25th Congress of International Council of the Aeronautical Sciences, 3 - 8 September 2006, Hamburg, Germany
Paper ICAS 2006-3.1.2


INVESTIGATION OF FLOW PHENOMENA ON GENERIC DELTA WING

A. Furman, C. Breitsamter
TU Munich, Germany

Keywords: Aerodynamics, Experiments, High Angle of Attack, Vortex Flow,Wind Tunnel

A comprehensive experimental research program on a generic delta wing is conducted within the “International Vortex Flow Experiment 2”. The aim is to setup a validated data base for test of modern CFD methods. Flow types of partly developed, fully developed and burst leading-edge vortices are investigated for different leading-edges.


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