06.1 - Flight Dynamics and Control (Control & Modelling)
GROUND EFFECT ON A SLENDER 65º DELTA WING WITH SIDESLIP, IMAGE METHOD, USING EULER
R.K. Nangia¹, T. Nangia¹; ¹Nangia, United Kingdom
With growing focus on supersonic/hypersonic flight, slender-wing performance, take-off and landing are of interest (typically up to AoA 16, AoS 10). Vortical flows lead to non-linearities particularly in longitudinal and directional moments. Using the “image” method, we show CFD results on the “ICE” Delta Wing in symmetric and asymmetric flow.