Flying LS6 glider with whool \ from aoa Watch Video
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Description: Objective : visualize flow separation in the root of LS6 glider.nnResult : flow in wing fuselage junction is sensitive to aoa & aileron:flap deflection.nnIn stall : nSeparation occurs at lower fuselage attitude when flap increase. Tip : visualize this by looking at tail position vs horizon when separation appears.nnIn normal flight : nTransition : separation is not visible. Very slight tuft activity on the fuselage sides.nCircling : Seperation occurs quite often, particularly on the wing ins
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