Tests by 10-ft wind tunnel at NACA, to determine control forces and air loads acting on split flaps, by using Clark-Y wing models with two different sizes of full-span split flaps.
Wind-tunnel measurement of air loads on split flaps
Nat Advisory Commitee Aeronautics -- Tech Note
1934
8 pages
6 Supp plates
Report
Englisch
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Wind-tunnel measurements of air loads on split flaps
NTRS | 1934
|Wind tunnel measurements of air loads on split flaps
SLUB | 1934
|Wind-tunnel tests of clark Y wing having split flaps with gaps
Engineering Index Backfile | 1938
|Wind-tunnel tests of clark Y wing having split flaps with gaps
Engineering Index Backfile | 1938
|