Selmin vittorio (22 resultados)
Idioma: Inglés
Editorial: Springer, 2010
Serie: Libro 10 de 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Librería: Ria Christie Collections, Uxbridge, Reino UnidoRia Christie Collections
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Condición: New. In.
Idioma: Inglés
Editorial: Springer, 2002
Serie: Libro 10 de 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Librería: Ria Christie Collections, Uxbridge, Reino UnidoRia Christie Collections
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Condición: New. In.
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Idioma: Inglés
Editorial: Springer Berlin Heidelberg, Springer Berlin Heidelberg, 2002
Serie: Libro 10 de 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Librería: AHA-BUCH GmbH, Einbeck, AlemaniaAHA-BUCH GmbH
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EUR 213,99
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Buch. Condición: Neu. Druck auf Anfrage Neuware - Printed after ordering - Aircraft design processes require extensive work in the area of both aerodynamics and structure, fonning an environment for aeroelasticity investigations. Present and future designs of European aircraft are characterized by an ever increasing aircraft siz…e and perfonnance. Strong weight saving requirements are met by introduction of new materials, leading to more flexible structure of the aircraft. Consequently, aeroelastic phenomena such as vortex-induced aeroelastic oscillations and moving shock waves can be predominant and may have a significant effect on the aircraft perfonnance. Hence, the ability to estimate reliable margins for aeroelastic instabilities (flutter) or dynamic loads (buffeting) is a major concern to the aircraft designer. As modern aircrafts have wing bending modes with frequencies that are low enough to influence the flight control system, demands on unsteady aerodynamics and structural analysis to predict flight control effectiveness and riding comfort for passengers are extremely high. Therefore, the aircraft industries need an improved capacity of robust, accurate and reliable prediction methods in the coupled aeroelastic, flight mechanics and loads disciplines. In particular, it is necessary to develop/improve and calibrate the numerical tools in order to predict with high level of accuracy and capability complex and non-classical aeroelastic phenomena, including aerodynamic non-linearities, such as shock waves and separation, as well as structural non-linearities, e. g. control surface free-play. Nowadays, robust methods for structural analysis and linearised unsteady aerodynamics are coupled and used by the aircraft industry to computationally clear a new design from flutter.
Idioma: Inglés
Editorial: J.B. Metzler, 2010
Serie: Libro 10 de 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Librería: Buchpark, Trebbin, AlemaniaBuchpark
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EUR 171,66
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Condición: Sehr gut. Zustand: Sehr gut | Seiten: 384 | Sprache: Englisch | Produktart: Bücher | Aircraft design processes require extensive work in the area of both aerodynamics and structure, fonning an environment for aeroelasticity investigations. Present and future designs of European aircraft are characterized by an ever in…creasing aircraft size and perfonnance. Strong weight saving requirements are met by introduction of new materials, leading to more flexible structure of the aircraft. Consequently, aeroelastic phenomena such as vortex-induced aeroelastic oscillations and moving shock waves can be predominant and may have a significant effect on the aircraft perfonnance. Hence, the ability to estimate reliable margins for aeroelastic instabilities (flutter) or dynamic loads (buffeting) is a major concern to the aircraft designer. As modern aircrafts have wing bending modes with frequencies that are low enough to influence the flight control system, demands on unsteady aerodynamics and structural analysis to predict flight control effectiveness and riding comfort for passengers are extremely high. Therefore, the aircraft industries need an improved capacity of robust, accurate and reliable prediction methods in the coupled aeroelastic, flight mechanics and loads disciplines. In particular, it is necessary to develop/improve and calibrate the numerical tools in order to predict with high level of accuracy and capability complex and non-classical aeroelastic phenomena, including aerodynamic non-linearities, such as shock waves and separation, as well as structural non-linearities, e. g. control surface free-play. Nowadays, robust methods for structural analysis and linearised unsteady aerodynamics are coupled and used by the aircraft industry to computationally clear a new design from flutter.
Idioma: Inglés
Editorial: Springer, 2010
Serie: Libro 10 de 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Librería: Books Puddle, New York, NY, Estados Unidos de AmericaBooks Puddle
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EUR 281,32
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Condición: New. pp. 384.
Idioma: Inglés
Editorial: Springer, 2002
Serie: Libro 10 de 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Librería: Books Puddle, New York, NY, Estados Unidos de AmericaBooks Puddle
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EUR 282,32
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Condición: New. pp. 388.
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Idioma: Inglés
Editorial: Springer, 2010
Serie: Libro 10 de 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Librería: AHA-BUCH GmbH, Einbeck, AlemaniaAHA-BUCH GmbH
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EUR 223,11
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Taschenbuch. Condición: Neu. Druck auf Anfrage Neuware - Printed after ordering - Aircraft design processes require extensive work in the area of both aerodynamics and structure, fonning an environment for aeroelasticity investigations. Present and future designs of European aircraft are characterized by an ever increasing aircr…aft size and perfonnance. Strong weight saving requirements are met by introduction of new materials, leading to more flexible structure of the aircraft. Consequently, aeroelastic phenomena such as vortex-induced aeroelastic oscillations and moving shock waves can be predominant and may have a significant effect on the aircraft perfonnance. Hence, the ability to estimate reliable margins for aeroelastic instabilities (flutter) or dynamic loads (buffeting) is a major concern to the aircraft designer. As modern aircrafts have wing bending modes with frequencies that are low enough to influence the flight control system, demands on unsteady aerodynamics and structural analysis to predict flight control effectiveness and riding comfort for passengers are extremely high. Therefore, the aircraft industries need an improved capacity of robust, accurate and reliable prediction methods in the coupled aeroelastic, flight mechanics and loads disciplines. In particular, it is necessary to develop/improve and calibrate the numerical tools in order to predict with high level of accuracy and capability complex and non-classical aeroelastic phenomena, including aerodynamic non-linearities, such as shock waves and separation, as well as structural non-linearities, e. g. control surface free-play. Nowadays, robust methods for structural analysis and linearised unsteady aerodynamics are coupled and used by the aircraft industry to computationally clear a new design from flutter.
Idioma: Inglés
Editorial: Springer, 2010
Serie: Libro 10 de 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Librería: Mispah books, Redhill, SURRE, Reino UnidoMispah books
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Paperback. Condición: Like New. LIKE NEW. SHIPS FROM MULTIPLE LOCATIONS. book.
Idioma: Inglés
Editorial: Springer, 2010
Serie: Libro 10 de 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Librería: Basi6 International, Irving, TX, Estados Unidos de AmericaBasi6 International
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EUR 176,84
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Condición: Brand New. New. US edition. Print on demand title. Delivery takes 20-25 days. Excellent Customer Service.
Idioma: Inglés
Editorial: Springer, 2002
Serie: Libro 10 de 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Librería: Basi6 International, Irving, TX, Estados Unidos de AmericaBasi6 International
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EUR 176,84
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Condición: Brand New. New. US edition. Print on demand title. Delivery takes 20-25 days. Excellent Customer Service.
Idioma: Inglés
Editorial: Springer, 2010
Serie: Libro 10 de 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Librería: Brook Bookstore On Demand, Napoli, NA, ItaliaBrook Bookstore On Demand
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Condición: new. Questo è un articolo print on demand.
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Idioma: Inglés
Editorial: Springer Berlin Heidelberg, 2010
Serie: Libro 10 de 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Librería: moluna, Greven, Alemaniamoluna
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EUR 180,07
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Condición: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. State of the art in computational fluid dynamics and nonlinear aeroelasticityAircraft design processes require extensive work in the area of both aerodynamics and structure, fonning an environment for aeroelasticity i…nvestigations. Present and future de.
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Idioma: Inglés
Editorial: Springer Berlin Heidelberg, 2002
Serie: Libro 10 de 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Librería: moluna, Greven, Alemaniamoluna
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EUR 180,07
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Condición: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. State of the art in computational fluid dynamics and nonlinear aeroelasticityState of the art in computational fluid dynamics and nonlinear aeroelasticityIncludes supplementary material: sn.pub/extrasAircraft design p…rocesses require e.
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Idioma: Inglés
Editorial: Springer Berlin Heidelberg Nov 2002, 2002
Serie: Libro 10 de 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Librería: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, AlemaniaBuchWeltWeit Ludwig Meier e.K.
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EUR 213,99
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Buch. Condición: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -Aircraft design processes require extensive work in the area of both aerodynamics and structure, fonning an environment for aeroelasticity investigations. Present and future designs of European aircraft are characterized by an ever increas…ing aircraft size and perfonnance. Strong weight saving requirements are met by introduction of new materials, leading to more flexible structure of the aircraft. Consequently, aeroelastic phenomena such as vortex-induced aeroelastic oscillations and moving shock waves can be predominant and may have a significant effect on the aircraft perfonnance. Hence, the ability to estimate reliable margins for aeroelastic instabilities (flutter) or dynamic loads (buffeting) is a major concern to the aircraft designer. As modern aircrafts have wing bending modes with frequencies that are low enough to influence the flight control system, demands on unsteady aerodynamics and structural analysis to predict flight control effectiveness and riding comfort for passengers are extremely high. Therefore, the aircraft industries need an improved capacity of robust, accurate and reliable prediction methods in the coupled aeroelastic, flight mechanics and loads disciplines. In particular, it is necessary to develop/improve and calibrate the numerical tools in order to predict with high level of accuracy and capability complex and non-classical aeroelastic phenomena, including aerodynamic non-linearities, such as shock waves and separation, as well as structural non-linearities, e. g. control surface free-play. Nowadays, robust methods for structural analysis and linearised unsteady aerodynamics are coupled and used by the aircraft industry to computationally clear a new design from flutter. 388 pp. Englisch.
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Idioma: Inglés
Editorial: Springer, 2002
Serie: Libro 10 de 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Librería: preigu, Osnabrück, Alemaniapreigu
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EUR 186,70
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Buch. Condición: Neu. Progress in Computational Flow-Structure Interaction | Results of the Project UNSI, supported by the European Union 1998 - 2000 | Werner Haase (u. a.) | Buch | Notes on Numerical Fluid Mechanics and Multidisciplinary Design | x | Englisch | 2002 | Springer | EAN 9783540439028 | Verantwortliche Person für di…e EU: Springer Verlag GmbH, Tiergartenstr. 17, 69121 Heidelberg, juergen[dot]hartmann[at]springer[dot]com | Anbieter: preigu Print on Demand.
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Idioma: Inglés
Editorial: Springer Berlin Heidelberg, Springer Nov 2002, 2002
Serie: Libro 10 de 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Librería: buchversandmimpf2000, Emtmannsberg, BAYE, Alemaniabuchversandmimpf2000
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EUR 213,99
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Buch. Condición: Neu. This item is printed on demand - Print on Demand Titel. Neuware -Aircraft design processes require extensive work in the area of both aerodynamics and structure, fonning an environment for aeroelasticity investigations. Present and future designs of European aircraft are characterized by an ever increasing…aircraft size and perfonnance. Strong weight saving requirements are met by introduction of new materials, leading to more flexible structure of the aircraft. Consequently, aeroelastic phenomena such as vortex-induced aeroelastic oscillations and moving shock waves can be predominant and may have a significant effect on the aircraft perfonnance. Hence, the ability to estimate reliable margins for aeroelastic instabilities (flutter) or dynamic loads (buffeting) is a major concern to the aircraft designer. As modern aircrafts have wing bending modes with frequencies that are low enough to influence the flight control system, demands on unsteady aerodynamics and structural analysis to predict flight control effectiveness and riding comfort for passengers are extremely high. Therefore, the aircraft industries need an improved capacity of robust, accurate and reliable prediction methods in the coupled aeroelastic, flight mechanics and loads disciplines. In particular, it is necessary to develop/improve and calibrate the numerical tools in order to predict with high level of accuracy and capability complex and non-classical aeroelastic phenomena, including aerodynamic non-linearities, such as shock waves and separation, as well as structural non-linearities, e. g. control surface free-play. Nowadays, robust methods for structural analysis and linearised unsteady aerodynamics are coupled and used by the aircraft industry to computationally clear a new design from flutter.Springer-Verlag GmbH, Tiergartenstr. 17, 69121 Heidelberg 388 pp. Englisch.
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Idioma: Inglés
Editorial: Springer Berlin Heidelberg, Springer Berlin Heidelberg Dez 2010, 2010
Serie: Libro 10 de 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Librería: buchversandmimpf2000, Emtmannsberg, BAYE, Alemaniabuchversandmimpf2000
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EUR 213,99
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Taschenbuch. Condición: Neu. This item is printed on demand - Print on Demand Titel. Neuware -Aircraft design processes require extensive work in the area of both aerodynamics and structure, fonning an environment for aeroelasticity investigations. Present and future designs of European aircraft are characterized by an ever incr…easing aircraft size and perfonnance. Strong weight saving requirements are met by introduction of new materials, leading to more flexible structure of the aircraft. Consequently, aeroelastic phenomena such as vortex-induced aeroelastic oscillations and moving shock waves can be predominant and may have a significant effect on the aircraft perfonnance. Hence, the ability to estimate reliable margins for aeroelastic instabilities (flutter) or dynamic loads (buffeting) is a major concern to the aircraft designer. As modern aircrafts have wing bending modes with frequencies that are low enough to influence the flight control system, demands on unsteady aerodynamics and structural analysis to predict flight control effectiveness and riding comfort for passengers are extremely high. Therefore, the aircraft industries need an improved capacity of robust, accurate and reliable prediction methods in the coupled aeroelastic, flight mechanics and loads disciplines. In particular, it is necessary to develop/improve and calibrate the numerical tools in order to predict with high level of accuracy and capability complex and non-classical aeroelastic phenomena, including aerodynamic non-linearities, such as shock waves and separation, as well as structural non-linearities, e. g. control surface free-play. Nowadays, robust methods for structural analysis and linearised unsteady aerodynamics are coupled and used by the aircraft industry to computationally clear a new design from flutter.Springer Verlag GmbH, Tiergartenstr. 17, 69121 Heidelberg 384 pp. Englisch.
Idioma: Inglés
Editorial: Springer, 2010
Serie: Libro 10 de 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Librería: Majestic Books, Hounslow, Reino UnidoMajestic Books
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EUR 296,42
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Condición: New. Print on Demand pp. 384 49:B&W 6.14 x 9.21 in or 234 x 156 mm (Royal 8vo) Perfect Bound on White w/Gloss Lam.
Idioma: Inglés
Editorial: Springer, 2002
Serie: Libro 10 de 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Librería: Majestic Books, Hounslow, Reino UnidoMajestic Books
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EUR 297,55
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Condición: New. Print on Demand pp. 388 Illus.
Idioma: Inglés
Editorial: Springer, 2002
Serie: Libro 10 de 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Librería: Biblios, frankfurt am main, HESSE, AlemaniaBiblios
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EUR 300,63
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Condición: New. PRINT ON DEMAND pp. 388.
Idioma: Inglés
Editorial: Springer, 2010
Serie: Libro 10 de 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Librería: Biblios, frankfurt am main, HESSE, AlemaniaBiblios
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EUR 300,75
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Condición: New. PRINT ON DEMAND pp. 384.
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Idioma: Inglés
Editorial: Springer Berlin Heidelberg Dez 2010, 2010
Serie: Libro 10 de 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Librería: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, AlemaniaBuchWeltWeit Ludwig Meier e.K.
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EUR 309,23
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Taschenbuch. Condición: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -Aircraft design processes require extensive work in the area of both aerodynamics and structure, fonning an environment for aeroelasticity investigations. Present and future designs of European aircraft are characterized by an ever…increasing aircraft size and perfonnance. Strong weight saving requirements are met by introduction of new materials, leading to more flexible structure of the aircraft. Consequently, aeroelastic phenomena such as vortex-induced aeroelastic oscillations and moving shock waves can be predominant and may have a significant effect on the aircraft perfonnance. Hence, the ability to estimate reliable margins for aeroelastic instabilities (flutter) or dynamic loads (buffeting) is a major concern to the aircraft designer. As modern aircrafts have wing bending modes with frequencies that are low enough to influence the flight control system, demands on unsteady aerodynamics and structural analysis to predict flight control effectiveness and riding comfort for passengers are extremely high. Therefore, the aircraft industries need an improved capacity of robust, accurate and reliable prediction methods in the coupled aeroelastic, flight mechanics and loads disciplines. In particular, it is necessary to develop/improve and calibrate the numerical tools in order to predict with high level of accuracy and capability complex and non-classical aeroelastic phenomena, including aerodynamic non-linearities, such as shock waves and separation, as well as structural non-linearities, e. g. control surface free-play. Nowadays, robust methods for structural analysis and linearised unsteady aerodynamics are coupled and used by the aircraft industry to computationally clear a new design from flutter. 384 pp. Englisch.
