Airfoil Section Characteristics as Affected by Variations of the Reynolds Number (1937)
NASA Technical Reports Server (NTRS) · leaf 37
AIRFOIL SECTION CHARACTERISTICS AS AFFECTED BY VARIATIONS OF THE REYNOLDS NUMBER 33 … Figure 44. The cdQ values at other lift coefficients may now be Airfoil section drag.—In design work, values of obtained from the generalized variation of ACdQ with the section minimum drag coefficient cdQ min for aerody- \ci~cipy\ presented in figure 45, where the standard airfoil characteristic…
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