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 22 23 24 25 26 Next > Last >>
MH25 9.98 39.57 1.459 39.57 0.851 0.0056
MH26 10.98 39.66 1.509 39.66 0.942 0.0046
MH27 11.98 44.7 1.499 39.74 0.991 0.0048
MH28 10.05 40.94 1.319 48.06 0.822 0.0054
MH29 13.6 40.94 1.626 26.59 0.97 0.0065
Coordinates
XUpper YUpper XLower YLower
0 0.02 0 0.02
0.02 0.12 0.01 -0.07
0.08 0.29 0.05 -0.15
0.19 0.47 0.12 -0.24
0.76 1.06 0.28 -0.37
1.83 1.76 0.49 -0.51
3.36 2.47 1.67 -1.01
5.34 3.16 3.29 -1.46
7.75 3.81 5.4 -1.86
10.58 4.4 8.01 -2.22
13.8 4.93 11.09 -2.53
17.39 5.39 14.6 -2.8
21.31 5.77 18.5 -3.03
25.54 6.07 22.75 -3.21
30.02 6.28 27.31 -3.36
34.71 6.41 32.11 -3.46
39.57 6.46 37.11 -3.51
44.54 6.42 42.25 -3.53
49.57 6.31 47.47 -3.5
54.61 6.12 52.72 -3.44
59.61 5.86 57.93 -3.33
64.5 5.54 63.05 -3.19
69.24 5.15 68.01 -3.02
73.77 4.7 72.76 -2.8
78.05 4.19 77.24 -2.54
82.02 3.63 81.4 -2.23
85.67 2.99 85.23 -1.83
89.01 2.28 88.74 -1.4
92.04 1.6 91.87 -0.98
94.69 0.99 94.58 -0.6
96.89 0.52 96.82 -0.29
98.57 0.2 98.54 -0.09
99.64 0.05 99.63 -0.01
100 0 100 0
X Y
1 0
0.9964 0.0005
0.9857 0.002
0.9689 0.0052
0.9469 0.0099
0.9204 0.016
0.8901 0.0228
0.8567 0.0299
0.8202 0.0363
0.7805 0.0419
0.7377 0.047
0.6924 0.0515
0.645 0.0554
0.5961 0.0586
0.5461 0.0612
0.4957 0.0631
0.4454 0.0642
0.3957 0.0646
0.3471 0.0641
0.3002 0.0628
0.2554 0.0607
0.2131 0.0577
0.1739 0.0539
0.138 0.0493
0.1058 0.044
0.0775 0.0381
0.0534 0.0316
0.0336 0.0247
0.0183 0.0176
0.0076 0.0106
0.0019 0.0047
0.0008 0.0029
0.0002 0.0012
0 0.0002
0 0.0002
0.0001 -0.0007
0.0005 -0.0015
0.0012 -0.0024
0.0028 -0.0037
0.0049 -0.0051
0.0167 -0.0101
0.0329 -0.0146
0.054 -0.0186
0.0801 -0.0222
0.1109 -0.0253
0.146 -0.028
0.185 -0.0303
0.2275 -0.0321
0.2731 -0.0336
0.3211 -0.0346
0.3711 -0.0351
0.4225 -0.0353
0.4747 -0.035
0.5272 -0.0344
0.5793 -0.0333
0.6305 -0.0319
0.6801 -0.0302
0.7276 -0.028
0.7724 -0.0254
0.814 -0.0223
0.8523 -0.0183
0.8874 -0.014
0.9187 -0.0098
0.9458 -0.006
0.9682 -0.0029
0.9854 -0.0009
0.9963 -0.0001
1 0
X Y
100 0
99.64 0.05
98.57 0.2
96.89 0.52
94.69 0.99
92.04 1.6
89.01 2.28
85.67 2.99
82.02 3.63
78.05 4.19
73.77 4.7
69.24 5.15
64.5 5.54
59.61 5.86
54.61 6.12
49.57 6.31
44.54 6.42
39.57 6.46
34.71 6.41
30.02 6.28
25.54 6.07
21.31 5.77
17.39 5.39
13.8 4.93
10.58 4.4
7.75 3.81
5.34 3.16
3.36 2.47
1.83 1.76
0.76 1.06
0.19 0.47
0.08 0.29
0.02 0.12
0 0.02
0 0.02
0.01 -0.07
0.05 -0.15
0.12 -0.24
0.28 -0.37
0.49 -0.51
1.67 -1.01
3.29 -1.46
5.4 -1.86
8.01 -2.22
11.09 -2.53
14.6 -2.8
18.5 -3.03
22.75 -3.21
27.31 -3.36
32.11 -3.46
37.11 -3.51
42.25 -3.53
47.47 -3.5
52.72 -3.44
57.93 -3.33
63.05 -3.19
68.01 -3.02
72.76 -2.8
77.24 -2.54
81.4 -2.23
85.23 -1.83
88.74 -1.4
91.87 -0.98
94.58 -0.6
96.82 -0.29
98.54 -0.09
99.63 -0.01
100 0
V 1.1