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