. "N\u00E1vrh, optimalizace a numerick\u00E1 anal\u00FDza ztr\u00E1ty stability kompozitn\u00ED desky vyztu\u017Een\u00E9 pod\u00E9ln\u00EDky" . . "N\u00E1vrh, optimalizace a numerick\u00E1 anal\u00FDza ztr\u00E1ty stability kompozitn\u00ED desky vyztu\u017Een\u00E9 pod\u00E9ln\u00EDky"@cs . "P\u0159\u00EDsp\u011Bvek se zab\u00FDv\u00E1 n\u00E1vrhem \u010D\u00E1sti leteck\u00E9 konstrukce, kterou tvo\u0159\u00ED kompozitn\u00ED deska vyztu\u017Een\u00E1 kompozitn\u00EDmi pod\u00E9ln\u00EDky. Nejprve byly pomoc\u00ED optimaliza\u010Dn\u00EDho softwaru ATOM vybr\u00E1ny vhodn\u00E9 profily. Vybran\u00E9 profily a jimi vyztu\u017Een\u00E1 deska byly analyzov\u00E1ny jako izotropn\u00ED (duralov\u00E9) a byl vybr\u00E1n profil nejvhodn\u011Bj\u0161\u00ED \u2013 \u201Eobr\u00E1cen\u00E9 T\u201C. Tento profil a t\u0159i varianty desky (r\u016Fzn\u00E1 skladba a konstantn\u00ED vs. prom\u011Bnn\u00E1 tlou\u0161\u0165ka) byly n\u00E1sledn\u011B podrobeny numerick\u00E9 anal\u00FDze na ztr\u00E1tu stability (nyn\u00ED u\u017E jako C/PPS kompozit s tkanou v\u00FDztu\u017E\u00ED) a porovn\u00E1ny mezi sebou." . "Kr\u00E1l, Michal" . . "N\u00E1vrh, optimalizace a numerick\u00E1 anal\u00FDza ztr\u00E1ty stability kompozitn\u00ED desky vyztu\u017Een\u00E9 pod\u00E9ln\u00EDky" . . . . "Paper deals with design of the part of airplane construction which is made from composite plate reinforced with composite stringers. In optimization software ATOM were chosen suitable profiles of the stringers (isotropic material) and the best solution was design as composite one \u2013 \u201Ereversed T\u201C. This profile and three versions of the plate (different lay-up and constant or varying plate thickness) were analyzed on buckling and compared with each other."@en . "DESIGN, OPTIMIZATION AND NUMERICAL ANALYSIS OF THE BUCKLING OF COMPOSITE PLATE WITH STRINGERS"@en . "RIV/68407700:21220/14:00215551" . . "5"^^ . "[7151561ED0AE]" . . . "5"^^ . . "Sedl\u00E1\u010Dek, Radek" . . . "DESIGN, OPTIMIZATION AND NUMERICAL ANALYSIS OF THE BUCKLING OF COMPOSITE PLATE WITH STRINGERS"@en . . "N\u00E1vrh, optimalizace a numerick\u00E1 anal\u00FDza ztr\u00E1ty stability kompozitn\u00ED desky vyztu\u017Een\u00E9 pod\u00E9ln\u00EDky"@cs . . "P(TA03010209), S" . . . . "P\u0159\u00EDsp\u011Bvek se zab\u00FDv\u00E1 n\u00E1vrhem \u010D\u00E1sti leteck\u00E9 konstrukce, kterou tvo\u0159\u00ED kompozitn\u00ED deska vyztu\u017Een\u00E1 kompozitn\u00EDmi pod\u00E9ln\u00EDky. Nejprve byly pomoc\u00ED optimaliza\u010Dn\u00EDho softwaru ATOM vybr\u00E1ny vhodn\u00E9 profily. Vybran\u00E9 profily a jimi vyztu\u017Een\u00E1 deska byly analyzov\u00E1ny jako izotropn\u00ED (duralov\u00E9) a byl vybr\u00E1n profil nejvhodn\u011Bj\u0161\u00ED \u2013 \u201Eobr\u00E1cen\u00E9 T\u201C. Tento profil a t\u0159i varianty desky (r\u016Fzn\u00E1 skladba a konstantn\u00ED vs. prom\u011Bnn\u00E1 tlou\u0161\u0165ka) byly n\u00E1sledn\u011B podrobeny numerick\u00E9 anal\u00FDze na ztr\u00E1tu stability (nyn\u00ED u\u017E jako C/PPS kompozit s tkanou v\u00FDztu\u017E\u00ED) a porovn\u00E1ny mezi sebou."@cs . "R\u016F\u017Ei\u010Dka, Pavel" . "RIV/68407700:21220/14:00215551!RIV15-MSM-21220___" . . . "Padovec, Zden\u011Bk" . "buckling analysis\u016F composite plate with stringers; optimization"@en . "31825" . "R\u016F\u017Ei\u010Dka, Milan" . "21220" .