Zobrazeno 1 - 8
of 8
pro vyhledávání: '"G. H. Bray"'
Publikováno v:
International Journal of Material Forming. 3:1019-1022
Reinforced structures for aircraft fuselages are conventionally composed by base (skin) aluminium plates and reinforcement elements (stringers), joined by riveting operations. During the last decade more effective approaches for reinforced fuselage a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a5211ee92e6f71ffe16e1b0f03fb66bd
https://doi.org/10.1007/s12289-010-0943-5
https://doi.org/10.1007/s12289-010-0943-5
Publikováno v:
Thin-Walled Structures. 47:1608-1622
The effect of an friction stir weld (FSW) on the buckling behavior of an integrally stiffened panel (ISP) structure was investigated. For proper consideration of the buckling modes, the Riks method based on geometric imperfection was introduced. The
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c9a49ac1cb5cbf2ff5674355baab7495
https://doi.org/10.1016/j.tws.2009.05.003
https://doi.org/10.1016/j.tws.2009.05.003
Publikováno v:
Metallurgical and Materials Transactions A. 36:2529-2539
High-cycle fatigue tests were carried out on a newly developed high-strength AA 2026 Al alloy, which was in the form of extrusion bars with square and rectangular cross sections, using a self-aligning four-point-bend rig at room temperature, 15 Hz, a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::41cbc7d6ce145637c8bd9c68d348260c
https://doi.org/10.1007/s11661-005-0126-z
https://doi.org/10.1007/s11661-005-0126-z
Publikováno v:
Fatigue & Fracture of Engineering Materials and Structures. 18:551-564
—The low cycle fatigue (LCF) behavior of two aluminum-lithium alloys was investigated. Efforts were aimed at understanding the effects of microstructure on the cyclic stress-strain behavior and methods by which different microstructures accommodate
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::264cd397551c5ff0be32bc46d486085b
https://doi.org/10.1111/j.1460-2695.1995.tb01417.x
https://doi.org/10.1111/j.1460-2695.1995.tb01417.x
Autor:
G. Feyen, Roberto J. Rioja, Julien Boselli, W. Wang, Dirk C. Mooy, G. H. Bray, Gregory B. Venema
Publikováno v:
ICAA13 Pittsburgh ISBN: 9783319482255
ICAA13: 13th International Conference on Aluminum Alloys
ICAA13: 13th International Conference on Aluminum Alloys
A significant volume of “thick” aluminum plate products is used in the manufacture of an aircraft’s internal structure in applications such as ribs, spars, frames, bulkheads, etc. With the recent launch of more fuel efficient and primarily meta
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b77a53ff2bc1ba1949eb20c63b1cc087
https://doi.org/10.1002/9781118495292.ch85
https://doi.org/10.1002/9781118495292.ch85
Publikováno v:
ICAA13 Pittsburgh ISBN: 9783319482255
ICAA13: 13th International Conference on Aluminum Alloys
ICAA13: 13th International Conference on Aluminum Alloys
Al-Li-Cu-Mg alloy products, with and without Ag additions provide substantial performance advantages over conventional 2xxx products. For lower wing applications, the combination of specific ultimate tensile strength and damage tolerance is of partic
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fa52048712546b229d7ced390908f083
https://doi.org/10.1007/978-3-319-48761-8_77
https://doi.org/10.1007/978-3-319-48761-8_77
Publikováno v:
ICAA13 Pittsburgh ISBN: 9783319482255
ICAA13: 13th International Conference on Aluminum Alloys
ICAA13: 13th International Conference on Aluminum Alloys
From the first use of 2017-T74 on the Junkers F13, improvements have been made to plate and extruded products for applications requiring the highest attainable strength and adequate fracture toughness. One such application is the upper wing of large
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::762e306f67c1973e262a5ddd3f8b33b8
https://doi.org/10.1007/978-3-319-48761-8_86
https://doi.org/10.1007/978-3-319-48761-8_86
Publikováno v:
Metallurgical Transactions A. 23:3055-3066
In ingot metallurgy (IM) alloys, the number of delay cycles following a single tensile overload typically increases from a minimum at an intermediate baseline stress intensity range, ΔKB, with decreasing ΔKB approaching threshold and increasing ΔK
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3b829f4eda312dd59d9250f847a3b8d6
https://doi.org/10.1007/bf02646123
https://doi.org/10.1007/bf02646123