US1000ROOT (us1000root-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: US1000ROOT (us1000root-il) Reynolds number: 200,000 Max Cl/Cd: 49.15 at α=7.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-us1000root-il-200000.txt Download as CSV file: xf-us1000root-il-200000.csv |
XFOIL Version 6.96
Calculated polar for: US1000ROOT
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.500 -0.7853 0.16282 0.15870 0.0012 1.0000 0.0162
-19.250 -0.8015 0.15461 0.15035 -0.0036 1.0000 0.0159
-19.000 -0.8138 0.14769 0.14330 -0.0076 1.0000 0.0155
-18.750 -0.8295 0.14018 0.13564 -0.0119 1.0000 0.0152
-18.500 -0.8447 0.13301 0.12829 -0.0157 1.0000 0.0149
-18.250 -0.8585 0.12632 0.12142 -0.0192 1.0000 0.0145
-18.000 -0.8677 0.12069 0.11562 -0.0220 1.0000 0.0143
-17.750 -0.8788 0.11481 0.10952 -0.0247 1.0000 0.0138
-17.500 -0.8877 0.10941 0.10388 -0.0269 1.0000 0.0134
-17.250 -0.8880 0.10570 0.10003 -0.0281 1.0000 0.0133
-17.000 -0.8864 0.10227 0.09644 -0.0288 1.0000 0.0131
-16.750 -0.8824 0.09934 0.09336 -0.0292 1.0000 0.0128
-16.500 -0.8762 0.09695 0.09091 -0.0293 1.0000 0.0130
-16.250 -0.8681 0.09485 0.08872 -0.0291 1.0000 0.0128
-16.000 -0.8580 0.09321 0.08703 -0.0286 1.0000 0.0129
-15.750 -0.8476 0.09167 0.08546 -0.0281 1.0000 0.0130
-15.500 -0.8356 0.09036 0.08410 -0.0275 1.0000 0.0128
-15.250 -0.8255 0.08918 0.08297 -0.0265 1.0000 0.0133
-15.000 -0.8197 0.08698 0.08075 -0.0266 1.0000 0.0138
-14.750 -0.8147 0.08472 0.07849 -0.0265 1.0000 0.0144
-14.500 -0.8090 0.08254 0.07630 -0.0266 1.0000 0.0142
-14.250 -0.8087 0.07951 0.07324 -0.0271 1.0000 0.0147
-14.000 -0.8082 0.07643 0.07013 -0.0279 1.0000 0.0148
-13.750 -0.8099 0.07306 0.06671 -0.0287 1.0000 0.0146
-13.500 -0.8153 0.06923 0.06281 -0.0297 1.0000 0.0145
-13.250 -0.8251 0.06479 0.05830 -0.0309 1.0000 0.0153
-13.000 -0.8340 0.06051 0.05393 -0.0321 1.0000 0.0160
-12.750 -0.8378 0.05701 0.05033 -0.0330 1.0000 0.0149
-12.500 -0.8510 0.05238 0.04558 -0.0341 1.0000 0.0163
-12.250 -0.8588 0.04857 0.04165 -0.0350 1.0000 0.0157
-12.000 -0.8668 0.04485 0.03780 -0.0356 1.0000 0.0166
-11.750 -0.8735 0.04146 0.03427 -0.0359 1.0000 0.0172
-11.500 -0.8873 0.03764 0.03028 -0.0358 1.0000 0.0180
-11.250 -0.8968 0.03457 0.02706 -0.0350 1.0000 0.0189
-11.000 -0.9007 0.03223 0.02460 -0.0339 1.0000 0.0197
-10.750 -0.9045 0.03010 0.02235 -0.0322 1.0000 0.0215
-10.500 -0.9229 0.02725 0.01937 -0.0288 1.0000 0.0304
-10.250 -0.9453 0.02464 0.01685 -0.0241 1.0000 0.0473
-10.000 -0.9687 0.02248 0.01500 -0.0183 1.0000 0.0990
-9.750 -0.9913 0.02079 0.01370 -0.0113 1.0000 0.1453
-9.500 -1.0185 0.01975 0.01312 -0.0025 1.0000 0.2112
-9.250 -1.0181 0.01944 0.01287 0.0021 1.0000 0.2291
-9.000 -1.0171 0.01929 0.01270 0.0066 1.0000 0.2414
-8.750 -1.0231 0.01928 0.01262 0.0123 1.0000 0.2508
-8.500 -1.0283 0.01926 0.01261 0.0178 1.0000 0.2590
-8.250 -1.0239 0.01927 0.01250 0.0214 0.9993 0.2683
-8.000 -0.9837 0.01921 0.01235 0.0183 0.9923 0.2814
-7.750 -0.9467 0.01919 0.01228 0.0158 0.9839 0.2961
-7.500 -0.9109 0.01899 0.01213 0.0138 0.9755 0.3064
-7.250 -0.8735 0.01875 0.01184 0.0115 0.9681 0.3156
-7.000 -0.8370 0.01850 0.01147 0.0095 0.9603 0.3241
-6.750 -0.7974 0.01806 0.01103 0.0070 0.9538 0.3300
-6.500 -0.7581 0.01771 0.01063 0.0046 0.9472 0.3369
-6.250 -0.7138 0.01724 0.01011 0.0011 0.9430 0.3439
-6.000 -0.6753 0.01690 0.00974 -0.0011 0.9349 0.3504
-5.750 -0.6264 0.01643 0.00919 -0.0055 0.9302 0.3575
-5.500 -0.5812 0.01605 0.00882 -0.0091 0.9226 0.3642
-5.250 -0.5313 0.01563 0.00832 -0.0138 0.9155 0.3718
-5.000 -0.4883 0.01533 0.00802 -0.0169 0.9046 0.3789
-4.750 -0.4484 0.01506 0.00767 -0.0195 0.8926 0.3863
-4.500 -0.4129 0.01486 0.00747 -0.0210 0.8792 0.3934
-4.250 -0.3840 0.01471 0.00724 -0.0212 0.8650 0.4011
-4.000 -0.3573 0.01457 0.00710 -0.0209 0.8505 0.4085
-3.750 -0.3330 0.01442 0.00690 -0.0200 0.8358 0.4161
-3.500 -0.3093 0.01427 0.00673 -0.0190 0.8210 0.4238
-3.250 -0.2864 0.01409 0.00654 -0.0178 0.8061 0.4320
-3.000 -0.2646 0.01395 0.00636 -0.0163 0.7907 0.4414
-2.750 -0.2417 0.01376 0.00619 -0.0151 0.7751 0.4501
-2.500 -0.2199 0.01360 0.00598 -0.0137 0.7587 0.4603
-2.250 -0.1974 0.01344 0.00580 -0.0124 0.7419 0.4702
-2.000 -0.1744 0.01327 0.00563 -0.0112 0.7251 0.4803
-1.750 -0.1523 0.01314 0.00547 -0.0098 0.7074 0.4915
-1.500 -0.1310 0.01305 0.00534 -0.0083 0.6889 0.5036
-1.250 -0.1092 0.01295 0.00522 -0.0069 0.6704 0.5159
-1.000 -0.0871 0.01288 0.00513 -0.0056 0.6526 0.5284
-0.750 -0.0649 0.01283 0.00505 -0.0042 0.6353 0.5412
-0.500 -0.0435 0.01279 0.00501 -0.0028 0.6177 0.5547
-0.250 -0.0221 0.01276 0.00499 -0.0013 0.6008 0.5691
0.000 -0.0008 0.01276 0.00498 0.0002 0.5847 0.5845
0.250 0.0205 0.01276 0.00499 0.0017 0.5693 0.6008
0.500 0.0419 0.01279 0.00501 0.0031 0.5549 0.6175
0.750 0.0633 0.01283 0.00505 0.0046 0.5415 0.6352
1.000 0.0853 0.01288 0.00513 0.0059 0.5284 0.6524
1.250 0.1074 0.01295 0.00523 0.0073 0.5160 0.6704
1.500 0.1292 0.01304 0.00534 0.0087 0.5036 0.6888
1.750 0.1505 0.01314 0.00547 0.0102 0.4916 0.7074
2.000 0.1726 0.01327 0.00564 0.0116 0.4805 0.7252
2.250 0.1956 0.01343 0.00581 0.0128 0.4704 0.7421
2.500 0.2180 0.01359 0.00599 0.0141 0.4602 0.7588
2.750 0.2399 0.01375 0.00619 0.0155 0.4502 0.7749
3.000 0.2627 0.01395 0.00637 0.0168 0.4415 0.7907
3.250 0.2845 0.01409 0.00655 0.0182 0.4321 0.8061
3.500 0.3073 0.01426 0.00675 0.0194 0.4239 0.8212
3.750 0.3310 0.01441 0.00691 0.0205 0.4162 0.8361
4.000 0.3553 0.01456 0.00711 0.0213 0.4085 0.8506
4.250 0.3821 0.01470 0.00725 0.0216 0.4012 0.8653
4.500 0.4112 0.01485 0.00748 0.0214 0.3934 0.8794
4.750 0.4470 0.01505 0.00768 0.0198 0.3863 0.8927
5.000 0.4874 0.01532 0.00804 0.0172 0.3790 0.9047
5.250 0.5292 0.01553 0.00822 0.0142 0.3684 0.9158
5.500 0.5757 0.01574 0.00841 0.0103 0.3552 0.9236
5.750 0.6194 0.01592 0.00866 0.0069 0.3425 0.9313
6.000 0.6654 0.01625 0.00906 0.0031 0.3325 0.9370
6.250 0.7032 0.01650 0.00931 0.0010 0.3206 0.9449
6.500 0.7426 0.01670 0.00953 -0.0015 0.3037 0.9510
6.750 0.7783 0.01697 0.00981 -0.0034 0.2897 0.9593
7.000 0.8175 0.01732 0.01017 -0.0059 0.2793 0.9664
7.250 0.8537 0.01758 0.01049 -0.0080 0.2599 0.9748
7.500 0.8866 0.01804 0.01079 -0.0098 0.2235 0.9845
7.750 0.9065 0.01996 0.01192 -0.0108 0.1094 0.9951
8.000 0.8872 0.02204 0.01350 -0.0050 0.0254 1.0000
8.250 0.8780 0.02192 0.01345 0.0011 0.0297 1.0000
8.500 0.8560 0.02254 0.01405 0.0093 0.0208 1.0000
8.750 0.8497 0.02329 0.01484 0.0146 0.0179 1.0000
9.000 0.8510 0.02401 0.01564 0.0185 0.0166 1.0000
9.250 0.8545 0.02479 0.01651 0.0217 0.0161 1.0000
9.500 0.8575 0.02574 0.01755 0.0246 0.0157 1.0000
9.750 0.8595 0.02691 0.01882 0.0272 0.0150 1.0000
10.000 0.8610 0.02826 0.02028 0.0295 0.0144 1.0000
10.250 0.8618 0.02980 0.02194 0.0315 0.0140 1.0000
10.500 0.8627 0.03150 0.02378 0.0330 0.0140 1.0000
10.750 0.8628 0.03342 0.02580 0.0343 0.0138 1.0000
11.000 0.8592 0.03584 0.02835 0.0352 0.0136 1.0000
11.250 0.8547 0.03858 0.03121 0.0356 0.0134 1.0000
11.500 0.8435 0.04223 0.03500 0.0356 0.0131 1.0000
11.750 0.8385 0.04546 0.03835 0.0352 0.0131 1.0000
12.000 0.8324 0.04899 0.04198 0.0346 0.0131 1.0000
12.250 0.8253 0.05274 0.04585 0.0337 0.0131 1.0000
12.500 0.8165 0.05680 0.05000 0.0327 0.0131 1.0000
12.750 0.8032 0.06144 0.05472 0.0316 0.0128 1.0000
13.000 0.8002 0.06491 0.05825 0.0307 0.0129 1.0000
13.250 0.7972 0.06835 0.06176 0.0299 0.0130 1.0000
13.500 0.7940 0.07173 0.06516 0.0293 0.0129 1.0000
13.750 0.7945 0.07452 0.06795 0.0291 0.0127 1.0000
14.000 0.7991 0.07684 0.07028 0.0290 0.0128 1.0000
14.250 0.8052 0.07909 0.07258 0.0287 0.0129 1.0000
14.500 0.8142 0.08059 0.07407 0.0294 0.0128 1.0000
14.750 0.8251 0.08197 0.07546 0.0301 0.0129 1.0000
15.000 0.8358 0.08345 0.07698 0.0306 0.0129 1.0000
15.250 0.8492 0.08447 0.07801 0.0317 0.0129 1.0000
15.500 0.8578 0.08654 0.08017 0.0315 0.0132 1.0000
15.750 0.8699 0.08796 0.08166 0.0324 0.0134 1.0000
16.000 0.8790 0.08997 0.08378 0.0327 0.0136 1.0000
16.250 0.8856 0.09247 0.08642 0.0329 0.0140 1.0000
16.500 0.8882 0.09564 0.08976 0.0326 0.0144 1.0000
16.750 0.8887 0.09911 0.09335 0.0314 0.0146 1.0000
17.000 0.8862 0.10323 0.09765 0.0303 0.0150 1.0000
17.250 0.8820 0.10762 0.10219 0.0287 0.0153 1.0000
17.500 0.8754 0.11251 0.10724 0.0268 0.0157 1.0000
17.750 0.8666 0.11785 0.11274 0.0244 0.0160 1.0000
18.000 0.8579 0.12327 0.11830 0.0219 0.0163 1.0000
18.250 0.8481 0.12899 0.12416 0.0191 0.0167 1.0000
18.500 0.8376 0.13500 0.13030 0.0160 0.0169 1.0000
18.750 0.8511 0.13662 0.13194 0.0167 0.0179 1.0000
19.000 0.8394 0.14306 0.13853 0.0123 0.0182 1.0000
19.250 0.8166 0.15256 0.14827 0.0059 0.0188 1.0000
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