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Description
  • Knowing the real history of the fatigue process is a valuable asset to for design, development, and reliable operation of structures exposed to time-variable loading service conditions. Information of this type is encoded in the fracture morphology. This information can be decoded by quantitative fractography and transformed it into a form interesting from the engineering point of view. Application of these fractographic methods is conditioned by the existence and detectability of fractographic features correlated with fatigue crack growth rate. In the paper presented, three various fractographic features are used for fractographic reconstitution - striations (constant amplitude loading), beach marks (simple program loading), and special inserted fracture marks (complex program loading). The importance and irreplaceable role of the fractographic analysis is illustrated by some case studies dealing with full-scale fatigue tests of aircraft structure parts.
  • Knowing the real history of the fatigue process is a valuable asset to for design, development, and reliable operation of structures exposed to time-variable loading service conditions. Information of this type is encoded in the fracture morphology. This information can be decoded by quantitative fractography and transformed it into a form interesting from the engineering point of view. Application of these fractographic methods is conditioned by the existence and detectability of fractographic features correlated with fatigue crack growth rate. In the paper presented, three various fractographic features are used for fractographic reconstitution - striations (constant amplitude loading), beach marks (simple program loading), and special inserted fracture marks (complex program loading). The importance and irreplaceable role of the fractographic analysis is illustrated by some case studies dealing with full-scale fatigue tests of aircraft structure parts. (en)
Title
  • Fatigue Crack Growth History in Damage Tolerance Design of Aircraft Structures
  • Fatigue Crack Growth History in Damage Tolerance Design of Aircraft Structures (en)
skos:prefLabel
  • Fatigue Crack Growth History in Damage Tolerance Design of Aircraft Structures
  • Fatigue Crack Growth History in Damage Tolerance Design of Aircraft Structures (en)
skos:notation
  • RIV/68407700:21340/09:00160541!RIV10-MSM-21340___
http://linked.open...avai/riv/aktivita
http://linked.open...avai/riv/aktivity
  • Z(MSM6840770021)
http://linked.open...iv/cisloPeriodika
  • 6
http://linked.open...vai/riv/dodaniDat
http://linked.open...aciTvurceVysledku
http://linked.open.../riv/druhVysledku
http://linked.open...iv/duvernostUdaju
http://linked.open...titaPredkladatele
http://linked.open...dnocenehoVysledku
  • 314723
http://linked.open...ai/riv/idVysledku
  • RIV/68407700:21340/09:00160541
http://linked.open...riv/jazykVysledku
http://linked.open.../riv/klicovaSlova
  • fatigue; crack growth rate; crack front; striations beach marks; fractographic reconstitution; full-scale test (en)
http://linked.open.../riv/klicoveSlovo
http://linked.open...odStatuVydavatele
  • NL - Nizozemsko
http://linked.open...ontrolniKodProRIV
  • [9639D4362563]
http://linked.open...i/riv/nazevZdroje
  • International Journal of Fatigue
http://linked.open...in/vavai/riv/obor
http://linked.open...ichTvurcuVysledku
http://linked.open...cetTvurcuVysledku
http://linked.open...UplatneniVysledku
http://linked.open...v/svazekPeriodika
  • 31
http://linked.open...iv/tvurceVysledku
  • Siegl, Jan
  • Kunz, Jiří
  • Nedbal, Ivan
http://linked.open...ain/vavai/riv/wos
  • 000265361600010
http://linked.open...n/vavai/riv/zamer
issn
  • 0142-1123
number of pages
http://localhost/t...ganizacniJednotka
  • 21340
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