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Publikováno v:
Metal Science and Heat Treatment. 43:298-301
A comprehensive study of the suitability of sheets of alloy 1441 of the Al – Cu – Mg – Li system for the production of long-life airplane fuselages is described. The alloy has been used in the Be 103 boatplane airframe and is tested for use in
Publikováno v:
Materials Science Forum. :907-912
A cooperative investigation was conducted to evaluate Al-Cu-Mg-Li alloy 1441 for long service life fuselage applications. Alloy 1441 is currently being used for fuselage applications on the Russian Be-103 amphibious aircraft, and is expected to be us
Autor:
D. L. Dicus
The effects of water vapor on fatigue crack growth in 7475-T651 aluminum alloy plate at frequencies of 1 Hz and 10 Hz were investigated. Twenty-five mm thick compact specimens were subjected to constant amplitude fatigue testing at a load ratio of 0.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::907ce444839f5e9a1b50db9fdd36f4fa
https://doi.org/10.1520/stp34452s
https://doi.org/10.1520/stp34452s