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008 100515s2010 gw | s |||| 0|eng d
020 _a9783642040887
_9978-3-642-04088-7
040 _cMX-MeUAM
050 4 _aTA357-359
082 0 4 _a620.1064
_223
100 1 _aSchröder, Wolfgang.
_eeditor.
245 1 0 _aSummary of Flow Modulation and Fluid-Structure Interaction Findings
_h[recurso electrónico] :
_bResults of the Collaborative Research Center SFB 401 at the RWTH Aachen University, Aachen, Germany, 1997-2008 /
_cedited by Wolfgang Schröder.
264 1 _aBerlin, Heidelberg :
_bSpringer Berlin Heidelberg,
_c2010.
300 _a420p. 294 illus.
_bonline resource.
336 _atext
_btxt
_2rdacontent
337 _acomputer
_bc
_2rdamedia
338 _aonline resource
_bcr
_2rdacarrier
347 _atext file
_bPDF
_2rda
490 1 _aNotes on Numerical Fluid Mechanics and Multidisciplinary Design,
_x1612-2909 ;
_v109
505 0 _aVortex Sheets of Aircraft in Takeoff and Landing -- An Adaptive Implicit Finite Volume Scheme for Compressible Turbulent Flows about Elastic Configurations -- Timestep Control for Weakly Instationary Flows -- Adaptive Multiscale Methods for Flow Problems: Recent Developments -- Interaction of Wing-Tip Vortices and Jets in the Extended Wake -- Experimental and Numerical Investigation of Unsteady Transonic Airfoil Flow -- Enabling Technologies for Robust High-Performance Simulations in Computational Fluid Dynamics -- Influencing Aircraft Wing Vortices -- Development of a Modular Method for Computational Aero-structural Analysis of Aircraft -- A Unified Approach to the Modeling of Airplane Wings and Numerical Grid Generation Using B-Spline Representations -- Parallel and Adaptive Methods for Fluid-Structure-Interactions -- Iterative Solvers for Discretized Stationary Euler Equations -- Unsteady Transonic Fluid - Structure - Interaction at the BAC 3-11 High Aspect Ratio Swept Wing -- Structural Idealization of Flexible Generic Wings in Computational Aeroelasticity -- Aero-structural Dynamics Experiments at High Reynolds Numbers.
520 _aThe Collaborative Research Center SFB 401: Flow Modulation and Fluid-Structure Interaction at Airplane Wings investigates numerically and experimentally fundamental problems of very high capacity aircraft having large elastic wings. This issue summarizes the findings of the 12-year research program at RWTH Aachen University which was funded by the Deutsche Forschungsgemeinschaft (DFG) from 1997 through 2008. The research program covered the following three main topics of large transport aircraft: (i) Model flow, wakes, and vortices of airplanes in high-lift-configuration, (ii) Numerical tools for large scale adaptive flow simulation based on multiscale analysis and a parametric mapping concept for grid generation, and (iii) Validated computational design tools based on direct aeroelastic simulation with reduced structural models.
650 0 _aEngineering.
650 0 _aEngineering mathematics.
650 0 _aVibration.
650 0 _aHydraulic engineering.
650 1 4 _aEngineering.
650 2 4 _aEngineering Fluid Dynamics.
650 2 4 _aAppl.Mathematics/Computational Methods of Engineering.
650 2 4 _aFluid- and Aerodynamics.
650 2 4 _aNumerical and Computational Physics.
650 2 4 _aVibration, Dynamical Systems, Control.
710 2 _aSpringerLink (Online service)
773 0 _tSpringer eBooks
776 0 8 _iPrinted edition:
_z9783642040870
830 0 _aNotes on Numerical Fluid Mechanics and Multidisciplinary Design,
_x1612-2909 ;
_v109
856 4 0 _zLibro electrónico
_uhttp://148.231.10.114:2048/login?url=http://link.springer.com/book/10.1007/978-3-642-04088-7
596 _a19
942 _cLIBRO_ELEC
999 _c201499
_d201499