Flow Modulation and Fluid-Structure Interaction at Airplane Wings: Research Results of the Collaborative Research Center SFB 401 at RWTH Aachen, University of Technology, Aachen, Germany - Tapa blanda

Sinopsis

1 Introduction.- 2 Model Flow, Wakes and Vortices in High Lift Configuration.- 2.1 Experimental Analysis and Modulation of Vortices.- 2.2 Simulation of Vortex Sheets at Take-Off and Landing.- 2.3 Analysis of Wakes and Wake-Jet Interaction.- 2.4 Aerodynamic Design of Transonic Adaptive Airfoils with Natural Transition.- 2.5 Experiments in a Transonic Shock Tube at High Mach and Reynolds Numbers.- 3 Numerical Tools and Approaches for Flow Simulation with Local Adaptivity.- 3.1 H-Adaptive Multiscale Schemes for the Compressible Navier-Stokes Equations - Polyhedral Discretization, Data Compression and Mesh Generation.- 3.2 Automated Gradient Calculation.- 4 Computational and Experimental Aeroelasticity.- 4.1 On Well-Posedness and Modelling for Nonlinear Aeroelasticity.- 4.2 Concepts for Reduced Structural Models of Airplane Wings in Aeroelasticity.- 4.3 Computational Aeroelasticity with Reduced Structural Models.- 4.4 Approximated Nonlinear Stability Analysis of the Dynamics of Flexible Aircraft.- 4.5 Analysis of Unsteady Airfoils at Low Speeds.- 4.6 Experiments on Transonic Aerodynamics about Elastically Suspended Airfoils.- 4.7 Design, Qualification and Experimental Investigation on Flexible Wind-Tunnel Wing Models.

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