Idioma: Inglés
Publicado por Smithers Rapra Technology, 2012
ISBN 10: 1847355862 ISBN 13: 9781847355867
Librería: EMCSquared, Doncaster, Reino Unido
EUR 31,26
Cantidad disponible: 1 disponibles
Añadir al carritoSoft cover. Condición: New. New Paperback book in stock and ready to ship!
EUR 12,99
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Añadir al carritoCondición: Muy bueno. : Este libro explora la relación entre Ezra Pound y la República Social Italiana, analizando su obra en el contexto del fascismo italiano. Originalmente publicado en 2009 y revisado en 2011, el autor, Antonio Pantano, ofrece una interpretación crítica de la obra de Pound y su conexión con los eventos históricos de la época. Incluye referencias bibliográficas. EAN: 9788875573683 Tipo: Libros Categoría: Historia Título: Ezra Pound e la Repubblica sociale italiana Autor: Antonio Pantano Idioma: ita Páginas: 279.
Idioma: Inglés
Publicado por LAP LAMBERT Academic Publishing, 2010
ISBN 10: 3838317777 ISBN 13: 9783838317779
Librería: preigu, Osnabrück, Alemania
EUR 57,30
Cantidad disponible: 5 disponibles
Añadir al carritoTaschenbuch. Condición: Neu. A NEW THERMAL THEORY FOR THERMO-MECHANICAL ANALYSIS OF COMPOSITES | A novel advanced finite element model for analysis of heat transfer in laminated composite structures | Antonio Pantano | Taschenbuch | 180 S. | Englisch | 2010 | LAP LAMBERT Academic Publishing | EAN 9783838317779 | Verantwortliche Person für die EU: BoD - Books on Demand, In de Tarpen 42, 22848 Norderstedt, info[at]bod[dot]de | Anbieter: preigu.
Idioma: Inglés
Publicado por LAP Lambert Academic Publishing, 2009
ISBN 10: 3838317777 ISBN 13: 9783838317779
Librería: Revaluation Books, Exeter, Reino Unido
EUR 134,93
Cantidad disponible: 1 disponibles
Añadir al carritoPaperback. Condición: Brand New. 180 pages. 8.66x5.91x0.41 inches. In Stock.
Idioma: Inglés
Publicado por LAP Lambert Academic Publishing, 2010
ISBN 10: 3838321537 ISBN 13: 9783838321530
Librería: Mispah books, Redhill, SURRE, Reino Unido
EUR 175,55
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Añadir al carritoPaperback. Condición: Like New. LIKE NEW. SHIPS FROM MULTIPLE LOCATIONS. book.
Idioma: Inglés
Publicado por Smithers Rapra Technology, 2012
ISBN 10: 1847355854 ISBN 13: 9781847355850
Librería: Mispah books, Redhill, SURRE, Reino Unido
EUR 292,18
Cantidad disponible: 1 disponibles
Añadir al carritoHardcover. Condición: Like New. LIKE NEW. SHIPS FROM MULTIPLE LOCATIONS. book.
Idioma: Inglés
Publicado por LAP LAMBERT Academic Publishing Mai 2010, 2010
ISBN 10: 3838317777 ISBN 13: 9783838317779
Librería: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Alemania
EUR 68,00
Cantidad disponible: 2 disponibles
Añadir al carritoTaschenbuch. Condición: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -The use of laminated and sandwich construction to achieve multi-functional objectives within a single structure continues to increase. It is especially desirable to use laminated construction in structures exposed to thermal loading, where heat resistant coating materials may be bonded to traditional structural materials. Design of such structures requires an accurate analysis of stresses induced by thermal as well as mechanical loads. A novel laminated plate theory and 3D finite element model based on first-order zig-zag sublaminate approximations are presented for thermal stress analysis of composite laminates and sandwich plates. The finite element is developed with the topology of an eight-noded brick, which can contain several physical layers. The novel features of the formulation allow accurate and efficient prediction of the distribution of temperatures, displacements and stresses in laminated plates wherein the plies have dissimilar thermal and/or structural properties. This work is aimed at research workers and students in mechanical engineer. It would also be of great interest to all scientists concerned with thermal stress behavior of composites. 180 pp. Englisch.
Idioma: Inglés
Publicado por LAP LAMBERT Academic Publishing Okt 2009, 2009
ISBN 10: 3838321537 ISBN 13: 9783838321530
Librería: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Alemania
EUR 79,00
Cantidad disponible: 1 disponibles
Añadir al carritoTaschenbuch. Condición: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -Modern computers have enabled engineers to perform large scale analyses of complex structures like entire aircrafts, automobiles, and ships. One issue that arises often is the need to perform a unified analysis of a structural assembly using sub-structural models created independently. These sub-structural models are frequently designed by different engineers, thus they are likely to be incompatible at their interfaces. Finite element interface technology has been developed to facilitate the joining of independently modeled substructures. Here an effective and robust interface element is presented. This method has been developed using penalty constraints and allows computationally efficient coupling of finite element models whose nodes do not necessarily coincide along their common interface. A significant effort has been directed toward developing an automatic calculation of the proper penalty parameter. Additionally, the interface formulation has been modified to simulate delamination growth in composite laminates. This work is aimed at research workers and students in mechanical engineer. It would also be of great interest to all scientists concerned with numerical simulations. 256 pp. Englisch.
Idioma: Inglés
Publicado por LAP LAMBERT Academic Publishing, 2010
ISBN 10: 3838317777 ISBN 13: 9783838317779
Librería: moluna, Greven, Alemania
EUR 55,21
Cantidad 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. Autor/Autorin: Pantano AntonioAntonio Pantano, Ph.D: Studied Engineering Mechanics at Michigan State University. Researcher at Massachusetts Institute of Technology. Director at Ausonia Servizi S.r.l., Palermo, Italy. Professor Rientro dei Cervell.
Idioma: Inglés
Publicado por LAP Lambert Academic Publishing, 2009
ISBN 10: 3838321537 ISBN 13: 9783838321530
Librería: moluna, Greven, Alemania
EUR 63,42
Cantidad 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. Modern computers have enabled engineers to perform large scale analyses of complex structures like entire aircrafts, automobiles, and ships. One issue that arises often is the need to perform a unified analysis of a structural assembly using sub-structural .
Idioma: Inglés
Publicado por LAP LAMBERT Academic Publishing Mai 2010, 2010
ISBN 10: 3838317777 ISBN 13: 9783838317779
Librería: buchversandmimpf2000, Emtmannsberg, BAYE, Alemania
EUR 68,00
Cantidad disponible: 1 disponibles
Añadir al carritoTaschenbuch. Condición: Neu. This item is printed on demand - Print on Demand Titel. Neuware -The use of laminated and sandwich construction to achieve multi-functional objectives within a single structure continues to increase. It is especially desirable to use laminated construction in structures exposed to thermal loading, where heat resistant coating materials may be bonded to traditional structural materials. Design of such structures requires an accurate analysis of stresses induced by thermal as well as mechanical loads. A novel laminated plate theory and 3D finite element model based on first-order zig-zag sublaminate approximations are presented for thermal stress analysis of composite laminates and sandwich plates. The finite element is developed with the topology of an eight-noded brick, which can contain several physical layers. The novel features of the formulation allow accurate and efficient prediction of the distribution of temperatures, displacements and stresses in laminated plates wherein the plies have dissimilar thermal and/or structural properties. This work is aimed at research workers and students in mechanical engineer. It would also be of great interest to all scientists concerned with thermal stress behavior of composites.VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 180 pp. Englisch.
Idioma: Inglés
Publicado por LAP LAMBERT Academic Publishing, 2009
ISBN 10: 3838317777 ISBN 13: 9783838317779
Librería: AHA-BUCH GmbH, Einbeck, Alemania
EUR 68,00
Cantidad disponible: 1 disponibles
Añadir al carritoTaschenbuch. Condición: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - The use of laminated and sandwich construction to achieve multi-functional objectives within a single structure continues to increase. It is especially desirable to use laminated construction in structures exposed to thermal loading, where heat resistant coating materials may be bonded to traditional structural materials. Design of such structures requires an accurate analysis of stresses induced by thermal as well as mechanical loads. A novel laminated plate theory and 3D finite element model based on first-order zig-zag sublaminate approximations are presented for thermal stress analysis of composite laminates and sandwich plates. The finite element is developed with the topology of an eight-noded brick, which can contain several physical layers. The novel features of the formulation allow accurate and efficient prediction of the distribution of temperatures, displacements and stresses in laminated plates wherein the plies have dissimilar thermal and/or structural properties. This work is aimed at research workers and students in mechanical engineer. It would also be of great interest to all scientists concerned with thermal stress behavior of composites.
Idioma: Inglés
Publicado por LAP LAMBERT Academic Publishing, 2010
ISBN 10: 3838321537 ISBN 13: 9783838321530
Librería: preigu, Osnabrück, Alemania
EUR 65,80
Cantidad disponible: 5 disponibles
Añadir al carritoTaschenbuch. Condición: Neu. A PENALTY-BASED INTERFACE TECHNOLOGY | A penalty-based interface technology for connecting independently modeled substructures and for simulating delamination growth in composite structures | Antonio Pantano | Taschenbuch | 256 S. | Englisch | 2010 | LAP LAMBERT Academic Publishing | EAN 9783838321530 | Verantwortliche Person für die EU: BoD - Books on Demand, In de Tarpen 42, 22848 Norderstedt, info[at]bod[dot]de | Anbieter: preigu Print on Demand.
Idioma: Inglés
Publicado por LAP LAMBERT Academic Publishing Okt 2009, 2009
ISBN 10: 3838321537 ISBN 13: 9783838321530
Librería: buchversandmimpf2000, Emtmannsberg, BAYE, Alemania
EUR 79,00
Cantidad disponible: 1 disponibles
Añadir al carritoTaschenbuch. Condición: Neu. This item is printed on demand - Print on Demand Titel. Neuware -Modern computers have enabled engineers to perform large scale analyses of complex structures like entire aircrafts, automobiles, and ships. One issue that arises often is the need to perform a unified analysis of a structural assembly using sub-structural models created independently. These sub-structural models are frequently designed by different engineers, thus they are likely to be incompatible at their interfaces. Finite element interface technology has been developed to facilitate the joining of independently modeled substructures. Here an effective and robust interface element is presented. This method has been developed using penalty constraints and allows computationally efficient coupling of finite element models whose nodes do not necessarily coincide along their common interface. A significant effort has been directed toward developing an automatic calculation of the proper penalty parameter. Additionally, the interface formulation has been modified to simulate delamination growth in composite laminates. This work is aimed at research workers and students in mechanical engineer. It would also be of great interest to all scientists concerned with numerical simulations.VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 256 pp. Englisch.
Idioma: Inglés
Publicado por LAP LAMBERT Academic Publishing, 2010
ISBN 10: 3838321537 ISBN 13: 9783838321530
Librería: AHA-BUCH GmbH, Einbeck, Alemania
EUR 79,00
Cantidad disponible: 1 disponibles
Añadir al carritoTaschenbuch. Condición: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - Modern computers have enabled engineers to perform large scale analyses of complex structures like entire aircrafts, automobiles, and ships. One issue that arises often is the need to perform a unified analysis of a structural assembly using sub-structural models created independently. These sub-structural models are frequently designed by different engineers, thus they are likely to be incompatible at their interfaces. Finite element interface technology has been developed to facilitate the joining of independently modeled substructures. Here an effective and robust interface element is presented. This method has been developed using penalty constraints and allows computationally efficient coupling of finite element models whose nodes do not necessarily coincide along their common interface. A significant effort has been directed toward developing an automatic calculation of the proper penalty parameter. Additionally, the interface formulation has been modified to simulate delamination growth in composite laminates. This work is aimed at research workers and students in mechanical engineer. It would also be of great interest to all scientists concerned with numerical simulations.