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
(Sprache: Englisch)
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...
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Klappentext zu „Summary of Flow Modulation and Fluid-Structure Interaction Findings “
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.
Inhaltsverzeichnis zu „Summary of Flow Modulation and Fluid-Structure Interaction Findings “
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.
Autoren-Porträt
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.
Bibliographische Angaben
- 2013, 420 Seiten, Masse: 15,5 x 23,5 cm, Kartoniert (TB), Englisch
- Herausgegeben: Wolfgang Schröder
- Verlag: Springer, Berlin
- ISBN-10: 3642263720
- ISBN-13: 9783642263729
Sprache:
Englisch
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