FLYING SHAPE ACQUISITION: Used for validation of RANS numerical model. Highlighted need for extremely accurate acquisition, in particular the angles. COMPARISON RANS / WIND TUNNEL. RANS model = accurate: less than 10% difference with force measurements. IMPORTANCE OF MODELLING THE HULL. Influences flow even at mid-span of mast. Influence on the lower tip vortices: tangles the 2 vortices & reduce suction and vorticity in vortex core. Increases lift and drag. SCALING EFFECTS (1:15 in 4m/s VS full scale in 15 kts). 10% difference in lift/drag & 11% difference of suction in upper tip vortex. Full similitude for 1:15 scale => wind speed 115 m/s!!!
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机译：飞行形状采集：用于验证RAN数值模型。强调需要极其准确的采集，特别是角度。比较RAN / WIND TUNNEL。 RAN模型=准确：与力测量的差异小于10％。模拟船体的重要性。即使在桅杆的中间跨度，也会影响流动。影响下尖端涡旋：缠结2涡流并减少涡旋芯中的吸力和涡旋。增加升力和拖动。缩放效果（1:15以4m / s为15 kts满量程）。上尖涡旋升降/拖拉和11％差异差异10％。完全类似于1:15 Scale =>风速115 M / s !!!
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