Results of tests of six airfoils having N A C A 230 mean line and varying in thickness from 0.00c to 0.21c; results agree with previous findings in showing that aerodynamically best section is one of moderate thickness.
Tests of N.A.C.A. Airfoils in variable-density wind tunnel
Nat Advisory Committee Aeronautics -- Tech Notes
1936
5 pages
Supp sheets
Report
Englisch
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Tests of N.A.C.A. airfoils in variable-density wind tunnel, series 24
Engineering Index Backfile | 1932
|Tests of N.A.C.A. Airfoils in variable-density wind tunnel, series 4e and 63
Engineering Index Backfile | 1931
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