Aerodynamic Characteristics of Twenty-Four Airfoils at High Speeds (1930)
NASA Technical Reports Server (NTRS) · leaf 18
Figure 41.—Drag coefficient, Cd vs. position of maximum ordinate for various lift coefficients, Figure 40.—Drag coefficient. Co vs. position of maximum ordinate for various lift coefficients, Cl, at V/c—1.08 for R family Cl, at V7c=0.95 for R family
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