Fatigue Crack Growth History in Concept of Damage Tolerance of Aircraft Structures

Kód výsledku v IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21340%2F07%3A00134923" target="_blank" >RIV/68407700:21340/07:00134923 - isvavai.cz</a>
Výsledek na webu
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Jazyk výsledku
angličtina
Název v původním jazyce
Fatigue Crack Growth History in Concept of Damage Tolerance of Aircraft Structures
Popis výsledku v původním jazyce
The knowledge of the real history of fatigue process is very valuable for design, development and reliable operation of structures exposed to the time-variable loading service conditions. Information of this type is encoded in the fracture surface morphology. It is possible to decode this information by means of quantitative fractography and transform it into the form interesting from engineering point of view. Importance and irreplaceable role of the fractographic analysis is illustrated by some case studies dealing with the full-scale fatigue tests of aircraft structure parts.
Název v anglickém jazyce
Fatigue Crack Growth History in Concept of Damage Tolerance of Aircraft Structures
Popis výsledku anglicky
The knowledge of the real history of fatigue process is very valuable for design, development and reliable operation of structures exposed to the time-variable loading service conditions. Information of this type is encoded in the fracture surface morphology. It is possible to decode this information by means of quantitative fractography and transform it into the form interesting from engineering point of view. Importance and irreplaceable role of the fractographic analysis is illustrated by some case studies dealing with the full-scale fatigue tests of aircraft structure parts.

Rok uplatnění
2007
Kód důvěrnosti údajů
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

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