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Progress in Computational Flow-structure Interaction
. Ed(S): Haase, Werner; Selmin, Vittorio; Winzell, Bengt
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Description for Progress in Computational Flow-structure Interaction
Hardback. Contains results gained from the EU-funded 4th Framework project, UNSI (Unsteady Viscous Flows in the Context of Fluid-Structure Interaction). Fifteen European organizations (industrial firms, research labs and universities) collaborate on non-linear, static and dynamic aeroelasticity applications. Editor(s): Haase, Werner; Selmin, Vittorio; Winzell, Bengt. Series: Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Num Pages: 384 pages, biography. BIC Classification: TGMF. Category: (P) Professional & Vocational; (UP) Postgraduate, Research & Scholarly; (UU) Undergraduate. Dimension: 156 x 234 x 22. Weight in Grams: 719.
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 ... Read more
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 ... Read more
Product Details
Format
Hardback
Publication date
2002
Publisher
Springer-Verlag Berlin and Heidelberg GmbH & Co. KG Germany
Number of pages
384
Condition
New
Series
Notes on Numerical Fluid Mechanics and Multidisciplinary Design
Number of Pages
374
Place of Publication
Berlin, Germany
ISBN
9783540439028
SKU
V9783540439028
Shipping Time
Usually ships in 15 to 20 working days
Ref
99-15
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