E9 konfigurace) a zahrnuj\u00ED charakteristiky s vlivem a bez vlivu zem\u011B."@cs . "Zpr\u00E1va se zab\u00FDv\u00E1 sestaven\u00EDm aerodynamick\u00FDch charakteristik letounu UL-39. Ve zpr\u00E1v\u011B je provedeno shrnut\u00ED aerodynamick\u00FDch charakteristik profilu v konfiguraci se vztlakovou klapkou vych\u00FDlenou do t\u0159\u00ED poloh (0\u02DA,15\u02DA a 35\u02DA). Na z\u00E1klad\u011B profilov\u00FDch hodnot je provedeno sestaven\u00ED vztlakov\u00FDch, momentov\u00FDch a odporov\u00FDch \u010Dar k\u0159\u00EDdla a letounu jako celku. Aerodynamick\u00E9 charakteristiky letounu jsou ur\u010Deny pro letoun ve vyv\u00E1\u017Een\u00E9m stavu (pro dv\u011B hmotov\u00E9 konfigurace) a zahrnuj\u00ED charakteristiky s vlivem a bez vlivu zem\u011B." . "Aerodynamic calculation of UL-39 airplane"@en . "Aerodynamic calculation of UL-39 airplane"@en . . "Brabec, Ji\u0159\u00ED" . . "2"^^ . . . . . "Aerodynamick\u00FD v\u00FDpo\u010Det letounu UL-39"@cs . "184794" . "Aerodynamick\u00FD v\u00FDpo\u010Det letounu UL-39" . . "21220" . . "RIV/68407700:21220/11:00190246" . . . "Aerodynamick\u00FD v\u00FDpo\u010Det letounu UL-39"@cs . . "Aerodynamick\u00FD v\u00FDpo\u010Det letounu UL-39" . "RIV/68407700:21220/11:00190246!RIV14-MPO-21220___" . "[EEA84CB7C336]" . "This paper deals with evaluation of aerodynamic characteristic of UL-39 airplane. Aerodynamic characteristics of used airfoil are summarised at first. Lift, drag and moment characteristics of complete airplane are determined with and without ground effect."@en . "P(FR-TI3/527)" . . . "Airplane; Aerodynamic; Characteristics"@en .