Thickness Influence on Crack Gowth Behaviour Under Constant and Variable Amplitude Loading (7475 T7351)

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F17%3AN0000162" target="_blank" >RIV/00010669:_____/17:N0000162 - isvavai.cz</a>
Result on the web
<a href="https://www.vzlu.cz/vyzkum/" target="_blank" >https://www.vzlu.cz/vyzkum/</a>
DOI - Digital Object Identifier
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Result language
angličtina
Original language name
Thickness Influence on Crack Gowth Behaviour Under Constant and Variable Amplitude Loading (7475 T7351)
Original language description
The report documents experimental research work focused on the thickness influence on crack propagation behaviour of 7475 T7351 plate material under constant and variable amplitude loading. The variable amplitude loading sequence representative for the L410NG airplane was considering. 7475 T7351 plate material with thickness of 76 mm was investigated. The plate material is machined into the final products with different thicknesses (typically from 2 up to 8 mm) in the L410NG airframe structure. Therefore, the research work was focused, and data is reported just within this typical thickness range. The thickness influence on the crack propagation behaviour is proved. The influence of thickness is different for constant and variable amplitude loading.
Czech name
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Czech description
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Project
<a href="/en/project/TE02000032" target="_blank" >TE02000032: Advanced Aerostructures Research Centre</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year
2017
Confidentiality
C - Předmět řešení projektu podléhá obchodnímu tajemství (§ 504 Občanského zákoníku), ale název projektu, cíle projektu a u ukončeného nebo zastaveného projektu zhodnocení výsledku řešení projektu (údaje P03, P04, P15, P19, P29, PN8) dodané do CEP, jsou upraveny tak, aby byly zveřejnitelné.

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