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This overview of cost- and time-efficient methods to obtain fatigue and fracture data introduces two virtual testing techniques. It includes a chapter devoted to the functionalization process as well as coverage of verification methods.
Virtual Testing and Predictive Modeling: For Fatigue and Fracture Mechanics Allowables provides an overview of cost and time efficient methods in generating the fatigue and fracture data of industrial structural parts.
Readers will find a systematic introduction to virtual testing to generate fatigue and fracture allowables through two useful techniques: the conventional continuum mechanics approach, and the utilization of multiscale modeling and simulation techniques to predict materials’ properties. In addition, a chapter devoted to the functionalization process covers the current approach to this technique, which strengthens interface durability through bonding dissimilar materials. Coverage of verification methods, used with devices such as the Transmission Electron Microscope (TEM) and the Atomic Force Microscope (AFM), are also described, which motivate discussion of the fundamental structure and deformation processes of nanoscale materials.
The virtual testing continuum approach already plays a crucial role in the life assessment of important manufactured structural parts in the aerospace, automotive, aircraft and defense industries when data is inaccessible to engineers. Virtual Testing and Predictive Modeling: For Fatigue and Fracture Mechanics Allowables provides a unique applications-focus view into these valuable methods, filling a critical void in references currently available.
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- VerlagSpringer
- Erscheinungsdatum2014
- ISBN 10 1489983708
- ISBN 13 9781489983701
- EinbandTapa blanda
- Anzahl der Seiten432
- HerausgeberFarahmand Bahram
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Virtual Testing and Predictive Modeling : For Fatigue and Fracture Mechanics Allowables
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Virtual Testing and Predictive Modeling
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ISBN 10: 1489983708
ISBN 13: 9781489983701
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Buchbeschreibung Taschenbuch. Zustand: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -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. However, in other cases, the design p- losophy has safe-life or single load path feature, where analysts must demonstrate that parts have adequate life during their service operation and the possibility of catastrophic failure is remote. For example, all pressurized vessels that have single load path feature are classi ed as high-risk parts. During their service operation, these tanks may develop cracks, which will grow gradually in a stable manner. 432 pp. Englisch. Bestandsnummer des Verkäufers 9781489983701
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Buchbeschreibung Zustand: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Provides cost-effective and efficient approaches to obtain fatigue and fracture dataDescribes virtual testing techniques that prove adequate life in manufactured structural partsWritten with a unique emphasis on applications beneficial to i. Bestandsnummer des Verkäufers 11466639
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Virtual Testing and Predictive Modeling : For Fatigue and Fracture Mechanics Allowables
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Buchbeschreibung Taschenbuch. Zustand: Neu. Druck auf Anfrage Neuware - Printed after ordering - Thematerialsusedinmanufacturingtheaerospace,aircraft,automobile,and nuclear 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. However, in other cases, the design p- losophy has safe-life or single load path feature, where analysts must demonstrate that parts have adequate life during their service operation and the possibility of catastrophic failure is remote. For example, all pressurized vessels that have single load path feature are classi ed as high-risk parts. During their service operation, these tanks may develop cracks, which will grow gradually in a stable manner. Bestandsnummer des Verkäufers 9781489983701
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Buchbeschreibung Zustand: New. This overview of cost- and time-efficient methods to obtain fatigue and fracture data introduces two virtual testing techniques. It includes a chapter devoted to the functionalization process as well as coverage of verification methods. Editor(s): Farahmand, Bahram. Num Pages: 430 pages, 35 black & white tables, biography. BIC Classification: PHD; TGB; TGMT; TRC. Category: (G) General (US: Trade). Dimension: 235 x 155 x 22. Weight in Grams: 658. . 2014. Paperback. . . . . Bestandsnummer des Verkäufers V9781489983701
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Virtual Testing and Predictive Modeling: For Fatigue and Fracture Mechanics Allowables
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(2014)
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ISBN 13: 9781489983701
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Buchbeschreibung Paperback / softback. Zustand: New. This item is printed on demand. New copy - Usually dispatched within 5-9 working days. Bestandsnummer des Verkäufers C9781489983701
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Virtual Testing and Predictive Modeling
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ISBN 10: 1489983708
ISBN 13: 9781489983701
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Buchbeschreibung Zustand: New. This overview of cost- and time-efficient methods to obtain fatigue and fracture data introduces two virtual testing techniques. It includes a chapter devoted to the functionalization process as well as coverage of verification methods. Editor(s): Farahmand, Bahram. Num Pages: 430 pages, 35 black & white tables, biography. BIC Classification: PHD; TGB; TGMT; TRC. Category: (G) General (US: Trade). Dimension: 235 x 155 x 22. Weight in Grams: 658. . 2014. Paperback. . . . . Books ship from the US and Ireland. Bestandsnummer des Verkäufers V9781489983701
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