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 21 22 23 24 25 Next > Last >>
MH18B 11.73 39.6 1.956 39.6 0.904 0.005
MH20 9.02 32.97 2.146 32.97 0.831 0.004
MH22 7.21 28.86 1.889 33.42 0.739 0.0041
MH23 7.99 34.09 1.27 38.95 0.76 0.0042
MH24 8.99 39.3 1.301 39.3 0.813 0.0052
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.27 0.69 0.27 -0.55
1.09 1.4 1.09 -1.04
2.45 2.12 2.45 -1.49
4.32 2.86 4.32 -1.89
6.7 3.6 6.7 -2.26
9.55 4.34 9.55 -2.61
12.84 5.07 12.84 -2.92
16.54 5.76 16.54 -3.21
20.61 6.4 20.61 -3.46
25 6.96 25 -3.67
29.66 7.4 29.66 -3.82
34.55 7.7 34.55 -3.9
39.6 7.82 39.6 -3.92
44.77 7.73 44.77 -3.87
50 7.42 50 -3.77
55.23 6.9 55.23 -3.61
60.4 6.19 60.4 -3.42
65.45 5.33 65.45 -3.2
70.34 4.38 70.34 -2.95
75 3.41 75 -2.68
79.39 2.48 79.39 -2.38
83.46 1.65 83.46 -2.07
87.16 0.98 87.16 -1.73
90.45 0.48 90.45 -1.38
93.3 0.15 93.3 -1.03
95.68 -0.03 95.68 -0.7
97.55 -0.1 97.55 -0.41
98.91 -0.1 98.91 -0.18
99.73 -0.03 99.73 -0.05
100 0 100 0
X Y
1 0
0.9973 -0.0003
0.9891 -0.001
0.9755 -0.001
0.9568 -0.0003
0.933 0.0015
0.9045 0.0048
0.8716 0.0098
0.8346 0.0165
0.7939 0.0248
0.75 0.0341
0.7034 0.0438
0.6545 0.0533
0.604 0.0619
0.5523 0.069
0.5 0.0742
0.4477 0.0773
0.396 0.0782
0.3455 0.077
0.2966 0.074
0.25 0.0696
0.2061 0.064
0.1654 0.0576
0.1284 0.0507
0.0955 0.0434
0.067 0.036
0.0432 0.0286
0.0245 0.0212
0.0109 0.014
0.0027 0.0069
0 0
0 0
0.0027 -0.0055
0.0109 -0.0104
0.0245 -0.0149
0.0432 -0.0189
0.067 -0.0226
0.0955 -0.0261
0.1284 -0.0292
0.1654 -0.0321
0.2061 -0.0346
0.25 -0.0367
0.2966 -0.0382
0.3455 -0.039
0.396 -0.0392
0.4477 -0.0387
0.5 -0.0377
0.5523 -0.0361
0.604 -0.0342
0.6545 -0.032
0.7034 -0.0295
0.75 -0.0268
0.7939 -0.0238
0.8346 -0.0207
0.8716 -0.0173
0.9045 -0.0138
0.933 -0.0103
0.9568 -0.007
0.9755 -0.0041
0.9891 -0.0018
0.9973 -0.0005
1 0
X Y
100 0
99.73 -0.03
98.91 -0.1
97.55 -0.1
95.68 -0.03
93.3 0.15
90.45 0.48
87.16 0.98
83.46 1.65
79.39 2.48
75 3.41
70.34 4.38
65.45 5.33
60.4 6.19
55.23 6.9
50 7.42
44.77 7.73
39.6 7.82
34.55 7.7
29.66 7.4
25 6.96
20.61 6.4
16.54 5.76
12.84 5.07
9.55 4.34
6.7 3.6
4.32 2.86
2.45 2.12
1.09 1.4
0.27 0.69
0 0
0 0
0.27 -0.55
1.09 -1.04
2.45 -1.49
4.32 -1.89
6.7 -2.26
9.55 -2.61
12.84 -2.92
16.54 -3.21
20.61 -3.46
25 -3.67
29.66 -3.82
34.55 -3.9
39.6 -3.92
44.77 -3.87
50 -3.77
55.23 -3.61
60.4 -3.42
65.45 -3.2
70.34 -2.95
75 -2.68
79.39 -2.38
83.46 -2.07
87.16 -1.73
90.45 -1.38
93.3 -1.03
95.68 -0.7
97.55 -0.41
98.91 -0.18
99.73 -0.05
100 0
V 1.1