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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 12 13 14 15 16 Next > Last >>
PRD 2B 12.25 30 4.725 40 1.371 0.0023
PRD 2A 12.95 30 3.852 40 1.744 0.0085
P-51H TIP 11.99 44.99 1.332 47.5 0.895 0.0062
P-51H ROOT 15.49 44.98 1.333 47.5 1.223 0.0031
P-51D TIP (BL215) 11.37 46.26 1.313 46.26 0.958 0.0054
Coordinates
XUpper YUpper XLower YLower
0 2.25 0 2.25
0.05 3 0.05 2.1
0.3 3.65 0.3 1.7
0.6 4 0.6 1.4
1 4.4 1 1.1
1.6 4.9 1.6 0.75
2.1 5.3 2.1 0.55
2.5 5.5 2.5 0.37
5 6.85 5 0.2
7.5 8 7.5 0.1
10 9 10 0
20 11.45 20 0
30 12.25 30 0
40 12.15 40 0
50 11.25 50 0
60 9.77 60 0
70 8 70 0
80 5.75 80 0
90 3.1 90 0
100 0 100 0
X Y
1 0
0.9 0.031
0.8 0.0575
0.7 0.08
0.6 0.0977
0.5 0.1125
0.4 0.1215
0.3 0.1225
0.2 0.1145
0.1 0.09
0.075 0.08
0.05 0.0685
0.025 0.055
0.021 0.053
0.016 0.049
0.01 0.044
0.006 0.04
0.003 0.0365
0.0005 0.03
0 0.0225
0 0.0225
0.0005 0.021
0.003 0.017
0.006 0.014
0.01 0.011
0.016 0.0075
0.021 0.0055
0.025 0.0037
0.05 0.002
0.075 0.001
0.1 0
0.2 0
0.3 0
0.4 0
0.5 0
0.6 0
0.7 0
0.8 0
0.9 0
1 0
X Y
100 0
90 3.1
80 5.75
70 8
60 9.77
50 11.25
40 12.15
30 12.25
20 11.45
10 9
7.5 8
5 6.85
2.5 5.5
2.1 5.3
1.6 4.9
1 4.4
0.6 4
0.3 3.65
0.05 3
0 2.25
0 2.25
0.05 2.1
0.3 1.7
0.6 1.4
1 1.1
1.6 0.75
2.1 0.55
2.5 0.37
5 0.2
7.5 0.1
10 0
20 0
30 0
40 0
50 0
60 0
70 0
80 0
90 0
100 0
V 1.1