Summary of Flow Modulation and Fluid-structure Interaction Findings: Results of the Collaborative Research Center Sfb 401 at the Rwth Aachen University, Aachen, Germany, 1997-2008

Schroder, Wolfgang (Editor)

ISBN 10: 3642263720 / ISBN 13: 9783642263729

Verlag: Springer Verlag, 2013

Beschreibung

2010 edition. 420 pages. 9.25x6.10x1.06 inches. In Stock.

Bestandsnummer des Verkäufers x-3642263720

Bibliografische Details

• Titel: Summary of Flow Modulation and Fluid-structure Interaction Findings: Results of the Collaborative Research Center Sfb 401 at the Rwth Aachen University, Aachen, Germany, 1997-2008
• Verlag: Springer Verlag
• Veröffentlichungsdatum: 2013
• Sprache: Englisch
• ISBN-10: 3642263720
• ISBN-13: 9783642263729
• Bindung: Paperback
• Zustand: Brand New

Über diesen Titel

Inhaltsangabe

Vortex 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.

Von der hinteren Coverseite

The Collaborative Research Center SFB 401: Flow Modulation and Fluid-StructureInteraction at Airplane Wings investigates numerically and experimentally fundamentalproblems of very high capacity aircraft having large elastic wings. This issue summarizesthe findings of the 12-year research program at RWTH Aachen University whichwas funded by the Deutsche Forschungsgemeinschaft (DFG) from 1997 through2008. The research program covered the following three main topics of large transportaircraft: (i) Model flow, wakes, and vortices of airplanes in high-lift-configuration,(ii) Numerical tools for large scale adaptive flow simulation based on multiscaleanalysis and a parametric mapping concept for grid generation, and (iii) Validatedcomputational design tools based on direct aeroelastic simulation with reducedstructural models.