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 23 24 25 26 27 Next > Last >>
MH32 8.71 30.13 2.368 44.4 0.742 0.0035
MH33 7.27 29.28 1.124 43.91 0.779 0.0042
MH42 8.93 33.43 1.963 38.14 0.99 0.0055
MH43 8.49 28.93 1.86 38.19 1.003 0.0046
MH45 9.83 27.56 1.644 36.72 1.027 0.0052
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.1 0 0.28 -0.46
0.29 0.6 1.17 -0.88
1.03 1.31 2.58 -1.27
2.19 2.07 4.5 -1.6
3.78 2.83 6.91 -1.87
5.79 3.56 9.78 -2.07
8.21 4.25 13.11 -2.21
11.02 4.86 16.85 -2.27
14.2 5.4 20.97 -2.27
17.74 5.84 25.43 -2.22
21.59 6.19 30.19 -2.13
25.73 6.44 35.18 -1.99
30.13 6.59 40.37 -1.82
34.73 6.63 45.65 -1.63
39.5 6.57 51.05 -1.43
44.4 6.41 56.43 -1.22
49.37 6.16 61.75 -1
54.37 5.83 66.95 -0.8
59.35 5.43 71.97 -0.61
64.25 4.98 76.75 -0.43
69.02 4.47 81.22 -0.29
73.6 3.91 85.33 -0.17
77.97 3.32 89.02 -0.08
82.09 2.71 92.25 -0.03
85.9 2.12 94.96 0
89.36 1.57 97.13 0.01
95.04 0.68 98.7 0.01
98.71 0.15 99.67 0
100 0 100 0
X Y
1 0
0.9871 0.0015
0.9504 0.0068
0.8936 0.0157
0.859 0.0212
0.8209 0.0271
0.7797 0.0332
0.736 0.0391
0.6902 0.0447
0.6425 0.0498
0.5935 0.0543
0.5437 0.0583
0.4937 0.0616
0.444 0.0641
0.395 0.0657
0.3473 0.0663
0.3013 0.0659
0.2573 0.0644
0.2159 0.0619
0.1774 0.0584
0.142 0.054
0.1102 0.0486
0.0821 0.0425
0.0579 0.0356
0.0378 0.0283
0.0219 0.0207
0.0103 0.0131
0.0029 0.006
0.001 0
0 0
0 0
0.0028 -0.0046
0.0117 -0.0088
0.0258 -0.0127
0.045 -0.016
0.0691 -0.0187
0.0978 -0.0207
0.1311 -0.0221
0.1685 -0.0227
0.2097 -0.0227
0.2543 -0.0222
0.3019 -0.0213
0.3518 -0.0199
0.4037 -0.0182
0.4565 -0.0163
0.5105 -0.0143
0.5643 -0.0122
0.6175 -0.01
0.6695 -0.008
0.7197 -0.0061
0.7675 -0.0043
0.8122 -0.0029
0.8533 -0.0017
0.8902 -0.0008
0.9225 -0.0003
0.9496 0
0.9713 0.0001
0.987 0.0001
0.9967 0
1 0
X Y
100 0
98.71 0.15
95.04 0.68
89.36 1.57
85.9 2.12
82.09 2.71
77.97 3.32
73.6 3.91
69.02 4.47
64.25 4.98
59.35 5.43
54.37 5.83
49.37 6.16
44.4 6.41
39.5 6.57
34.73 6.63
30.13 6.59
25.73 6.44
21.59 6.19
17.74 5.84
14.2 5.4
11.02 4.86
8.21 4.25
5.79 3.56
3.78 2.83
2.19 2.07
1.03 1.31
0.29 0.6
0.1 0
0 0
0 0
0.28 -0.46
1.17 -0.88
2.58 -1.27
4.5 -1.6
6.91 -1.87
9.78 -2.07
13.11 -2.21
16.85 -2.27
20.97 -2.27
25.43 -2.22
30.19 -2.13
35.18 -1.99
40.37 -1.82
45.65 -1.63
51.05 -1.43
56.43 -1.22
61.75 -1
66.95 -0.8
71.97 -0.61
76.75 -0.43
81.22 -0.29
85.33 -0.17
89.02 -0.08
92.25 -0.03
94.96 0
97.13 0.01
98.7 0.01
99.67 0
100 0
V 1.1