Tests conducted in NACA 7 by 10 ft tunnel to ascertain aerodynamic characteristics, which involved determination of best slot gap opening, effects of slot width, and effect of trailing edge flap; results of tests.
Wind-tunnel tests of Clark Y wing with "maxwell" leading-edge slots
Nat Advisory Committee Aeronautics -- Tech Note
1937
6 pages
9 Supp sheets
Aufsatz (Zeitschrift)
Englisch
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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
|