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
01.07.1931
Sonstige
Keine Angabe
Englisch
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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