Simulation of Wing and Nacelle Stall, Juni 2010

Joint Symposium of DFG FOR 1066 and DLR-Airbus C²A²S²E: "Simulation of Wing and Nacelle Stall"

22 - 23 June 2010, Braunschweig, Germany

Symposium Co-Chairmen: Prof. R. Radespiel and Prof. N. Kroll

Reliable simulations of flow separation on airfoils, wings and powered engine nacelles at high Reynolds numbers represent great challenges in defining suitable mathematical models, computing numerically accurate solutions and providing comprehensive experimental data for the validation of numerical simulations. Additional scientific problems arise from the need to consider airframe-engine interactions and inhomogeneous onset flow conditions as real aircraft operate in atmospheric environments with sometimes rather large distortions. The symposium aims to bring together scientists dealing with numerical simulations of these flows and researchers who contribute experimental work for validation. The participation of young researchers is encouraged. The exchange of ideas and results will be through 30 minutes presentations by the participants. Invited lectures given by leading international scientists and engineers from industry and academia will highlight the current status in the field.


FUNDAMENTALS OF STALL MODELLING – 1

FUNDAMENTALS OF STALL MODELLING – 2

SIMULATION OF ATMOSPHERIC DISTURBANCES

Weigold, W., Kruse, M.:
Gust and Turbulence Simulation for Design and Certification of Large Aeroplanes - Industrial Application of Unsteady Aerodynamics for Loads

INLET AND ENGINE FLOWS

APPLICATIONS IN HIGH-LIFT FLOWS