Antonio pantano (14 resultados)

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  • Idioma: Inglés

    Editorial: Smithers Rapra Technology, 2012

    1847355862 / 9781847355867

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    Librería: EMCSquared, Doncaster, Reino UnidoEMCSquared

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    Condición: Nuevo

    EUR 31,23

    Envío por EUR 4,78 
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    Cantidad disponible: 1 disponibles

    Soft cover. Condición: New. New Paperback book in stock and ready to ship.

  • Idioma: Inglés

    Editorial: LAP LAMBERT Academic Publishing, 2010

    3838317777 / 9783838317779

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    Librería: preigu, Osnabrück, Alemaniapreigu

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    Condición: Nuevo

    EUR 58,05

    Envío por EUR 70,00 
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    Cantidad disponible: 5 disponibles

    Taschenbuch. 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

    Editorial: LAP LAMBERT Academic Publishing, 2010

    3838321537 / 9783838321530

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    Librería: preigu, Osnabrück, Alemaniapreigu

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    Condición: Nuevo

    EUR 66,50

    Envío por EUR 70,00 
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    Cantidad disponible: 5 disponibles

    Taschenbuch. 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.

  • Idioma: Inglés

    Editorial: LAP Lambert Academic Publishing, 2009

    3838317777 / 9783838317779

    • Tapa blanda

    Librería: Revaluation Books, Exeter, Reino UnidoRevaluation Books

    Vendedor de 5 estrellas
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    Condición: Nuevo

    EUR 137,84

    Envío por EUR 11,66 
    Se envía de Reino Unido a Estados Unidos de America

    Cantidad disponible: 1 disponibles

    Paperback. Condición: Brand New. 180 pages. 8.66x5.91x0.41 inches. In Stock.

  • Idioma: Inglés

    Editorial: LAP Lambert Academic Publishing, 2010

    3838321537 / 9783838321530

    • Tapa blanda

    Librería: Mispah books, Redhill, SURRE, Reino UnidoMispah books

    Vendedor de 4 estrellas
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    Condición: Usado - Como Nuevo

    EUR 175,37

    Envío por EUR 29,15 
    Se envía de Reino Unido a Estados Unidos de America

    Cantidad disponible: 1 disponibles

    Paperback. Condición: Like New. LIKE NEW. SHIPS FROM MULTIPLE LOCATIONS. book.

  • Idioma: Inglés

    Editorial: Smithers Rapra Technology, 2012

    1847355854 / 9781847355850

    • Tapa dura

    Librería: Mispah books, Redhill, SURRE, Reino UnidoMispah books

    Vendedor de 4 estrellas
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    Condición: Usado - Como Nuevo

    EUR 291,88

    Envío por EUR 29,15 
    Se envía de Reino Unido a Estados Unidos de America

    Cantidad disponible: 1 disponibles

    Hardcover. Condición: Like New. LIKE NEW. SHIPS FROM MULTIPLE LOCATIONS. book.

  • Idioma: Inglés

    Editorial: LAP LAMBERT Academic Publishing Mai 2010, 2010

    3838317777 / 9783838317779

    • Tapa blanda
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    Librería: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, AlemaniaBuchWeltWeit Ludwig Meier e.K.

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    Condición: Nuevo

    EUR 68,00

    Envío por EUR 23,00 
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    Cantidad disponible: 2 disponibles

    Taschenbuch. 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

    Editorial: LAP LAMBERT Academic Publishing Okt 2009, 2009

    3838321537 / 9783838321530

    • Tapa blanda
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    Librería: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, AlemaniaBuchWeltWeit Ludwig Meier e.K.

    Vendedor de 5 estrellas
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    Condición: Nuevo

    EUR 79,00

    Envío por EUR 23,00 
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    Cantidad disponible: 1 disponibles

    Taschenbuch. 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

    Editorial: LAP LAMBERT Academic Publishing, 2010

    3838317777 / 9783838317779

    • Tapa blanda
    • Impresión bajo demanda

    Librería: moluna, Greven, Alemaniamoluna

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    Condición: Nuevo

    EUR 55,21

    Envío por EUR 48,99 
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    Cantidad disponible: Más de 20 disponibles

    Condición: 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

    Editorial: LAP Lambert Academic Publishing, 2009

    3838321537 / 9783838321530

    • Tapa blanda
    • Impresión bajo demanda

    Librería: moluna, Greven, Alemaniamoluna

    Vendedor de 5 estrellas
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    Condición: Nuevo

    EUR 63,42

    Envío por EUR 48,99 
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    Cantidad disponible: Más de 20 disponibles

    Condición: 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

    Editorial: LAP LAMBERT Academic Publishing Mai 2010, 2010

    3838317777 / 9783838317779

    • Tapa blanda
    • Impresión bajo demanda

    Librería: buchversandmimpf2000, Emtmannsberg, BAYE, Alemaniabuchversandmimpf2000

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    Condición: Nuevo

    EUR 68,00

    Envío por EUR 60,00 
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    Cantidad disponible: 1 disponibles

    Taschenbuch. 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

    Editorial: LAP LAMBERT Academic Publishing, 2009

    3838317777 / 9783838317779

    • Tapa blanda
    • Impresión bajo demanda

    Librería: AHA-BUCH GmbH, Einbeck, AlemaniaAHA-BUCH GmbH

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    Condición: Nuevo

    EUR 68,00

    Envío por EUR 61,43 
    Se envía de Alemania a Estados Unidos de America

    Cantidad disponible: 1 disponibles

    Taschenbuch. 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

    Editorial: LAP LAMBERT Academic Publishing Okt 2009, 2009

    3838321537 / 9783838321530

    • Tapa blanda
    • Impresión bajo demanda

    Librería: buchversandmimpf2000, Emtmannsberg, BAYE, Alemaniabuchversandmimpf2000

    Vendedor de 5 estrellas
    Contactar con el vendedor

    Condición: Nuevo

    EUR 79,00

    Envío por EUR 60,00 
    Se envía de Alemania a Estados Unidos de America

    Cantidad disponible: 1 disponibles

    Taschenbuch. 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

    Editorial: LAP LAMBERT Academic Publishing, 2010

    3838321537 / 9783838321530

    • Tapa blanda
    • Impresión bajo demanda

    Librería: AHA-BUCH GmbH, Einbeck, AlemaniaAHA-BUCH GmbH

    Vendedor de 5 estrellas
    Contactar con el vendedor

    Condición: Nuevo

    EUR 79,00

    Envío por EUR 62,00 
    Se envía de Alemania a Estados Unidos de America

    Cantidad disponible: 1 disponibles

    Taschenbuch. 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.