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 /

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 /

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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...

Πλήρης περιγραφή

Λεπτομέρειες βιβλιογραφικής εγγραφής
Συγγραφή απο Οργανισμό/Αρχή: SpringerLink (Online service)
Άλλοι συγγραφείς: Schröder, Wolfgang (Επιμελητής έκδοσης)
Μορφή: Ηλεκτρονική πηγή Ηλ. βιβλίο
Γλώσσα:English
Έκδοση: Berlin, Heidelberg : Springer Berlin Heidelberg, 2010.
Σειρά:Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 109
Θέματα:
Engineering.
Physics.
Continuum physics.
Fluids.
Applied mathematics.
Engineering mathematics.
Fluid mechanics.
Aerospace engineering.
Astronautics.
Aerospace Technology and Astronautics.
Classical Continuum Physics.
Engineering Fluid Dynamics.
Appl.Mathematics/Computational Methods of Engineering.
Fluid- and Aerodynamics.
Numerical and Computational Physics.
Διαθέσιμο Online:Full Text via HEAL-Link
Πίνακας περιεχομένων:
  • 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.

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