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Winfoil Airfoils - Total Number: 277
Name T/C % T/C % Chord Position Camber % Camber Chord % CL Max CD Min
<< First < Prev 36 37 38 39 40 Next > Last >>
HN93-F3F.323 8.55 30 2.001 45 1.061 0.0052
HN93-F3B.320 8.85 30 2.146 40 0.942 0.0059
HN93-285.935 9.35 30 2.846 40 1.035 0.006
GOTTINGEN 622 8 30 2.38 40 1.015 0.011
GOTTINGEN 549 13.83 30 4.688 40 1.706 0.0084
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.15 0.36 0.15 -0.33
0.4 0.8 0.4 -0.62
1 1.28 1 -0.9
2 1.92 2 -1.22
4 2.83 4 -1.66
6 3.5 6 -1.94
8 4.02 8 -2.14
10 4.43 10 -2.28
15 5.22 15 -2.47
20 5.71 20 -2.52
25 6.01 25 -2.49
30 6.16 30 -2.4
35 6.18 35 -2.27
40 6.1 40 -2.11
45 5.93 45 -1.93
50 5.68 50 -1.74
55 5.35 55 -1.53
60 4.97 60 -1.32
65 4.53 65 -1.1
70 4.01 70 -0.88
75 3.44 75 -0.67
80 2.81 80 -0.47
85 2.12 85 -0.29
90 1.4 90 -0.13
95 0.66 95 -0.02
100 0 100 0
X Y
1 0
0.95 0.0066
0.9 0.014
0.85 0.0212
0.8 0.0281
0.75 0.0344
0.7 0.0401
0.65 0.0453
0.6 0.0497
0.55 0.0535
0.5 0.0568
0.45 0.0593
0.4 0.061
0.35 0.0618
0.3 0.0616
0.25 0.0601
0.2 0.0571
0.15 0.0522
0.1 0.0443
0.08 0.0402
0.06 0.035
0.04 0.0283
0.02 0.0192
0.01 0.0128
0.004 0.008
0.0015 0.0036
0 0
0 0
0.0015 -0.0033
0.004 -0.0062
0.01 -0.009
0.02 -0.0122
0.04 -0.0166
0.06 -0.0194
0.08 -0.0214
0.1 -0.0228
0.15 -0.0247
0.2 -0.0252
0.25 -0.0249
0.3 -0.024
0.35 -0.0227
0.4 -0.0211
0.45 -0.0193
0.5 -0.0174
0.55 -0.0153
0.6 -0.0132
0.65 -0.011
0.7 -0.0088
0.75 -0.0067
0.8 -0.0047
0.85 -0.0029
0.9 -0.0013
0.95 -0.0002
1 0
X Y
100 0
95 0.66
90 1.4
85 2.12
80 2.81
75 3.44
70 4.01
65 4.53
60 4.97
55 5.35
50 5.68
45 5.93
40 6.1
35 6.18
30 6.16
25 6.01
20 5.71
15 5.22
10 4.43
8 4.02
6 3.5
4 2.83
2 1.92
1 1.28
0.4 0.8
0.15 0.36
0 0
0 0
0.15 -0.33
0.4 -0.62
1 -0.9
2 -1.22
4 -1.66
6 -1.94
8 -2.14
10 -2.28
15 -2.47
20 -2.52
25 -2.49
30 -2.4
35 -2.27
40 -2.11
45 -1.93
50 -1.74
55 -1.53
60 -1.32
65 -1.1
70 -0.88
75 -0.67
80 -0.47
85 -0.29
90 -0.13
95 -0.02
100 0
V 1.1