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Progress in Computational Flow-Structure Interaction - Results of the Project UNSI, supported by the European Union 1998 - 2000 (Paperback, Softcover reprint of the original 1st ed. 2003) Loot Price: R5,786
Discovery Miles 57 860
Progress in Computational Flow-Structure Interaction - Results of the Project UNSI, supported by the European Union 1998 - 2000...

Progress in Computational Flow-Structure Interaction - Results of the Project UNSI, supported by the European Union 1998 - 2000 (Paperback, Softcover reprint of the original 1st ed. 2003)

Werner Haase, Vittorio Selmin, Bengt Winzell

Series: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 81

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Loot Price R5,786 Discovery Miles 57 860 | Repayment Terms: R542 pm x 12*

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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.

General

Imprint: Springer-Verlag
Country of origin: Germany
Series: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 81
Release date: December 2010
First published: 2003
Editors: Werner Haase • Vittorio Selmin • Bengt Winzell
Dimensions: 235 x 155 x 20mm (L x W x T)
Format: Paperback
Pages: 374
Edition: Softcover reprint of the original 1st ed. 2003
ISBN-13: 978-3-642-07868-2
Categories: Books > Science & Mathematics > Mathematics > Applied mathematics > Mathematics for scientists & engineers
Books > Science & Mathematics > Physics > Classical mechanics > General
Books > Professional & Technical > Transport technology > Automotive technology > General
Books > Professional & Technical > Mechanical engineering & materials > Materials science > Mechanics of fluids > General
LSN: 3-642-07868-0
Barcode: 9783642078682

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