Airfoil:

mm

Job Status

Please wait while the PDF is generated...

Plot Number:

File:

Search for Airfoil
Winfoil Airfoils - Total Number: 277
Name T/C % T/C % Chord Position Camber % Camber Chord % CL Max CD Min
<< First < Prev 44 45 46 47 48 Next > Last >>
RAF 38 12.6 30 2.531 40 1.523 0.0058
RAF 6 9.97 29.97 4.541 29.97 1.996 0.0078
RG 15 8.92 30.25 1.761 39.73 1.11 0.0057
RG8 10.78 30 2.224 60 1.096 0.0069
RITZ 1-30-10 9.94 30 0.999 30 1.008 0.0093
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
2.5 2.98 2.5 -2.02
5 4.21 5 -2.66
10 5.94 10 -3.38
20 7.91 20 -3.86
30 8.75 30 -3.9
40 8.69 40 -3.66
50 8.06 50 -3.23
60 6.85 60 -2.73
70 5.27 70 -2.13
80 3.54 80 -1.46
90 1.83 90 -0.79
100 0 100 0
X Y
1 0
0.9 0.0183
0.8 0.0354
0.7 0.0527
0.6 0.0685
0.5 0.0806
0.4 0.0869
0.3 0.0875
0.2 0.0791
0.1 0.0594
0.05 0.0421
0.025 0.0298
0 0
0 0
0.025 -0.0202
0.05 -0.0266
0.1 -0.0338
0.2 -0.0386
0.3 -0.039
0.4 -0.0366
0.5 -0.0323
0.6 -0.0273
0.7 -0.0213
0.8 -0.0146
0.9 -0.0079
1 0
X Y
100 0
90 1.83
80 3.54
70 5.27
60 6.85
50 8.06
40 8.69
30 8.75
20 7.91
10 5.94
5 4.21
2.5 2.98
0 0
0 0
2.5 -2.02
5 -2.66
10 -3.38
20 -3.86
30 -3.9
40 -3.66
50 -3.23
60 -2.73
70 -2.13
80 -1.46
90 -0.79
100 0
V 1.1