"Ra\u0161ka, Jan" . . . . . . "3"^^ . "[0809146B1FC6]" . . "Design and Verification of a Jet Trainer Aircraft Primary Structure Repair Using an Adhesively Bonded Boron Composite Patch"@en . "3"^^ . . "RIV/00010669:_____/13:#0001564!RIV14-MPO-00010669" . . . "2013-06-26+02:00"^^ . . . "Design and Verification of a Jet Trainer Aircraft Primary Structure Repair Using an Adhesively Bonded Boron Composite Patch" . "Kos (Greece)" . . "978-960-88104-3-3" . . "Doubrava, Radek" . "Kos (Greece)" . . "Design and Verification of a Jet Trainer Aircraft Primary Structure Repair Using an Adhesively Bonded Boron Composite Patch" . "repair; Metallic structure; Composite patch; bonding; FE analysis"@en . "Laboratory of Technology & Strength of Materials, University of Patras (Greece)" . "RIV/00010669:_____/13:#0001564" . . "68563" . "3rd International Conference of Engineering Against Failure (ICEAF III)" . . "R\u016F\u017Eek, Roman" . . "11"^^ . "Different types of damages or cracks in structural parts of airframe can occur in the service of aging aircrafts. Damages are commonly repaired by patch which can be joined to the original structure by different techniques like riveting and bonding for example. The paper provides information about a repair of fatigue crack in metallic wing structure of a jet trainer aircraft using adhesively bonded boron composite patch. Design and numerical analysis of the repair is presented." . "http://www.vzlu.cz/cz/transfer-vysledku/clanky-ve-sbornicich-d/" . "Design and Verification of a Jet Trainer Aircraft Primary Structure Repair Using an Adhesively Bonded Boron Composite Patch"@en . "I" . . . "Different types of damages or cracks in structural parts of airframe can occur in the service of aging aircrafts. Damages are commonly repaired by patch which can be joined to the original structure by different techniques like riveting and bonding for example. The paper provides information about a repair of fatigue crack in metallic wing structure of a jet trainer aircraft using adhesively bonded boron composite patch. Design and numerical analysis of the repair is presented."@en . .