Airfoil Comparison

Configure geometry filters and flow conditions to run a NeuralFoil powered aerodynamic airfoil comparison!

Geometry Filters

Filter airfoils by geometry parameters before running analysis.

Include Foils with

in the name

Exclude Foils with

in the name

Thickness

Camber

Matching airfoils:0 airfoils

Configure the flow conditions for the performance analysis.

Reynolds Number (thousands)

Range: 80k - 5000k

Mach Number

Range: 0 - 0.8, Step size: 0.05

Alpha Range (degrees)

Min

Max

Range: -25° to 90°, Step size: 0.5°

N_crit

Range: 5 - 9 (integer only)

No airfoils match the selected filters.