GA 37-011


GA 37-011

Curve fits of basic Javafoil data for GA 37-011, smooth airfoils, Mach 0:


Re: 500k | 1M | 3M | 6M

Re = 500k | 1M | 3M | 6M





Re = 1M | 500k | 3M | 6M





Re = 3M | 500k | 1M | 6M





Re = 6M | 500k | 1M | 3M