The conventional approach to through-life-support for aircraft structures can be divided into the following phases: (i) detection of defects, (ii) diagnosis of their nature and significan… Meer...
The conventional approach to through-life-support for aircraft structures can be divided into the following phases: (i) detection of defects, (ii) diagnosis of their nature and significance, (iii) forecasting future behaviour-prognosis, and (iv) pre scription and implementation of remedial measures including repairs. Considerable scientific effort has been devoted to developing the science and technology base for the first three phases. Of particular note is the development of fracture mechanics as a major analytical tool for metals, for predicting residual strength in the presence of cracks ( damage tolerance) and rate of crack propagation under service loading. Intensive effort is currently being devoted to developing similar approaches for fibre composite structures, particularly to assess damage tolerance and durability in the presence of delamination damage. Until recently there has been no major attempt to develop a science and tech nology base for the last phase, particularly with respect to the development of repairs. Approaches are required which will allow assessment of the type and magnitude of defects amenable to repair and the influence of the repair on the stress intensity factor (or some related parameter). Approaches are also required for the development and design of optimum repairs and for assessment of their durability. Books > Engineering Hard cover, Springer Shop<
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The conventional approach to through-life-support for aircraft structures can be divided into the following phases: (i) detection of defects, (ii) diagnosis of their nature and significan… Meer...
The conventional approach to through-life-support for aircraft structures can be divided into the following phases: (i) detection of defects, (ii) diagnosis of their nature and significance, (iii) forecasting future behaviour-prognosis, and (iv) pre scription and implementation of remedial measures including repairs. Considerable scientific effort has been devoted to developing the science and technology base for the first three phases. Of particular note is the development of fracture mechanics as a major analytical tool for metals, for predicting residual strength in the presence of cracks ( damage tolerance) and rate of crack propagation under service loading. Intensive effort is currently being devoted to developing similar approaches for fibre composite structures, particularly to assess damage tolerance and durability in the presence of delamination damage. Until recently there has been no major attempt to develop a science and tech nology base for the last phase, particularly with respect to the development of repairs. Approaches are required which will allow assessment of the type and magnitude of defects amenable to repair and the influence of the repair on the stress intensity factor (or some related parameter). Approaches are also required for the development and design of optimum repairs and for assessment of their durability. Books > Engineering Hard cover, Springer Shop<
Springer.com
new in stock. Verzendingskosten:zzgl. Versandkosten. (EUR 0.00) Details...
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Springer. Used - Good. Ships from UK in 48 hours or less (usually same day). Your purchase helps support Sri Lankan Children's Charity 'The Rainbow Centre'. Ex-library, so s… Meer...
Springer. Used - Good. Ships from UK in 48 hours or less (usually same day). Your purchase helps support Sri Lankan Children's Charity 'The Rainbow Centre'. Ex-library, so some stamps and wear, but in good overall condition. 100% money back guarantee. We are a world class secondhand bookstore based in Hertfordshire, United Kingdom and specialize in high quality textbooks across an enormous variety of subjects. We aim to provide a vast range of textbooks, rare and collectible books at a great price. Our donations to The Rainbow Centre have helped provide an education and a safe haven to hundreds of children who live in appalling conditions. We provide a 100% money back guarantee and are dedicated to providing our customers with the highest standards of service in the bookselling industry., Springer, 2.5<
Kluwer Academic Publishers, 1988. Hardcover. New. Usually Dispatched within 1-2 Business Days , Buy with confidence , excellent customer service, Kluwer Academic Publishers, 1988, 6
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Bonded Repair of Aircraft Structures ab 320.99 € als gebundene Ausgabe: Auflage 1988. Aus dem Bereich: Bücher, Wissenschaft, Technik, Medien > Bücher, SPRINGER NATURE
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The conventional approach to through-life-support for aircraft structures can be divided into the following phases: (i) detection of defects, (ii) diagnosis of their nature and significan… Meer...
The conventional approach to through-life-support for aircraft structures can be divided into the following phases: (i) detection of defects, (ii) diagnosis of their nature and significance, (iii) forecasting future behaviour-prognosis, and (iv) pre scription and implementation of remedial measures including repairs. Considerable scientific effort has been devoted to developing the science and technology base for the first three phases. Of particular note is the development of fracture mechanics as a major analytical tool for metals, for predicting residual strength in the presence of cracks ( damage tolerance) and rate of crack propagation under service loading. Intensive effort is currently being devoted to developing similar approaches for fibre composite structures, particularly to assess damage tolerance and durability in the presence of delamination damage. Until recently there has been no major attempt to develop a science and tech nology base for the last phase, particularly with respect to the development of repairs. Approaches are required which will allow assessment of the type and magnitude of defects amenable to repair and the influence of the repair on the stress intensity factor (or some related parameter). Approaches are also required for the development and design of optimum repairs and for assessment of their durability. Books > Engineering Hard cover, Springer Shop<
new in stock. Verzendingskosten:zzgl. Versandkosten. (EUR 0.00)
The conventional approach to through-life-support for aircraft structures can be divided into the following phases: (i) detection of defects, (ii) diagnosis of their nature and significan… Meer...
The conventional approach to through-life-support for aircraft structures can be divided into the following phases: (i) detection of defects, (ii) diagnosis of their nature and significance, (iii) forecasting future behaviour-prognosis, and (iv) pre scription and implementation of remedial measures including repairs. Considerable scientific effort has been devoted to developing the science and technology base for the first three phases. Of particular note is the development of fracture mechanics as a major analytical tool for metals, for predicting residual strength in the presence of cracks ( damage tolerance) and rate of crack propagation under service loading. Intensive effort is currently being devoted to developing similar approaches for fibre composite structures, particularly to assess damage tolerance and durability in the presence of delamination damage. Until recently there has been no major attempt to develop a science and tech nology base for the last phase, particularly with respect to the development of repairs. Approaches are required which will allow assessment of the type and magnitude of defects amenable to repair and the influence of the repair on the stress intensity factor (or some related parameter). Approaches are also required for the development and design of optimum repairs and for assessment of their durability. Books > Engineering Hard cover, Springer Shop<
new in stock. Verzendingskosten:zzgl. Versandkosten. (EUR 0.00)
Springer. Used - Good. Ships from UK in 48 hours or less (usually same day). Your purchase helps support Sri Lankan Children's Charity 'The Rainbow Centre'. Ex-library, so s… Meer...
Springer. Used - Good. Ships from UK in 48 hours or less (usually same day). Your purchase helps support Sri Lankan Children's Charity 'The Rainbow Centre'. Ex-library, so some stamps and wear, but in good overall condition. 100% money back guarantee. We are a world class secondhand bookstore based in Hertfordshire, United Kingdom and specialize in high quality textbooks across an enormous variety of subjects. We aim to provide a vast range of textbooks, rare and collectible books at a great price. Our donations to The Rainbow Centre have helped provide an education and a safe haven to hundreds of children who live in appalling conditions. We provide a 100% money back guarantee and are dedicated to providing our customers with the highest standards of service in the bookselling industry., Springer, 2.5<
Kluwer Academic Publishers, 1988. Hardcover. New. Usually Dispatched within 1-2 Business Days , Buy with confidence , excellent customer service, Kluwer Academic Publishers, 1988, 6
Bonded Repair of Aircraft Structures ab 320.99 € als gebundene Ausgabe: Auflage 1988. Aus dem Bereich: Bücher, Wissenschaft, Technik, Medien > Bücher, SPRINGER NATURE
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Bibliografische gegevens van het best passende boek
Gedetalleerde informatie over het boek. - Bonded Repair of Aircraft Structures (Engineering Applications of Fracture Mechanics (7), Band 7)
EAN (ISBN-13): 9789024736065 ISBN (ISBN-10): 9024736064 Gebonden uitgave Verschijningsjaar: 1988 Uitgever: Baker, A. Jones, Springer 232 Bladzijden Gewicht: 0,503 kg Taal: eng/Englisch
Boek bevindt zich in het datenbestand sinds 2007-05-27T15:26:44+02:00 (Amsterdam) Detailpagina laatst gewijzigd op 2023-04-11T16:51:52+02:00 (Amsterdam) ISBN/EAN: 9024736064
ISBN - alternatieve schrijfwijzen: 90-247-3606-4, 978-90-247-3606-5 alternatieve schrijfwijzen en verwante zoekwoorden: Auteur van het boek: piccard, jones, baker jed Titel van het boek: engineering fracture mechanics, bonded repair aircraft structures, structure
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