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...
Sábháilte in:
| Rannpháirtithe: | |
|---|---|
| Formáid: | Livre numérique |
| Teanga: | Anglais |
| Foilsithe / Cruthaithe: |
Berlin, Heidelberg :
Springer Berlin Heidelberg
[20..].
Cham : Springer Nature |
| Eagrán: | 1st ed. 2010. |
| Sraith: | Notes on Numerical Fluid Mechanics and Multidisciplinary Design
109 |
| Rochtain ar líne: | Accès sur la plateforme de l'éditeur Accès sur la plateforme Istex Accès Université d'Orléans Accès INSA CVL |
| Nóta: |
Archives Springer e-books (Licence nationale) Archives Springer e-books (Licence nationale) |
| Autres localisations: | Voir dans le Sudoc |
| Edition sous un autre format: | • Summary of Flow Modulation and Fluid-Structure Interaction Findings, Texte imprimé, 9783642040962 • Summary of Flow Modulation and Fluid-Structure Interaction Findings, Texte imprimé, 9783642263729 • Summary of Flow Modulation and Fluid-Structure Interaction Findings, Texte imprimé, 9783642040870 • Summary of Flow Modulation and Fluid-Structure Interaction Findings, Texte imprimé, 9783642040962 • Summary of Flow Modulation and Fluid-Structure Interaction Findings, Texte imprimé, 9783642263729 • Summary of Flow Modulation and Fluid-Structure Interaction Findings, Texte imprimé, 9783642040870 |
Clár na nÁbhar:
- 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.