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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| Format: | Electronic |
| Language: | English |
| Published: |
Berlin, Heidelberg :
Springer Berlin Heidelberg,
2010.
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| Series: | Notes on Numerical Fluid Mechanics and Multidisciplinary Design,
109 |
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| Online Access: | https://ezaccess.library.uitm.edu.my/login?url=http://dx.doi.org/10.1007/978-3-642-04088-7 |
Table of Contents:
- 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 <U+0013> Structure <U+0013> 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.