Articoli correlati a Virtual Testing and Predictive Modeling: For Fatigue...

Virtual Testing and Predictive Modeling: For Fatigue and Fracture Mechanics Allowables - Brossura

 
9781489983701: Virtual Testing and Predictive Modeling: For Fatigue and Fracture Mechanics Allowables
Vedi tutte le copie di questo ISBN:
 
 

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.

Le informazioni nella sezione "Riassunto" possono far riferimento a edizioni diverse di questo titolo.

Dalla quarta di copertina:

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.

Contenuti:
Virtual Testing and Its Application in Aerospace Structural Parts.- Tools for Assessing the Damage Tolerance of Primary Structural Components.- Cohesive Technology Applied to the Modeling and Simulation of Fatigue Failure.- Fatigue Damage Map as a Virtual Tool for Fatigue Damage Tolerance.- Predicting Creep and Creep/Fatigue Crack Initiation and Growth for Virtual Testing and Life Assessment of Components.- Computational Approach Toward Advanced Composite Material Qualification and Structural Certification.- Modeling of Multiscale Fatigue Crack Growth: Nano/Micro and Micro/Macro Transitions.- Multiscale Modeling of Nanocomposite Materials.- Predictive Modeling.- Multiscale Approach to Predicting the Mechanical Behavior of Polymeric Melts.- Prediction of Damage Propagation and Failure of Composite Structures (Without Testing).- Functional Nanostructured Polymer–Metal Interfaces.- Advanced Experimental Techniques for Multiscale Modeling of Materials.

Le informazioni nella sezione "Su questo libro" possono far riferimento a edizioni diverse di questo titolo.

  • EditoreSpringer
  • Data di pubblicazione2014
  • ISBN 10 1489983708
  • ISBN 13 9781489983701
  • RilegaturaCopertina flessibile
  • Numero di pagine432
  • RedattoreFarahmand Bahram

Altre edizioni note dello stesso titolo

9780387959238: Virtual Testing and Predictive Modeling: For Fatigue and Fracture Mechanics Allowables

Edizione in evidenza

ISBN 10:  0387959238 ISBN 13:  9780387959238
Casa editrice: Springer Verlag, 2009
Rilegato

I migliori risultati di ricerca su AbeBooks

Immagini fornite dal venditore

Editore: Springer (2014)
ISBN 10: 1489983708 ISBN 13: 9781489983701
Nuovo Soft Cover Quantità: 1
Da:
booksXpress
(Bayonne, NJ, U.S.A.)
Valutazione libreria

Descrizione libro Soft Cover. Condizione: new. Codice articolo 9781489983701

Informazioni sul venditore | Contatta il venditore

Compra nuovo
EUR 117,11
Convertire valuta

Aggiungere al carrello

Spese di spedizione: GRATIS
In U.S.A.
Destinazione, tempi e costi
Immagini fornite dal venditore

Bahram Farahmand
Editore: Springer US Nov 2014 (2014)
ISBN 10: 1489983708 ISBN 13: 9781489983701
Nuovo Taschenbuch Quantità: 2
Print on Demand
Da:
BuchWeltWeit Ludwig Meier e.K.
(Bergisch Gladbach, Germania)
Valutazione libreria

Descrizione libro Taschenbuch. Condizione: 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. Codice articolo 9781489983701

Informazioni sul venditore | Contatta il venditore

Compra nuovo
EUR 117,69
Convertire valuta

Aggiungere al carrello

Spese di spedizione: EUR 23,00
Da: Germania a: U.S.A.
Destinazione, tempi e costi
Foto dell'editore

Bahram Farahmand
Editore: Springer (2014)
ISBN 10: 1489983708 ISBN 13: 9781489983701
Nuovo Brossura Quantità: > 20
Print on Demand
Da:
Ria Christie Collections
(Uxbridge, Regno Unito)
Valutazione libreria

Descrizione libro Condizione: New. PRINT ON DEMAND Book; New; Fast Shipping from the UK. No. book. Codice articolo ria9781489983701_lsuk

Informazioni sul venditore | Contatta il venditore

Compra nuovo
EUR 130,45
Convertire valuta

Aggiungere al carrello

Spese di spedizione: EUR 11,69
Da: Regno Unito a: U.S.A.
Destinazione, tempi e costi
Immagini fornite dal venditore

Farahmand, Bahram
Editore: Springer US (2014)
ISBN 10: 1489983708 ISBN 13: 9781489983701
Nuovo Brossura Quantità: > 20
Print on Demand
Da:
moluna
(Greven, Germania)
Valutazione libreria

Descrizione libro Condizione: 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. Codice articolo 11466639

Informazioni sul venditore | Contatta il venditore

Compra nuovo
EUR 98,54
Convertire valuta

Aggiungere al carrello

Spese di spedizione: EUR 48,99
Da: Germania a: U.S.A.
Destinazione, tempi e costi
Immagini fornite dal venditore

Bahram Farahmand
Editore: Springer US (2014)
ISBN 10: 1489983708 ISBN 13: 9781489983701
Nuovo Taschenbuch Quantità: 1
Da:
AHA-BUCH GmbH
(Einbeck, Germania)
Valutazione libreria

Descrizione libro Taschenbuch. Condizione: 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. Codice articolo 9781489983701

Informazioni sul venditore | Contatta il venditore

Compra nuovo
EUR 119,10
Convertire valuta

Aggiungere al carrello

Spese di spedizione: EUR 32,99
Da: Germania a: U.S.A.
Destinazione, tempi e costi
Foto dell'editore

Bahram Farahmand
ISBN 10: 1489983708 ISBN 13: 9781489983701
Nuovo Paperback / softback Quantità: > 20
Print on Demand
Da:
THE SAINT BOOKSTORE
(Southport, Regno Unito)
Valutazione libreria

Descrizione libro Paperback / softback. Condizione: New. This item is printed on demand. New copy - Usually dispatched within 5-9 working days. Codice articolo C9781489983701

Informazioni sul venditore | Contatta il venditore

Compra nuovo
EUR 155,67
Convertire valuta

Aggiungere al carrello

Spese di spedizione: EUR 10,48
Da: Regno Unito a: U.S.A.
Destinazione, tempi e costi