03.2 - Experimental Aerodynamics
EXPERIMENTAL AND NUMERICAL INVESTIGATION OF A STRUCTURAL-DYNAMICALLY SCALED DELTA WING WITH TRAINING EDGE FLAPS
K. Bantscheff¹, F. Santelli¹, C. Breitsamter¹; ¹Technische Universität München / Lehrstuhl für Aerodynamik, Germany
The main objective of this work focuses on the conduction of experimental investigations of a newly developed aeroelastically scaled delta wing featuring deflectable trailing edge flaps. The model at hand is used to study the effects of different flap angles on the occurring flow phenomena for low Mach numbers and stationary inflow conditions considering dynamic deformations.