| 书目名称 | Virtual Testing and Predictive Modeling | | 副标题 | For Fatigue and Frac | | 编辑 | Bahram Farahmand | | 视频video | | | 概述 | Provides cost-effective and efficient approaches to obtain fatigue and fracture data.Describes virtual testing techniques that prove adequate life in manufactured structural parts.Written with a uniqu | | 图书封面 |  | | 描述 | Thematerialsusedinmanufacturingtheaerospace,aircraft,automobile,andnuclear parts have inherent aws that may grow under uctuating load environments during the operational phase of the structural hardware. The design philosophy, material selection, analysis approach, testing, quality control, inspection, and manufacturing are key elements that can contribute to failure prevention and assure a trouble-free structure. To have a robust structure, it must be designed to withstand the envir- mental load throughout its service life, even when the structure has pre-existing aws or when a part of the structure has already failed. If the design philosophy of the structure is based on the fail-safe requirements, or multiple load path design, partial failure of a structural component due to crack propagation is localized and safely contained or arrested. For that reason, proper inspection technique must be scheduled for reusable parts to detect the amount and rate of crack growth, and the possible need for repairing or replacement of the part. An example of a fail-sa- designed structure with crack-arrest feature, common to all aircraft structural parts, is the skin-stiffened design con guration | | 出版日期 | Book 2009 | | 关键词 | composite; composite material; continuum mechanics; damage; deformation; fatigue; fracture; fracture mechan | | 版次 | 1 | | doi | https://doi.org/10.1007/978-0-387-95924-5 | | isbn_softcover | 978-1-4899-8370-1 | | isbn_ebook | 978-0-387-95924-5 | | copyright | Springer-Verlag US 2009 |
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发表于 2025-3-21 17:58:04
