Aerodynamics force tests made in N.A.C.A. 7 by 10-ft wind tunnel on model wing with 20% chord split flap deflected 60° downward; results given in form of curves of lift, drag, and center of pressure.
Effect of partial-span split flaps on aerodynamic characteristics of clark Y wing
Nat Advisory Committee Aeronautics -- Tech Notes
1933
5 pages
4 Supp Sheets
Aufsatz (Zeitschrift)
Englisch
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Engineering Index Backfile | 1938
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Engineering Index Backfile | 1934
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