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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 /

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...

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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor Corporativo: SpringerLink (Online service)
Otros Autores: Schröder, Wolfgang (Editor )
Formato: Electrónico eBook
Idioma:Inglés
Publicado: Berlin, Heidelberg : Springer Berlin Heidelberg : Imprint: Springer, 2010.
Edición:1st ed. 2010.
Colección:Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 109
Temas:
Acceso en línea:Texto Completo
Tabla de Contenidos:
  • 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.