Progress computational flow structure interaction (20 risultati)
Lingua: Inglese
Editore: Springer, 2002
Serie: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Libro 10 di 30. Libro 10 di 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Serie: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Libro 10 di 30. Libro 10 di 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Serie: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Libro 10 di 30. Libro 10 di 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Condizione: 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 i…ncreasing 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.
Lingua: Inglese
Editore: Springer Berlin Heidelberg, Springer Berlin Heidelberg, 2002
Serie: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Libro 10 di 30. Libro 10 di 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Da: AHA-BUCH GmbH, Einbeck, GermaniaAHA-BUCH GmbH
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Buch. Condizione: 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 si…ze 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.
Lingua: Inglese
Editore: Springer, 2010
Serie: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Libro 10 di 30. Libro 10 di 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Condizione: New. pp. 384.
Lingua: Inglese
Editore: Springer, 2002
Serie: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Libro 10 di 30. Libro 10 di 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Condizione: New. pp. 388.
Lingua: Inglese
Editore: Springer, 2010
Serie: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Libro 10 di 30. Libro 10 di 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Da: AHA-BUCH GmbH, Einbeck, GermaniaAHA-BUCH GmbH
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Taschenbuch. Condizione: 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 airc…raft 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.
Lingua: Inglese
Editore: Springer, 2010
Serie: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Libro 10 di 30. Libro 10 di 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Lingua: Inglese
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Serie: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Libro 10 di 30. Libro 10 di 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Lingua: Inglese
Editore: Springer Berlin Heidelberg, 2002
Serie: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Libro 10 di 30. Libro 10 di 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Condizione: 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…processes require e.
Lingua: Inglese
Editore: Springer Berlin Heidelberg, 2010
Serie: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Libro 10 di 30. Libro 10 di 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Condizione: 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…investigations. Present and future de.
Lingua: Inglese
Editore: Springer Berlin Heidelberg Nov 2002, 2002
Serie: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Libro 10 di 30. Libro 10 di 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Da: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, GermaniaBuchWeltWeit Ludwig Meier e.K.
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Buch. Condizione: 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 increa…sing 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.
Altre immaginiLingua: Inglese
Editore: Springer, 2002
Serie: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Libro 10 di 30. Libro 10 di 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Buch. Condizione: 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 d…ie EU: Springer Verlag GmbH, Tiergartenstr. 17, 69121 Heidelberg, juergen[dot]hartmann[at]springer[dot]com | Anbieter: preigu Print on Demand.
Lingua: Inglese
Editore: Springer Berlin Heidelberg, Springer Nov 2002, 2002
Serie: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Libro 10 di 30. Libro 10 di 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Buch. Condizione: 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.
Lingua: Inglese
Editore: Springer Berlin Heidelberg, Springer Berlin Heidelberg Dez 2010, 2010
Serie: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Libro 10 di 30. Libro 10 di 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Da: buchversandmimpf2000, Emtmannsberg, BAYE, Germaniabuchversandmimpf2000
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Taschenbuch. Condizione: 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 inc…reasing 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.
Lingua: Inglese
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Serie: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Libro 10 di 30. Libro 10 di 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Condizione: 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.
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Condizione: New. Print on Demand pp. 388 Illus.
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Condizione: New. PRINT ON DEMAND pp. 388.
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Condizione: New. PRINT ON DEMAND pp. 384.
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Da: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, GermaniaBuchWeltWeit Ludwig Meier e.K.
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Taschenbuch. Condizione: 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.
