6-series
An improvement over 1-series airfoils with emphasis on maximizing laminar flow. The airfoil is described using six digits in the following sequence:
- The number "6" indicating the series.
- One digit describing the distance of the minimum pressure area in tens of percent of chord.
- The subscript digit gives the range of lift coefficient in tenths above and below the design lift coefficient in which favorable pressure gradients exist on both surfaces
- A hyphen.
- One digit describing the design lift coefficient in tenths.
- Two digits describing the maximum thickness in tens of percent of chord.
For example, the NACA 612-315 a=0.5 has the area of minimum pressure 10% of the chord back, maintains low drag 0.2 above and below the lift coefficient of 0.3, has a maximum thickness of 15% of the chord, and maintains laminar flow over 50% of the chord.
Read more about this topic: NACA Airfoil