Aerodynamic Characteristics of Twenty-Four Airfoils at High Speeds (1930)
NASA Technical Reports Server (NTRS) · leaf 15
Figure 28—Drag coefficient, Co vs. camber ratio for various lift coefficients, Cl, at V/c=0.80, FIGURE 29.—Drag coefficient, Co vs. camber ratio for various lift coefficients Cl, at F/c=0.95, for C family for C family
NASA Technical Reports Server (NTRS)
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