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100515s2010 gw | s |||| 0|eng d |
| 020 |
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|a 9783642040887
|9 978-3-642-04088-7
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|a 10.1007/978-3-642-04088-7
|2 doi
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|a TA357-359
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|a TEC009070
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|a SCI085000
|2 bisacsh
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|a 620.1064
|2 23
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|a Schrd̲er, Wolfgang.
|e editor.
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|a Summary of Flow Modulation and Fluid-Structure Interaction Findings
|b Results of the Collaborative Research Center SFB 401 at the RWTH Aachen University, Aachen, Germany, 1997-2008 /
|c edited by Wolfgang Schrd̲er.
|h [electronic resource] :
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| 264 |
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|a Berlin, Heidelberg :
|b Springer Berlin Heidelberg,
|c 2010.
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| 300 |
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|a 420p. 294 illus.
|b online resource.
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| 336 |
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|a text
|b txt
|2 rdacontent
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|a computer
|b c
|2 rdamedia
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|a online resource
|b cr
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|a text file
|b PDF
|2 rda
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|a Notes on Numerical Fluid Mechanics and Multidisciplinary Design,
|v 109
|x 1612-2909 ;
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|a Introduction -- Vortex Sheets of Aircraft in Takeoff and Landing -- An Adaptive Implicit Finite Volume Scheme for Compressible Turbulent Flows about Elastic Configurations -- Timestep Control forWeakly Instationary Flows.-Adaptive Multiscale Methods for Flow Problems: Recent Developments -- Interaction ofWing-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 AircraftWing 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 <U+0013> Structure <U+0013> 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.
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|a The 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.
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|a Engineering.
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|a Engineering mathematics.
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|a Vibration.
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|a Hydraulic engineering.
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|a Engineering.
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| 650 |
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|a Engineering Fluid Dynamics.
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| 650 |
2 |
4 |
|a Appl.Mathematics/Computational Methods of Engineering.
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| 650 |
2 |
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|a Fluid- and Aerodynamics.
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| 650 |
2 |
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|a Numerical and Computational Physics.
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| 650 |
2 |
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|a Vibration, Dynamical Systems, Control.
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| 710 |
2 |
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|a SpringerLink (Online service)
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|t Springer eBooks
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| 776 |
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8 |
|i Printed edition:
|z 9783642040870
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| 830 |
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|a Notes on Numerical Fluid Mechanics and Multidisciplinary Design,
|v 109
|x 1612-2909 ;
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| 856 |
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|u https://ezaccess.library.uitm.edu.my/login?url=http://dx.doi.org/10.1007/978-3-642-04088-7
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| 912 |
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|a ZDB-2-ENG
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| 950 |
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|a Engineering (Springer-11647)
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