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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: R5,454
Discovery Miles 54 540
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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)
Series: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 81
Expected to ship within 10 - 15 working days
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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.
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