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
Herausgegeben:Schröder, Wolfgang

• Broschiertes Buch

Produktbeschreibung

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.

Produktdetails

• Notes on Numerical Fluid Mechanics and Multidisciplinary Design 109
• Verlag: Springer / Springer Berlin Heidelberg / Springer, Berlin
• 2010
• Seitenzahl: 448
• Erscheinungstermin: 5. September 2012
• Englisch
• Abmessung: 235mm x 155mm x 25mm
• Gewicht: 675g
• ISBN-13: 9783642263729
• ISBN-10: 3642263720
• Artikelnr.: 36064773

Autorenporträt

Wolfgang Schröder ist Leitender Oberarzt an der Chirurgischen Universitätsklinik Köln. Er ist Mitglied im Präsidium des Berufsverbands der Chirurgen (BDC), leitet die Weiter- und Fortbildungsakademie des BDC.

Inhaltsangabe

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 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.