The characteristics of 78 related airfoil sections from tests in the variable-density wind tunnel (1933)
NASA Technical Reports Server (NTRS) · leaf 52
CHARACTERISTICS OP AIRFOIL SECTIONS FROM TESTS IN VARIABLE-DENSITY "WIND TUNNEL 51 and for the highly cambered sections a definite increase it is not primarily dependent upon the shape of the accompanies a forward movement of the camber. mean line. Nevertheless it is interesting to compare … an airfoil section. The variation of this ratio with Figure 04.—Additional profile drag as a function or CL— CloVu Results are for air- thickness is shown in figure 95. The curves of this foils having normal camber positions (0.3c to 0.5c). figure indicate that the highest values of the ratio are…
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
