Articles liés à Progress in Computational Flow-Structure Interaction:...
Progress in Computational Flow-Structure Interaction: Results of the Project UNSI, supported by the European Union 1998 – 2000 - Couverture souple
- ÉditeurSpringer
- Date d'édition2010
- ISBN 10 3642078680
- ISBN 13 9783642078682
- ReliureBroché
- Langueanglais
- Nombre de pages384
- ÉditeurHaase Werner, Selmin Vittorio, Winzell Bengt
Acheter neuf
Afficher cet article
EUR 213,72
EUR 3,60 expédition vers Etats-Unis
Destinations, frais et délaisAutres éditions populaires du même titre
Résultats de recherche pour Progress in Computational Flow-Structure Interaction:...
Image d'archives
Progress in Computational Flow-Structure Interaction : Results of the Project UNSI, supported by the European Union 1998 ¿ 2000
Edité par
Springer Berlin Heidelberg, 2010
ISBN 10 : 3642078680
ISBN 13 : 9783642078682
Ancien ou d'occasion
Couverture souple
Vendeur : Buchpark, Trebbin, Allemagne
Évaluation du vendeur 5 sur 5 étoiles
Etat : Sehr gut. Zustand: Sehr gut - Gepflegter, sauberer Zustand. | Seiten: 384 | Sprache: Englisch | Produktart: Bücher. N° de réf. du vendeur 10449266/2
Quantité disponible : 1 disponible(s)
Image d'archives
Progress in Computational Flow-Structure Interaction: Results of the Project UNSI, supported by the European Union 1998 - 2000 (Notes on Numerical Fluid Mechanics and Multidisciplinary Design)
Vendeur : Lucky's Textbooks, Dallas, TX, Etats-Unis
Évaluation du vendeur 5 sur 5 étoiles
Etat : New. N° de réf. du vendeur ABLIING23Mar3113020216632
Quantité disponible : Plus de 20 disponibles
Image fournie par le vendeur
Progress in Computational Flow-Structure Interaction
Edité par
Springer Berlin Heidelberg, 2010
ISBN 10 : 3642078680
ISBN 13 : 9783642078682
Neuf
Couverture souple
Vendeur : moluna, Greven, Allemagne
Évaluation du vendeur 5 sur 5 étoiles
Etat : 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. N° de réf. du vendeur 5046923
Quantité disponible : Plus de 20 disponibles
Image fournie par le vendeur
Progress in Computational Flow-Structure Interaction : Results of the Project UNSI, supported by the European Union 1998 ¿ 2000
Edité par
Springer Berlin Heidelberg, 2010
ISBN 10 : 3642078680
ISBN 13 : 9783642078682
Neuf
Taschenbuch
Vendeur : AHA-BUCH GmbH, Einbeck, Allemagne
Évaluation du vendeur 5 sur 5 étoiles
Taschenbuch. Etat : 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 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. N° de réf. du vendeur 9783642078682
Quantité disponible : 1 disponible(s)
Image d'archives
Progress in Computational Flow-Structure Interaction: Results of the Project UNSI, supported by the European Union 1998 - 2000 (Notes on Numerical Fluid Mechanics and Multidisciplinary Design)
Vendeur : Ria Christie Collections, Uxbridge, Royaume-Uni
Évaluation du vendeur 5 sur 5 étoiles
Etat : New. In. N° de réf. du vendeur ria9783642078682_new
Quantité disponible : Plus de 20 disponibles
Image d'archives
Progress in Computational Flow-Structure Interaction: Results of the Project UNSI, supported by the European Union 1998 - 2000 (Notes on Numerical Fluid Mechanics and Multidisciplinary Design)
Vendeur : California Books, Miami, FL, Etats-Unis
Évaluation du vendeur 5 sur 5 étoiles
Etat : New. N° de réf. du vendeur I-9783642078682
Quantité disponible : Plus de 20 disponibles
Image fournie par le vendeur
Progress in Computational Flow-Structure Interaction
Edité par
Springer Berlin Heidelberg Dez 2010, 2010
ISBN 10 : 3642078680
ISBN 13 : 9783642078682
Neuf
Taschenbuch
Vendeur : BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Allemagne
Évaluation du vendeur 5 sur 5 étoiles
Taschenbuch. Etat : 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. N° de réf. du vendeur 9783642078682
Quantité disponible : 2 disponible(s)
Image d'archives
Progress in Computational Flow-Structure Interaction
Vendeur : Biblios, Frankfurt am main, HESSE, Allemagne
Évaluation du vendeur 5 sur 5 étoiles
Etat : New. N° de réf. du vendeur 182459463
Quantité disponible : 4 disponible(s)
Image d'archives
Progress in Computational Flow-Structure Interaction
impression à la demandeVendeur : Majestic Books, Hounslow, Royaume-Uni
Évaluation du vendeur 5 sur 5 étoiles
Etat : 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. N° de réf. du vendeur 5388434
Quantité disponible : 4 disponible(s)
Image d'archives
Progress in Computational Flow-Structure Interaction: Results of the Project UNSI, supported by the European Union 1998 2000 (Notes on Numerical Fluid Mechanics and Multidisciplinary Design (81))
Edité par
Springer, 2010
ISBN 10 : 3642078680
ISBN 13 : 9783642078682
Ancien ou d'occasion
Paperback
Vendeur : Mispah books, Redhill, SURRE, Royaume-Uni
Évaluation du vendeur 4 sur 5 étoiles
Paperback. Etat : Like New. Like New. book. N° de réf. du vendeur ERICA79736420786806
Quantité disponible : 1 disponible(s)