Principal Investigator:
Torsten Auerswald and Jens Bange
, Center for Applied Geoscience, University of Tübingen (Germany)
HPC Platform used:
Hermit and Hornet of HLRS
Local Project ID:
WAF
This project aims at the simulation of the influence of a turbulent atmospheric boundary layer flow on a wing. For this purpose the compressible flow solver DLR-TAU is used, which is developed by the German Aerospace Center (DLR). For initialising the simulation with a turbulent wind field a method to generate synthetic turbulence is used. This method uses statistics from measured time series from the atmospheric boundary layer to generate a threedimensional turbulent wind field which can be used as initial field in the flow simulations.
