03.1 - Aerodynamics - CFD Methods and Validation
MORPHING WING WITH SURFACE DISCONTINUITY - COMPARATIVE TESTS
A. Tarnowski¹, T. Goetzendorf-Grabowski¹, J. Mieloszyk¹; ¹Warsaw University of Technology, Poland
This article describes comparative analysis of wind tunnel tests of the novel morphing flying wing and reference (non-morphing) flying wing, both sharing the same geometry. Additionally, the results of numerical aerodynamic analysis are presented as the background and preparation for the wind tunnel experiments.