Aerodynamic force tests made in wind tunnel using highly tapered Clark Y wing equipped with various split flaps; results given for both full and partial span split flaps.
Effects of full-span and partial-span split flaps on aerodynamic characteristics of tapered wing
Nat Advisory Committee Aeronautics -- Tech Notes
1934
6 pages
5 Supp plates, Bibliography
Report
English
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Effect of partial-span split flaps on aerodynamic characteristics of clark Y wing
Engineering Index Backfile | 1933
|Calculation of aerodynamic characteristics of tapered wings with partial-span flaps
Engineering Index Backfile | 1939
|Engineering Index Backfile | 1939
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