"Composite patch for fatigue crack repair in metallic structures of L-39 aircraft"@en . "Doubrava, Radek" . "V\u00FDzkumn\u00FD a zku\u0161ebn\u00ED leteck\u00FD \u00FAstav, a.s., Praha" . "design; composite; patch; repair; metallic structure"@en . . "527053" . . "Je proveden n\u00E1vrh velikosti a skladby kompozitov\u00E9 z\u00E1platy pro opravu \u00FAnavov\u00E9 trhliny v kovov\u00E9 konstrukci letounu L-39 v\u010Detn\u011B vytvo\u0159en\u00E9ho MKP modelu zat\u00ED\u017Een\u00ED a okrajov\u00FDch podm\u00EDnek. \u00DA\u010Dinnost opravy je experiment\u00E1ln\u011B ov\u011B\u0159ena."@cs . . . "Je proveden n\u00E1vrh velikosti a skladby kompozitov\u00E9 z\u00E1platy pro opravu \u00FAnavov\u00E9 trhliny v kovov\u00E9 konstrukci letounu L-39 v\u010Detn\u011B vytvo\u0159en\u00E9ho MKP modelu zat\u00ED\u017Een\u00ED a okrajov\u00FDch podm\u00EDnek. \u00DA\u010Dinnost opravy je experiment\u00E1ln\u011B ov\u011B\u0159ena." . "Kompozitov\u00E1 z\u00E1plata pro opravu \u00FAnavov\u00E9 trhliny v kovov\u00E9 konstrukci letoun L-39"@cs . "Kompozitov\u00E1 z\u00E1plata pro opravu \u00FAnavov\u00E9 trhliny v kovov\u00E9 konstrukci letoun L-39" . . "RIV/00010669:_____/05:#0000029!RIV06-MPO-00010669" . . . "P(FD-K3/008)" . "R\u016F\u017Eek, Roman" . "Kompozitov\u00E1 z\u00E1plata pro opravu \u00FAnavov\u00E9 trhliny v kovov\u00E9 konstrukci letoun L-39"@cs . "Ra\u0161ka, Jan" . "RIV/00010669:_____/05:#0000029" . . . . "[741A3B63BF24]" . . "Kompozitov\u00E1 z\u00E1plata L-39" . . "3"^^ . "3"^^ . . . . . . "Composite patch for fatigue crack repair in metallic structures of L-39 aircraft"@en . "Oprava trhliny v konstrukci v \u010CR a \u00FAspora n\u00E1klad\u016F p\u0159i zad\u00E1v\u00E1n\u00ED relevantn\u00EDch prac\u00ED do zahrani\u010D\u00ED" . "Oprava trhliny v konstrukci v \u010CR a \u00FAspora n\u00E1klad\u016F p\u0159i zad\u00E1v\u00E1n\u00ED relevantn\u00EDch prac\u00ED do zahrani\u010D\u00ED" . "Kompozitov\u00E1 z\u00E1plata pro opravu \u00FAnavov\u00E9 trhliny v kovov\u00E9 konstrukci letoun L-39" . . . "Composite patch for fatigue crack repair in metallic structure of L-39 aircraft including FE model, boundary conditions and size and plies definitions is designed. The designed repair is experimentally verified."@en . . . .