Low-speed wind tunnel tests have been made to investigate the flow around
a leading-edge vortex flap at the maximum L/D condition. Tests were also made to
measure the performance of the inverted vortex flap and the vortex ...
Low speed wind tunnel measurements have been made on a 1.15m span 60º delta wing with rounded leading-edge vortex flaps. the purpose of the measurements was to assess the benefits of the measurements was to assess the ...
Low speed wind tunnel studies have been conducted to investigate the effect of vortex flaps with a rounded leading-edge on delta wing performance. Measurements were done using the 60º delta wing at a Reynolds number based ...