"The paper deals with an experimental research of active boundary layer control using periodic excitation by a synthetic jet on a straight compressor blade cascade flow. Synthetic jet was introduced on the side wall of the tunnel perpendicularly into the main flow just in position of leading edge of compressor blades. Visualizations of the flow field on the wall and total loss coefficient were obtained."@en . . "4"^^ . . . "[8D569FD0C8E8]" . "0-9533991-9-2" . . "P(1M06059), P(GA101/08/1112)" . "2008-09-14+02:00"^^ . . . . "ICAS 2008 - Proceedings" . "RIV/68407700:21220/08:02148468" . "8"^^ . "International Council of the Aeronautical Sciences" . "Separation Control by Synthetic Jet Actuator in Straight Blade Cascade" . "Separation Control by Synthetic Jet Actuator in Straight Blade Cascade"@en . "\u0160afa\u0159\u00EDk, Pavel" . "Anchorage" . "394440" . . "RIV/68407700:21220/08:02148468!RIV09-MSM-21220___" . . . . "Anchorage, Alaska" . . . "\u0158\u00EDzen\u00ED odtr\u017Een\u00ED mezn\u00ED vrstvy syntetizovan\u00FDm paprskem v p\u0159\u00EDm\u00E9 lopatkov\u00E9 m\u0159\u00ED\u017Ei"@cs . "V \u010Dl\u00E1nku je shrnut vliv syntetizovan\u00E9ho paprsku (periodick\u00E9 vyfukov\u00E1n\u00ED a nas\u00E1v\u00E1n\u00ED) na proudov\u00E9 pole v p\u0159\u00EDm\u00E9 kompresorov\u00E9 lopatkov\u00E9 m\u0159\u00ED\u017Ei. V\u00FDstupn\u00ED obdl\u00E9n\u00EDkov\u00FD otvor (slot) gener\u00E1toru syntetizovan\u00E9ho paprsku byl um\u00EDst\u011Bn na bo\u010Dn\u00ED st\u011Bnu tunelu na spojnici n\u00E1b\u011B\u017En\u00FDch hran soused\u00EDc\u00EDch lopatek."@cs . "blade cascade; flow control; synthetic jet"@en . "No\u017Ei\u010Dka, Ji\u0159\u00ED" . "\u0158\u00EDzen\u00ED odtr\u017Een\u00ED mezn\u00ED vrstvy syntetizovan\u00FDm paprskem v p\u0159\u00EDm\u00E9 lopatkov\u00E9 m\u0159\u00ED\u017Ei"@cs . . . . . . "Separation Control by Synthetic Jet Actuator in Straight Blade Cascade" . "21220" . "The paper deals with an experimental research of active boundary layer control using periodic excitation by a synthetic jet on a straight compressor blade cascade flow. Synthetic jet was introduced on the side wall of the tunnel perpendicularly into the main flow just in position of leading edge of compressor blades. Visualizations of the flow field on the wall and total loss coefficient were obtained." . "Popelka, L." . "Mat\u011Bjka, Milan" . "Separation Control by Synthetic Jet Actuator in Straight Blade Cascade"@en . . "3"^^ .