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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 44 45 46 47 48 Next > Last >>
CLARK Y 11.73 30.87 3.528 43.47 1.595 0.006
CLARK W 11.21 30 3.684 40 1.643 0.0075
CLARK V 11.6 30 3.355 50 1.617 0.0074
CLARK K 11.38 39.65 3.245 39.65 1.676 0.0066
BOEING-VERTOL VR-1 10.95 35.27 1.542 43.33 1.121 0.0059
Coordinates
XUpper YUpper XLower YLower
0 0.05 0 0.05
0.11 0.62 0.11 -0.45
0.43 1.25 0.43 -0.9
0.96 1.94 0.96 -1.3
1.7 2.65 1.7 -1.65
2.65 3.35 2.65 -1.96
3.81 4.03 3.81 -2.21
5.16 4.68 5.16 -2.41
6.7 5.31 6.7 -2.57
8.43 5.94 8.43 -2.68
10.33 6.55 10.33 -2.76
12.41 7.13 12.41 -2.82
14.65 7.66 14.65 -2.84
17.03 8.11 17.03 -2.83
19.56 8.48 19.56 -2.8
22.22 8.77 22.22 -2.73
25 9 25 -2.65
27.89 9.16 27.89 -2.56
30.87 9.27 30.87 -2.46
33.93 9.32 33.93 -2.35
37.06 9.31 37.06 -2.24
43.47 9.13 43.47 -2.02
50 8.72 50 -1.79
56.53 8.11 56.53 -1.57
62.94 7.32 62.94 -1.35
69.13 6.41 69.13 -1.13
75 5.41 75 -0.93
80.44 4.39 80.44 -0.74
85.36 3.4 85.36 -0.58
89.67 2.48 89.67 -0.43
93.3 1.66 93.3 -0.3
96.19 0.97 96.19 -0.19
98.3 0.45 98.3 -0.09
99.57 0.12 99.57 -0.03
100 0 100 0
X Y
1 0
0.9957 0.0012
0.983 0.0045
0.9619 0.0097
0.933 0.0166
0.8967 0.0248
0.8536 0.034
0.8044 0.0439
0.75 0.0541
0.6913 0.0641
0.6294 0.0732
0.5653 0.0811
0.5 0.0872
0.4347 0.0913
0.3706 0.0931
0.3393 0.0932
0.3087 0.0927
0.2789 0.0916
0.25 0.09
0.2222 0.0877
0.1956 0.0848
0.1703 0.0811
0.1465 0.0766
0.1241 0.0713
0.1033 0.0655
0.0843 0.0594
0.067 0.0531
0.0516 0.0468
0.0381 0.0403
0.0265 0.0335
0.017 0.0265
0.0096 0.0194
0.0043 0.0125
0.0011 0.0062
0 0.0005
0 0.0005
0.0011 -0.0045
0.0043 -0.009
0.0096 -0.013
0.017 -0.0165
0.0265 -0.0196
0.0381 -0.0221
0.0516 -0.0241
0.067 -0.0257
0.0843 -0.0268
0.1033 -0.0276
0.1241 -0.0282
0.1465 -0.0284
0.1703 -0.0283
0.1956 -0.028
0.2222 -0.0273
0.25 -0.0265
0.2789 -0.0256
0.3087 -0.0246
0.3393 -0.0235
0.3706 -0.0224
0.4347 -0.0202
0.5 -0.0179
0.5653 -0.0157
0.6294 -0.0135
0.6913 -0.0113
0.75 -0.0093
0.8044 -0.0074
0.8536 -0.0058
0.8967 -0.0043
0.933 -0.003
0.9619 -0.0019
0.983 -0.0009
0.9957 -0.0003
1 0
X Y
100 0
99.57 0.12
98.3 0.45
96.19 0.97
93.3 1.66
89.67 2.48
85.36 3.4
80.44 4.39
75 5.41
69.13 6.41
62.94 7.32
56.53 8.11
50 8.72
43.47 9.13
37.06 9.31
33.93 9.32
30.87 9.27
27.89 9.16
25 9
22.22 8.77
19.56 8.48
17.03 8.11
14.65 7.66
12.41 7.13
10.33 6.55
8.43 5.94
6.7 5.31
5.16 4.68
3.81 4.03
2.65 3.35
1.7 2.65
0.96 1.94
0.43 1.25
0.11 0.62
0 0.05
0 0.05
0.11 -0.45
0.43 -0.9
0.96 -1.3
1.7 -1.65
2.65 -1.96
3.81 -2.21
5.16 -2.41
6.7 -2.57
8.43 -2.68
10.33 -2.76
12.41 -2.82
14.65 -2.84
17.03 -2.83
19.56 -2.8
22.22 -2.73
25 -2.65
27.89 -2.56
30.87 -2.46
33.93 -2.35
37.06 -2.24
43.47 -2.02
50 -1.79
56.53 -1.57
62.94 -1.35
69.13 -1.13
75 -0.93
80.44 -0.74
85.36 -0.58
89.67 -0.43
93.3 -0.3
96.19 -0.19
98.3 -0.09
99.57 -0.03
100 0
V 1.1