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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 28 29 30 31 32 Next > Last >>
NACA 2213 12.93 1.987 20.6285 1.452 0.0095
NACA 23012 11.97 1.835 15 1.173 0.0072
NACA 23015 14.97 1.831 15 1.48 0.0116
NACA 23018 17.96 1.835 15 1.275 0.0132
NACA 23021 20.95 1.846 10 1.121 0.0046
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.3376 1.558 0.8946 -1.3154
1.964 3.2237 2.9342 -2.3041
4.8789 4.8957 6.0291 -3.0115
9.0383 6.4177 10.0749 -3.5084
14.3489 7.601 14.9628 -3.8866
20.6285 8.2531 20.6236 -4.2534
27.3499 8.467 27.2905 -4.5005
34.632 8.3868 34.5144 -4.5195
42.2923 8.035 42.1205 -4.3432
50.1392 7.4502 49.924 -4.0139
57.9774 6.681 57.7347 -3.5766
65.6128 5.7808 65.3611 -3.074
72.8572 4.8042 72.6151 -2.5424
79.5331 3.8049 79.317 -2.012
85.4776 2.836 85.3001 -1.5083
90.5467 1.9496 90.4144 -1.0542
94.6182 1.1955 94.5312 -0.6714
97.5946 0.6194 97.5461 -0.3801
99.4051 0.2582 99.3825 -0.1978
100.0068 0.1363 99.9931 -0.1363
X Y
1.000068 0.001363
0.994051 0.002582
0.975946 0.006194
0.946182 0.011955
0.905467 0.019496
0.854776 0.02836
0.795331 0.038049
0.728572 0.048042
0.656128 0.057808
0.579774 0.06681
0.501392 0.074502
0.422923 0.08035
0.34632 0.083868
0.273499 0.08467
0.206285 0.082531
0.143489 0.07601
0.090383 0.064177
0.048789 0.048957
0.01964 0.032237
0.003376 0.01558
0 0
0 0
0.008946 -0.013154
0.029342 -0.023041
0.060291 -0.030115
0.100749 -0.035084
0.149628 -0.038866
0.206236 -0.042534
0.272905 -0.045005
0.345144 -0.045195
0.421205 -0.043432
0.49924 -0.040139
0.577347 -0.035766
0.653611 -0.03074
0.726151 -0.025424
0.79317 -0.02012
0.853001 -0.015083
0.904144 -0.010542
0.945312 -0.006714
0.975461 -0.003801
0.993825 -0.001978
0.999931 -0.001363
X Y
100.0068 0.1363
99.4051 0.2582
97.5946 0.6194
94.6182 1.1955
90.5467 1.9496
85.4776 2.836
79.5331 3.8049
72.8572 4.8042
65.6128 5.7808
57.9774 6.681
50.1392 7.4502
42.2923 8.035
34.632 8.3868
27.3499 8.467
20.6285 8.2531
14.3489 7.601
9.0383 6.4177
4.8789 4.8957
1.964 3.2237
0.3376 1.558
0 0
0 0
0.8946 -1.3154
2.9342 -2.3041
6.0291 -3.0115
10.0749 -3.5084
14.9628 -3.8866
20.6236 -4.2534
27.2905 -4.5005
34.5144 -4.5195
42.1205 -4.3432
49.924 -4.0139
57.7347 -3.5766
65.3611 -3.074
72.6151 -2.5424
79.317 -2.012
85.3001 -1.5083
90.4144 -1.0542
94.5312 -0.6714
97.5461 -0.3801
99.3825 -0.1978
99.9931 -0.1363
V 1.1