
Winfoil Airfoils - Total Number: 277
Name | T/C % | T/C % Chord Position | Camber % | Camber Chord % | CL Max | CD Min |
---|---|---|---|---|---|---|
<< First < Prev 41 42 43 44 45 Next > Last >> | ||||||
PRD 2A | 12.95 | 30 | 3.852 | 40 | 1.744 | 0.0085 |
PRD 2B | 12.25 | 30 | 4.725 | 40 | 1.371 | 0.0023 |
PRD 2C | 8.66 | 30 | 3.399 | 30 | 1.091 | 0 |
RAE 2822 | 12.09 | 37.85 | 1.263 | 75.71 | 0.903 | 0.0066 |
RAE 5214 | 9.64 | 30.87 | 1.433 | 69.13 | 1.2 | 0.0042 |
Coordinates
XUpper | YUpper | XLower | YLower |
---|---|---|---|
0 | 4.15 | 0 | 4.15 |
0.6 | 5.73 | 0.6 | 3.27 |
2.5 | 7.24 | 2.5 | 2.25 |
5 | 8.63 | 5 | 1.51 |
7.5 | 9.64 | 7.5 | 1 |
10 | 10.5 | 10 | 0.7 |
20 | 12.62 | 20 | 0.5 |
30 | 13.17 | 30 | 0.2 |
40 | 12.65 | 40 | 0 |
50 | 11.57 | 50 | 0 |
60 | 9.82 | 60 | 0 |
70 | 8 | 70 | 0 |
80 | 5.77 | 80 | 0 |
90 | 3.11 | 90 | 0 |
100 | 0 | 100 | 0 |
X | Y |
---|---|
1 | 0 |
0.9 | 0.0311 |
0.8 | 0.0577 |
0.7 | 0.08 |
0.6 | 0.0982 |
0.5 | 0.1157 |
0.4 | 0.1265 |
0.3 | 0.1317 |
0.2 | 0.1262 |
0.1 | 0.105 |
0.075 | 0.0964 |
0.05 | 0.0863 |
0.025 | 0.0724 |
0.006 | 0.0573 |
0 | 0.0415 |
0 | 0.0415 |
0.006 | 0.0327 |
0.025 | 0.0225 |
0.05 | 0.0151 |
0.075 | 0.01 |
0.1 | 0.007 |
0.2 | 0.005 |
0.3 | 0.002 |
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 | 3.11 |
80 | 5.77 |
70 | 8 |
60 | 9.82 |
50 | 11.57 |
40 | 12.65 |
30 | 13.17 |
20 | 12.62 |
10 | 10.5 |
7.5 | 9.64 |
5 | 8.63 |
2.5 | 7.24 |
0.6 | 5.73 |
0 | 4.15 |
0 | 4.15 |
0.6 | 3.27 |
2.5 | 2.25 |
5 | 1.51 |
7.5 | 1 |
10 | 0.7 |
20 | 0.5 |
30 | 0.2 |
40 | 0 |
50 | 0 |
60 | 0 |
70 | 0 |
80 | 0 |
90 | 0 |
100 | 0 |
V 1.1