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| Original file line number | Diff line number | Diff line change |
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| @@ -0,0 +1,17 @@ | ||
| Round root section with a Cd of 0.60 | ||
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| 1 Number of airfoil tables in this file | ||
| 1.0 Reynolds numbers in millions | ||
| 0.0 Control setting | ||
| 0.0 Stall angle (deg) | ||
| 0.0 Zero lift angle of attack (deg) | ||
| 0.0 Cn slope for zero lift (dimensionless) | ||
| 0.0 Cn at stall value for positive angle of attack | ||
| 0.0 Cn at stall value for negative angle of attack | ||
| 0.0 Angle of attack for minimum CD (deg) | ||
| 0.60 Minimum CD value | ||
| -180.00 0.000 0.6000 0.000 | ||
| 0.00 0.000 0.6000 0.000 | ||
| 180.00 0.000 0.6000 0.000 | ||
| EOT |
This file contains bidirectional Unicode text that may be interpreted or compiled differently than what appears below. To review, open the file in an editor that reveals hidden Unicode characters.
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| Original file line number | Diff line number | Diff line change |
|---|---|---|
| @@ -0,0 +1,159 @@ | ||
| DU00-W2-350 | ||
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| 1 Number of airfoil tables in this file | ||
| 1.0 Reynolds numbers in millions | ||
| 0.0 Control setting | ||
| 10.0 Stall angle (deg) | ||
| -8.0 Zero Cn angle of attack (deg) | ||
| 7.0 Cn slope for zero lift (dimensionless) | ||
| 1.4 Cn at stall value for positive angle of attack | ||
| -0.5 Cn at stall value for negative angle of attack | ||
| 0.0 Angle of attack for minimum CD (deg) | ||
| 0.10 Minimum CD value | ||
| -180.0 0.000 0.000 0.000 | ||
| -175.0 0.217 0.054 0.200 | ||
| -170.0 0.433 0.107 0.400 | ||
| -165.0 0.620 0.163 0.212 | ||
| -160.0 0.806 0.219 0.024 | ||
| -155.0 0.763 0.314 0.048 | ||
| -150.0 0.719 0.409 0.072 | ||
| -145.0 0.695 0.525 0.094 | ||
| -140.0 0.670 0.640 0.116 | ||
| -135.0 0.636 0.763 0.140 | ||
| -130.0 0.601 0.886 0.163 | ||
| -125.0 0.548 1.001 0.187 | ||
| -120.0 0.494 1.116 0.211 | ||
| -115.0 0.422 1.208 0.234 | ||
| -110.0 0.350 1.301 0.256 | ||
| -105.0 0.265 1.360 0.273 | ||
| -100.0 0.180 1.418 0.291 | ||
| -95.0 0.090 1.436 0.301 | ||
| -90.0 0.000 1.453 0.312 | ||
| -85.0 -0.090 1.436 0.316 | ||
| -80.0 -0.180 1.418 0.320 | ||
| -75.0 -0.265 1.360 0.316 | ||
| -70.0 -0.350 1.301 0.312 | ||
| -65.0 -0.422 1.208 0.302 | ||
| -60.0 -0.494 1.116 0.292 | ||
| -55.0 -0.548 1.001 0.279 | ||
| -50.0 -0.601 0.886 0.267 | ||
| -45.0 -0.640 0.764 0.254 | ||
| -40.0 -0.670 0.640 0.244 | ||
| -38.0 -0.681 0.592 0.240 | ||
| -36.0 -0.691 0.544 0.238 | ||
| -34.0 -0.700 0.498 0.237 | ||
| -32.0 -0.709 0.452 0.237 | ||
| -30.0 -0.719 0.409 0.238 | ||
| -28.0 -0.730 0.366 0.242 | ||
| -26.0 -0.743 0.326 0.247 | ||
| -24.0 -0.759 0.288 0.257 | ||
| -22.0 -0.780 0.252 0.270 | ||
| -20.0 -0.806 0.219 0.289 | ||
| -19.0 -0.791 0.204 0.265 | ||
| -18.0 -0.776 0.188 0.241 | ||
| -17.0 -0.761 0.173 0.218 | ||
| -16.0 -0.746 0.157 0.194 | ||
| -15.0 -0.731 0.142 0.170 | ||
| -14.0 -0.716 0.126 0.146 | ||
| -13.5 -0.709 0.118 0.134 | ||
| -13.0 -0.701 0.111 0.122 | ||
| -12.5 -0.694 0.103 0.110 | ||
| -12.0 -0.686 0.095 0.098 | ||
| -11.5 -0.679 0.087 0.086 | ||
| -11.0 -0.671 0.080 0.075 | ||
| -10.5 -0.664 0.072 0.063 | ||
| -10.0 -0.656 0.064 0.051 | ||
| -9.5 -0.649 0.056 0.039 | ||
| -9.0 -0.641 0.049 0.027 | ||
| -8.5 -0.634 0.041 0.015 | ||
| -8.0 -0.626 0.033 0.003 | ||
| -7.5 -0.584 0.029 -0.001 | ||
| -7.0 -0.541 0.026 -0.005 | ||
| -6.5 -0.494 0.023 -0.010 | ||
| -6.0 -0.447 0.020 -0.014 | ||
| -5.5 -0.396 0.018 -0.019 | ||
| -5.0 -0.344 0.016 -0.023 | ||
| -4.5 -0.289 0.014 -0.028 | ||
| -4.0 -0.233 0.013 -0.033 | ||
| -3.5 -0.174 0.012 -0.038 | ||
| -3.0 -0.115 0.012 -0.043 | ||
| -2.5 -0.054 0.011 -0.048 | ||
| -2.0 0.007 0.011 -0.052 | ||
| -1.5 0.070 0.011 -0.056 | ||
| -1.0 0.133 0.010 -0.060 | ||
| -0.5 0.197 0.010 -0.064 | ||
| 0.0 0.261 0.010 -0.068 | ||
| 0.5 0.326 0.010 -0.072 | ||
| 1.0 0.391 0.010 -0.075 | ||
| 1.5 0.457 0.010 -0.079 | ||
| 2.0 0.522 0.010 -0.082 | ||
| 2.5 0.587 0.011 -0.085 | ||
| 3.0 0.652 0.011 -0.087 | ||
| 3.5 0.716 0.011 -0.089 | ||
| 4.0 0.779 0.011 -0.091 | ||
| 4.5 0.841 0.012 -0.093 | ||
| 5.0 0.902 0.012 -0.095 | ||
| 5.5 0.961 0.012 -0.097 | ||
| 6.0 1.020 0.013 -0.098 | ||
| 6.5 1.075 0.013 -0.099 | ||
| 7.0 1.129 0.014 -0.100 | ||
| 7.5 1.178 0.015 -0.101 | ||
| 8.0 1.227 0.015 -0.102 | ||
| 8.5 1.268 0.016 -0.103 | ||
| 9.0 1.308 0.017 -0.104 | ||
| 9.5 1.339 0.020 -0.105 | ||
| 10.0 1.369 0.022 -0.106 | ||
| 10.5 1.381 0.026 -0.107 | ||
| 11.0 1.393 0.029 -0.107 | ||
| 11.5 1.368 0.035 -0.108 | ||
| 12.0 1.342 0.041 -0.108 | ||
| 12.5 1.317 0.050 -0.109 | ||
| 13.0 1.291 0.059 -0.109 | ||
| 13.5 1.270 0.069 -0.109 | ||
| 14.0 1.249 0.080 -0.109 | ||
| 15.0 1.211 0.103 -0.110 | ||
| 16.0 1.188 0.130 -0.119 | ||
| 17.0 1.172 0.154 -0.132 | ||
| 18.0 1.165 0.179 -0.143 | ||
| 19.0 1.176 0.203 -0.148 | ||
| 20.0 1.152 0.219 -0.157 | ||
| 22.0 1.114 0.252 -0.172 | ||
| 24.0 1.084 0.288 -0.184 | ||
| 26.0 1.062 0.326 -0.196 | ||
| 28.0 1.043 0.366 -0.206 | ||
| 30.0 1.027 0.409 -0.215 | ||
| 32.0 1.013 0.452 -0.224 | ||
| 34.0 1.000 0.498 -0.233 | ||
| 36.0 0.986 0.544 -0.242 | ||
| 38.0 0.973 0.592 -0.250 | ||
| 40.0 0.958 0.640 -0.259 | ||
| 45.0 0.914 0.764 -0.279 | ||
| 50.0 0.859 0.886 -0.299 | ||
| 55.0 0.782 1.001 -0.318 | ||
| 60.0 0.706 1.116 -0.337 | ||
| 65.0 0.603 1.208 -0.354 | ||
| 70.0 0.500 1.301 -0.371 | ||
| 75.0 0.378 1.360 -0.384 | ||
| 80.0 0.257 1.418 -0.397 | ||
| 85.0 0.128 1.436 -0.406 | ||
| 90.0 0.000 1.453 -0.415 | ||
| 95.0 -0.090 1.436 -0.419 | ||
| 100.0 -0.180 1.418 -0.423 | ||
| 105.0 -0.265 1.360 -0.419 | ||
| 110.0 -0.350 1.301 -0.415 | ||
| 115.0 -0.422 1.208 -0.405 | ||
| 120.0 -0.494 1.116 -0.395 | ||
| 125.0 -0.548 1.001 -0.383 | ||
| 130.0 -0.601 0.886 -0.370 | ||
| 135.0 -0.636 0.763 -0.358 | ||
| 140.0 -0.670 0.640 -0.347 | ||
| 145.0 -0.695 0.525 -0.344 | ||
| 150.0 -0.719 0.409 -0.341 | ||
| 155.0 -0.763 0.314 -0.367 | ||
| 160.0 -0.806 0.219 -0.392 | ||
| 165.0 -0.605 0.164 -0.446 | ||
| 170.0 -0.403 0.110 -0.500 | ||
| 175.0 -0.202 0.055 -0.250 | ||
| 180.0 0.000 0.000 0.000 | ||
| EOT |
This file contains bidirectional Unicode text that may be interpreted or compiled differently than what appears below. To review, open the file in an editor that reveals hidden Unicode characters.
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| Original file line number | Diff line number | Diff line change |
|---|---|---|
| @@ -0,0 +1,159 @@ | ||
| DU08-W-210 | ||
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| 1 Number of airfoil tables in this file | ||
| 1.0 Reynolds numbers in millions | ||
| 0.0 Control setting | ||
| 10.0 Stall angle (deg) | ||
| -4.0 Zero lift angle of attack (deg) | ||
| 7.0 Cn slope for zero lift (dimensionless) | ||
| 1.4 Cn at stall value for positive angle of attack | ||
| -0.5 Cn at stall value for negative angle of attack | ||
| 0.0 Angle of attack for minimum CD (deg) | ||
| 0.006 Minimum CD value | ||
| -180.0 0.000 0.000 0.000 | ||
| -175.0 0.250 0.038 0.200 | ||
| -170.0 0.501 0.075 0.400 | ||
| -165.0 0.655 0.124 0.150 | ||
| -160.0 0.809 0.172 -0.099 | ||
| -155.0 0.764 0.269 -0.066 | ||
| -150.0 0.720 0.365 -0.033 | ||
| -145.0 0.696 0.484 -0.008 | ||
| -140.0 0.671 0.602 0.018 | ||
| -135.0 0.636 0.728 0.043 | ||
| -130.0 0.601 0.854 0.069 | ||
| -125.0 0.548 0.973 0.095 | ||
| -120.0 0.494 1.091 0.122 | ||
| -115.0 0.422 1.188 0.147 | ||
| -110.0 0.350 1.284 0.172 | ||
| -105.0 0.265 1.347 0.193 | ||
| -100.0 0.180 1.410 0.215 | ||
| -95.0 0.090 1.431 0.229 | ||
| -90.0 0.000 1.453 0.244 | ||
| -85.0 -0.090 1.431 0.250 | ||
| -80.0 -0.180 1.410 0.256 | ||
| -75.0 -0.265 1.347 0.254 | ||
| -70.0 -0.350 1.284 0.251 | ||
| -65.0 -0.422 1.188 0.243 | ||
| -60.0 -0.494 1.091 0.235 | ||
| -55.0 -0.548 0.973 0.223 | ||
| -50.0 -0.601 0.854 0.212 | ||
| -45.0 -0.641 0.728 0.202 | ||
| -40.0 -0.671 0.602 0.194 | ||
| -38.0 -0.682 0.553 0.192 | ||
| -36.0 -0.691 0.504 0.191 | ||
| -34.0 -0.701 0.456 0.191 | ||
| -32.0 -0.710 0.410 0.193 | ||
| -30.0 -0.720 0.365 0.196 | ||
| -28.0 -0.731 0.322 0.203 | ||
| -26.0 -0.745 0.282 0.212 | ||
| -24.0 -0.761 0.243 0.225 | ||
| -22.0 -0.781 0.206 0.243 | ||
| -20.0 -0.809 0.172 0.269 | ||
| -19.0 -0.825 0.156 0.286 | ||
| -18.0 -0.820 0.141 0.280 | ||
| -17.0 -0.814 0.128 0.266 | ||
| -16.0 -0.782 0.115 0.227 | ||
| -15.0 -0.751 0.102 0.187 | ||
| -14.0 -0.720 0.088 0.147 | ||
| -13.5 -0.704 0.082 0.127 | ||
| -13.0 -0.688 0.075 0.108 | ||
| -12.5 -0.673 0.069 0.088 | ||
| -12.0 -0.657 0.062 0.068 | ||
| -11.5 -0.641 0.055 0.048 | ||
| -11.0 -0.626 0.049 0.028 | ||
| -10.5 -0.610 0.042 0.008 | ||
| -10.0 -0.594 0.036 -0.012 | ||
| -9.5 -0.579 0.029 -0.031 | ||
| -9.0 -0.563 0.022 -0.051 | ||
| -8.5 -0.536 0.017 -0.069 | ||
| -8.0 -0.508 0.012 -0.086 | ||
| -7.5 -0.437 0.010 -0.095 | ||
| -7.0 -0.366 0.009 -0.103 | ||
| -6.5 -0.304 0.008 -0.105 | ||
| -6.0 -0.242 0.007 -0.107 | ||
| -5.5 -0.180 0.007 -0.109 | ||
| -5.0 -0.119 0.007 -0.110 | ||
| -4.5 -0.058 0.007 -0.112 | ||
| -4.0 0.003 0.006 -0.113 | ||
| -3.5 0.064 0.006 -0.114 | ||
| -3.0 0.124 0.006 -0.116 | ||
| -2.5 0.185 0.006 -0.117 | ||
| -2.0 0.245 0.006 -0.118 | ||
| -1.5 0.305 0.006 -0.119 | ||
| -1.0 0.365 0.006 -0.120 | ||
| -0.5 0.425 0.006 -0.121 | ||
| 0.0 0.485 0.006 -0.122 | ||
| 0.5 0.545 0.006 -0.124 | ||
| 1.0 0.604 0.006 -0.125 | ||
| 1.5 0.664 0.007 -0.125 | ||
| 2.0 0.723 0.007 -0.126 | ||
| 2.5 0.782 0.007 -0.127 | ||
| 3.0 0.841 0.007 -0.128 | ||
| 3.5 0.900 0.007 -0.129 | ||
| 4.0 0.959 0.007 -0.130 | ||
| 4.5 1.017 0.007 -0.131 | ||
| 5.0 1.075 0.007 -0.131 | ||
| 5.5 1.132 0.007 -0.132 | ||
| 6.0 1.188 0.008 -0.133 | ||
| 6.5 1.242 0.008 -0.133 | ||
| 7.0 1.291 0.009 -0.132 | ||
| 7.5 1.333 0.011 -0.130 | ||
| 8.0 1.373 0.012 -0.128 | ||
| 8.5 1.412 0.013 -0.126 | ||
| 9.0 1.451 0.015 -0.124 | ||
| 9.5 1.489 0.016 -0.122 | ||
| 10.0 1.516 0.017 -0.122 | ||
| 10.5 1.542 0.018 -0.122 | ||
| 11.0 1.563 0.020 -0.122 | ||
| 11.5 1.580 0.022 -0.122 | ||
| 12.0 1.587 0.035 -0.124 | ||
| 12.5 1.549 0.049 -0.125 | ||
| 13.0 1.510 0.062 -0.127 | ||
| 13.5 1.460 0.076 -0.129 | ||
| 14.0 1.410 0.089 -0.130 | ||
| 15.0 1.340 0.103 -0.132 | ||
| 16.0 1.300 0.116 -0.133 | ||
| 17.0 1.260 0.130 -0.135 | ||
| 18.0 1.200 0.143 -0.137 | ||
| 19.0 1.179 0.156 -0.138 | ||
| 20.0 1.155 0.172 -0.148 | ||
| 22.0 1.116 0.206 -0.172 | ||
| 24.0 1.087 0.243 -0.192 | ||
| 26.0 1.064 0.282 -0.208 | ||
| 28.0 1.045 0.322 -0.223 | ||
| 30.0 1.029 0.365 -0.236 | ||
| 32.0 1.015 0.410 -0.248 | ||
| 34.0 1.001 0.456 -0.259 | ||
| 36.0 0.988 0.504 -0.270 | ||
| 38.0 0.974 0.553 -0.280 | ||
| 40.0 0.959 0.602 -0.291 | ||
| 45.0 0.915 0.728 -0.315 | ||
| 50.0 0.859 0.854 -0.338 | ||
| 55.0 0.783 0.973 -0.361 | ||
| 60.0 0.706 1.091 -0.383 | ||
| 65.0 0.603 1.188 -0.403 | ||
| 70.0 0.500 1.284 -0.423 | ||
| 75.0 0.378 1.347 -0.440 | ||
| 80.0 0.257 1.410 -0.457 | ||
| 85.0 0.128 1.431 -0.470 | ||
| 90.0 0.000 1.453 -0.483 | ||
| 95.0 -0.090 1.431 -0.489 | ||
| 100.0 -0.180 1.410 -0.495 | ||
| 105.0 -0.265 1.347 -0.493 | ||
| 110.0 -0.350 1.284 -0.491 | ||
| 115.0 -0.422 1.188 -0.483 | ||
| 120.0 -0.494 1.091 -0.474 | ||
| 125.0 -0.548 0.973 -0.463 | ||
| 130.0 -0.601 0.854 -0.452 | ||
| 135.0 -0.636 0.728 -0.442 | ||
| 140.0 -0.671 0.602 -0.433 | ||
| 145.0 -0.696 0.484 -0.435 | ||
| 150.0 -0.720 0.365 -0.436 | ||
| 155.0 -0.764 0.269 -0.472 | ||
| 160.0 -0.809 0.172 -0.509 | ||
| 165.0 -0.639 0.125 -0.504 | ||
| 170.0 -0.469 0.078 -0.500 | ||
| 175.0 -0.235 0.039 -0.250 | ||
| 180.0 0.000 0.000 0.000 | ||
| EOT |
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