In case of small leading airfoil full-scale and model maximum lift coefficients are in agreement at 0.74; with large leading airfoil, however, full scale reaches 0.85 as compared with 0.77 for model.
Full-scale and model measurements of lift and drag of Bristol fighter with Handley Page slotted wings
Aeronautical Research Committee -- Reports Memoranda
1925
9 pages
14 Figs.
Report
English
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