Glasair III - the AOE home page
Glasair III - the AOE home page
Glasair III - the AOE home page
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Spanload0.4<strong>Glasair</strong> Spanload0.350.30.25c a vg/C Lc0.20.15AR=6.2λ=0.75α=4°0.10.05Planar Wing, e=0.972261° Washout e=0.99009Elliptic Spanload00 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1η=y/(b/2)*Using Lifting Line Theory