Librería: PsychoBabel & Skoob Books, Didcot, Reino Unido
EUR 117,91
Convertir monedaCantidad disponible: 1 disponibles
Añadir al carritoHardcover. Condición: Very Good. Estado de la sobrecubierta: No Dust Jacket. Hardcover with printed boards, no dust jacket, in very good condition. Board corners are slightly bumped. Label affixed to FEP to cover ink mark. Binding is sound and pages are clear. LW. Used.
Librería: Buchpark, Trebbin, Alemania
Condición: Sehr gut. Zustand: Sehr gut | Sprache: Englisch | Produktart: Bücher.
Librería: Best Price, Torrance, CA, Estados Unidos de America
EUR 104,49
Convertir monedaCantidad disponible: 1 disponibles
Añadir al carritoCondición: New. SUPER FAST SHIPPING.
Librería: Ria Christie Collections, Uxbridge, Reino Unido
EUR 128,65
Convertir monedaCantidad disponible: Más de 20 disponibles
Añadir al carritoCondición: New. In.
Publicado por Springer US, Springer US, 2014
ISBN 10: 1489983708 ISBN 13: 9781489983701
Idioma: Inglés
Librería: AHA-BUCH GmbH, Einbeck, Alemania
EUR 122,12
Convertir monedaCantidad disponible: 1 disponibles
Añadir al carritoTaschenbuch. Condición: 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.
Publicado por Springer US, Springer US Nov 2014, 2014
ISBN 10: 1489983708 ISBN 13: 9781489983701
Idioma: Inglés
Librería: buchversandmimpf2000, Emtmannsberg, BAYE, Alemania
EUR 117,69
Convertir monedaCantidad disponible: 2 disponibles
Añadir al carritoTaschenbuch. Condición: Neu. 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.Springer Verlag GmbH, Tiergartenstr. 17, 69121 Heidelberg 432 pp. Englisch.
Librería: Books Puddle, New York, NY, Estados Unidos de America
EUR 157,93
Convertir monedaCantidad disponible: 4 disponibles
Añadir al carritoCondición: New. pp. 432.
Librería: Ria Christie Collections, Uxbridge, Reino Unido
EUR 165,81
Convertir monedaCantidad disponible: Más de 20 disponibles
Añadir al carritoCondición: New. In.
Librería: Best Price, Torrance, CA, Estados Unidos de America
EUR 147,84
Convertir monedaCantidad disponible: 2 disponibles
Añadir al carritoCondición: New. SUPER FAST SHIPPING.
Librería: Mispah books, Redhill, SURRE, Reino Unido
EUR 176,27
Convertir monedaCantidad disponible: 1 disponibles
Añadir al carritoPaperback. Condición: Like New. Like New. book.
Librería: Lucky's Textbooks, Dallas, TX, Estados Unidos de America
EUR 156,70
Convertir monedaCantidad disponible: Más de 20 disponibles
Añadir al carritoCondición: New.
Librería: AHA-BUCH GmbH, Einbeck, Alemania
EUR 247,94
Convertir monedaCantidad disponible: 2 disponibles
Añadir al carritoBuch. Condición: Neu. 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.
Librería: moluna, Greven, Alemania
EUR 98,54
Convertir monedaCantidad disponible: Más de 20 disponibles
Añadir al carritoCondición: 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.
Librería: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Alemania
EUR 117,69
Convertir monedaCantidad disponible: 2 disponibles
Añadir al carritoTaschenbuch. Condición: 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.
Publicado por Springer-Verlag New York Inc., 2014
ISBN 10: 1489983708 ISBN 13: 9781489983701
Idioma: Inglés
Librería: THE SAINT BOOKSTORE, Southport, Reino Unido
EUR 150,93
Convertir monedaCantidad disponible: Más de 20 disponibles
Añadir al carritoPaperback / softback. Condición: New. This item is printed on demand. New copy - Usually dispatched within 5-9 working days 658.
Librería: moluna, Greven, Alemania
EUR 137,26
Convertir monedaCantidad disponible: Más de 20 disponibles
Añadir al carritoGebunden. Condición: 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.
Librería: Majestic Books, Hounslow, Reino Unido
EUR 163,99
Convertir monedaCantidad disponible: 4 disponibles
Añadir al carritoCondición: New. Print on Demand pp. 432.
Librería: Biblios, Frankfurt am main, HESSE, Alemania
EUR 169,07
Convertir monedaCantidad disponible: 4 disponibles
Añadir al carritoCondición: New. PRINT ON DEMAND pp. 432.