Progress in Computational Flow-Structure Interaction

Language: English

Published by Springer Berlin Heidelberg Nov 2002, 2002

3540439021 / 9783540439028

Series: Book 10 of 30 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design

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Seller: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, GermanyBuchWeltWeit Ludwig Meier e.K.

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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. 388 pp. Englisch.

Seller Inventory # 9783540439028

Title
Progress in Computational Flow-Structure Interaction
Author
Werner Haase
Publisher
Springer Berlin Heidelberg Nov 2002
Publication year
2002
Condition
Neu
Binding
Buch
Language
English
ISBN 10
3540439021
ISBN 13
9783540439028
Item weight
746 grams
Dimensions
241x160x26 mm
Series
Book 10 of 30: Notes on Numerical Fluid Mechanics and Multidisciplinary Design

BuchWeltWeit Ludwig Meier e.K.

Bergisch Gladbach, Germany

5-star seller

AbeBooks seller since January 11, 2012

Shipping rates from Germany to U.S.A.

Item5 to 15 business days5 to 15 business days
First itemUS$ 26.74US$ 26.74
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BuchWeltWeit Ludwig Meier e.K.

Germany