Fatigue Crack Growth History in Concept of Damage Tolerance of Aircraft Structures
The result's identifiers
Result code in 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>
Result on the web
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DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
Fatigue Crack Growth History in Concept of Damage Tolerance of Aircraft Structures
Original language description
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.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
JL - Fatigue and fracture mechanics
OECD FORD branch
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Result continuities
Project
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Continuities
Z - Vyzkumny zamer (s odkazem do CEZ)
Others
Publication year
2007
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
Damage Tolerance of Aircraft Structures
ISBN
978-90-90-22002-4
ISSN
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e-ISSN
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Number of pages
10
Pages from-to
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Publisher name
Delft University of Technology
Place of publication
Delft
Event location
Delft
Event date
Sep 25, 2007
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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