Results are given in form of load distributions and as calculated moment coefficients; experimental values of rolling and yawing moment coefficients were in fairly close agreement with theory.
Pressure distribution measurements on tapered wing with partial-span split flap in curved flight
Nat Advisory Committee Aeronautics -- Tech Note
1939
6 pages
6 Supp sheets, Bibliography
Report
English
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Pressure-distribution measurements on tapered wing with full-span split flap in curved flight
Engineering Index Backfile | 1939
|Pressure-distribution measurements on rectangular wing with partial-span split flap in curved flight
Engineering Index Backfile | 1939
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