English: Lift and drag coefficients for NACA 633618 airfoil. Red values at Re=9.10^6, blue at 3.10^6. Full curves Cl, dashed Cd. Data Nasa via Abbott & Doenhoff, Theory of wing sections.
to share – to copy, distribute and transmit the work
to remix – to adapt the work
Under the following conditions:
attribution – You must give appropriate credit, provide a link to the license, and indicate if changes were made. You may do so in any reasonable manner, but not in any way that suggests the licensor endorses you or your use.
share alike – If you remix, transform, or build upon the material, you must distribute your contributions under the same or compatible license as the original.