Autor:	L. F. Yakovenko, I. N. Fridlyander, Yu. A. Pokhil, E. N. Aleksenko, V. V. Eremenko
Rok vydání:	2000
Předmět:	Materials science Alloy Cryogenics engineering.material Paris' law Crack growth resistance curve Superalloy Crack closure visual_art engineering Aluminium alloy visual_art.visual_art_medium Composite material Stress intensity factor
Zdroj:	Advances in Cryogenic Engineering Materials ISBN: 9781461369264
DOI:	10.1007/978-1-4615-4293-3_14
Popis:	The aim of this study was to investigate fatigue crack growth resistance of a new superlight high-strength Al-Cu-Li alloy at 293 and 77K and to assess the possibility of its application in cryogenic aerospace structures.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::805868aac4ecb36d95595b594128de0e https://doi.org/10.1007/978-1-4615-4293-3_14 Zobrazit plný text záznamu