Tests to find lift, drag, and center-of-pressure characteristics of split-flap airfoil with internal air passage; highest lift coefficient 2.08 obtained with passage closed.
Wind-tunnel tests of hall high-lift wing
Nat Advisory Committee Aeronautics -- Tech Notes
1932
4 pages
6 Supp plates
Report
English
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Wind tunnel tests of a hall high lift wing
SLUB | 1932
|Wind-tunnel Tests of a Hall High-life Wing
NTRS | 1932
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