Titlebook: New Results in Numerical and Experimental Fluid Mechanics IX; Contributions to the Andreas Dillmann,Gerd Heller,Ulrich Rist Book 2014 Sprin

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New Results in Numerical and Experimental Fluid Mechanics IXContributions to the

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Numerical Investigation of the Flutter Behaviour of a Laminar Supercritical Airfoilaminar flow on this boundary is however still unclear. Therefore numerical simulations have been performed. These show that the flutter behaviour of a laminar supercritical airfoil is more critical at transonic conditions in case of (partly) laminar flow.

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Influence of Meshing on Flow Simulation in the Wing-Body Junction of Transport Aircraftlest meshing effort the unstructured grid simulation yields good agreement of surface pressure and boundary layers with the hybrid meshes. The strong impact of the boundary layer grid edge on the velocity profiles emphasizes the need of sufficiently high boundary layer grids on all surface parts.

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Aero-Elastic Multipoint Optimization Using the Coupled Adjoint Approach structure solvers. This new study employs the coupled adjoint approach to perform a proof-of-concept multipoint aero-elastic optimization. The optimized design is then compared to another design resulting from a single point optimization and proved to have a better overall performance.