Tests with three different sized split trailing-edged flaps, in N.A.C.A. 7 by 10-ft wind tunnel; split flaps when deflected about their original axis locations gave slightly higher maximum lift coefficients than conventional trailing-edge flaps, and lift coefficients were increased still further by moving axes toward rear.
Aerodynamic characteristics of model wing having split flap deflected downward and moved to rear
Nat Advisory Committee Aeronautics -- Tech Notes
1932
7 pages
11 Supp plates
Report
English
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Aerodynamic performance of a wing with a deflected tip-mounted reverse half-delta wing
Tema Archive | 2012
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