Step 1: Recall the NACA 6-series airfoil designation.
For a NACA 6-series airfoil,
\[
\boxed{\text{NACA }6x\text{-}abc}
\]
where
• First digit (\(6\)) denotes the 6-series airfoil.
• Second digit indicates the location of minimum pressure.
• Third digit indicates the design lift coefficient.
• Last two digits indicate the maximum thickness as a percentage of the chord.
Step 2: Interpret NACA 64-212.
For
\[
\boxed{\text{NACA }64\text{-}212,}
\]
the third digit
\[
\boxed{2}
\]
represents the design lift coefficient.
Therefore,
\[
\boxed{\text{Design Lift Coefficient}}
\]
is the correct answer.
Thus,
\[
\boxed{(A)}
\]
is the correct answer.