Summary Of Flow Modulation And Fluid Structure Interaction Findings


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Summary of Flow Modulation and Fluid-Structure Interaction Findings


Summary of Flow Modulation and Fluid-Structure Interaction Findings

Author: Wolfgang Schröder

language: en

Publisher: Springer Science & Business Media

Release Date: 2010-05-16


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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 at RWTH Aachen University which was funded by the Deutsche Forschungsgemeinschaft (DFG) from 1997 through 2008. The research program covered the following three main topics of large transport aircraft: (i) Model flow, wakes, and vortices of airplanes in high-lift-configuration, (ii) Numerical tools for large scale adaptive flow simulation based on multiscale analysis and a parametric mapping concept for grid generation, and (iii) Validated computational design tools based on direct aeroelastic simulation with reduced structural models.

Summary of Flow Modulation and Fluid-Structure Interaction Findings


Summary of Flow Modulation and Fluid-Structure Interaction Findings

Author: Wolfgang Schr©œder

language: en

Publisher:

Release Date: 2010


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ADIGMA – A European Initiative on the Development of Adaptive Higher-Order Variational Methods for Aerospace Applications


ADIGMA – A European Initiative on the Development of Adaptive Higher-Order Variational Methods for Aerospace Applications

Author: Norbert Kroll

language: en

Publisher: Springer Science & Business Media

Release Date: 2010-09-18


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This volume contains results gained from the EU-funded 6th Framework project ADIGMA (Adaptive Higher-order Variational Methods for Aerodynamic Applications in Industry). The goal of ADIGMA was the development and utilization of innovative adaptive higher-order methods for the compressible flow equations enabling reliable, mesh independent numerical solutions for large-scale aerodynamic applications in aircraft industry. The ADIGMA consortium was comprised of 22 organizations which included the main European aircraft manufacturers, the major European research establishments and several universities, all with well proven expertise in Computational Fluid Dynamics (CFD). The book presents an introduction to the project, exhibits partners’ methods and approaches and provides a critical assessment of the newly developed methods for industrial aerodynamic applications. The best numerical strategies for integration as major building blocks for the next generation of industrial flow solvers are identified.