This paper is the first of a series covering an investigation of a family of airfoils all formed from a basic profile. It gives in preliminary form the results of six symmetrical airfoils, differing only in maximum thickness. The maximum thickness-to-chord ratios are 0.06, 0.09, 0.12, 0.15, 0.18, and 0.21.
Tests of six symmetrical airfoils in the variable density wind tunnel
1931-07-01
Miscellaneous
No indication
English
Tests of six symmetrical airfoils in variable density wind tunnel
Engineering Index Backfile | 1931
|Tests of N.A.C.A. Airfoils in variable-density wind tunnel
Engineering Index Backfile | 1936
|Tests of related airfoils in the variable-density wind tunnel
TIBKAT | 1937
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