S1014 (s1014-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: S1014 (s1014-il) Reynolds number: 500,000 Max Cl/Cd: 45.76 at α=4.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-s1014-il-500000.txt Download as CSV file: xf-s1014-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: S1014
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.0958 0.09511 0.09113 -0.0437 1.0000 0.0236
-19.500 -1.1058 0.08962 0.08549 -0.0467 1.0000 0.0239
-19.250 -1.1134 0.08464 0.08038 -0.0493 1.0000 0.0240
-19.000 -1.1204 0.07993 0.07554 -0.0517 1.0000 0.0243
-18.750 -1.1288 0.07537 0.07092 -0.0536 1.0000 0.0248
-18.500 -1.1342 0.07118 0.06667 -0.0554 1.0000 0.0252
-18.250 -1.1367 0.06739 0.06281 -0.0571 1.0000 0.0256
-18.000 -1.1388 0.06387 0.05921 -0.0586 0.9585 0.0261
-17.750 -1.1273 0.06002 0.05519 -0.0630 0.9325 0.0267
-17.500 -1.1218 0.05701 0.05198 -0.0649 0.9132 0.0274
-17.250 -1.1205 0.05434 0.04914 -0.0653 0.9023 0.0279
-17.000 -1.1177 0.05197 0.04659 -0.0655 0.8947 0.0284
-16.750 -1.1177 0.04937 0.04385 -0.0655 0.8896 0.0291
-16.500 -1.1186 0.04679 0.04122 -0.0653 0.8852 0.0298
-16.250 -1.1150 0.04474 0.03908 -0.0650 0.8813 0.0304
-16.000 -1.1097 0.04294 0.03719 -0.0646 0.8779 0.0311
-15.750 -1.1029 0.04125 0.03542 -0.0642 0.8751 0.0320
-15.500 -1.0945 0.03976 0.03382 -0.0637 0.8724 0.0330
-15.250 -1.0844 0.03844 0.03238 -0.0632 0.8699 0.0339
-15.000 -1.0817 0.03656 0.03044 -0.0622 0.8676 0.0349
-14.750 -1.0750 0.03510 0.02895 -0.0613 0.8654 0.0360
-14.500 -1.0644 0.03398 0.02776 -0.0605 0.8633 0.0373
-14.250 -1.0531 0.03293 0.02663 -0.0597 0.8614 0.0387
-14.000 -1.0399 0.03197 0.02557 -0.0590 0.8599 0.0398
-13.750 -1.0330 0.03057 0.02414 -0.0578 0.8583 0.0414
-13.500 -1.0219 0.02953 0.02309 -0.0568 0.8567 0.0430
-13.250 -1.0083 0.02869 0.02220 -0.0560 0.8551 0.0445
-13.000 -0.9923 0.02802 0.02145 -0.0553 0.8534 0.0464
-12.750 -0.9815 0.02700 0.02039 -0.0541 0.8518 0.0484
-12.500 -0.9689 0.02613 0.01951 -0.0530 0.8503 0.0504
-12.250 -0.9526 0.02551 0.01885 -0.0522 0.8490 0.0526
-12.000 -0.9355 0.02495 0.01821 -0.0514 0.8478 0.0546
-11.750 -0.9236 0.02407 0.01730 -0.0501 0.8466 0.0570
-11.500 -0.9082 0.02344 0.01667 -0.0491 0.8454 0.0597
-11.250 -0.8900 0.02295 0.01614 -0.0484 0.8445 0.0624
-11.000 -0.8728 0.02238 0.01553 -0.0476 0.8436 0.0649
-10.750 -0.8586 0.02164 0.01482 -0.0464 0.8427 0.0682
-10.500 -0.8403 0.02116 0.01433 -0.0456 0.8418 0.0716
-10.250 -0.8199 0.02080 0.01390 -0.0451 0.8409 0.0744
-10.000 -0.8058 0.02008 0.01323 -0.0438 0.8398 0.0787
-9.750 -0.7871 0.01965 0.01280 -0.0430 0.8389 0.0831
-9.500 -0.7676 0.01926 0.01237 -0.0422 0.8380 0.0867
-9.250 -0.7516 0.01868 0.01184 -0.0410 0.8371 0.0920
-9.000 -0.7321 0.01831 0.01145 -0.0403 0.8362 0.0969
-8.750 -0.7148 0.01783 0.01099 -0.0392 0.8351 0.1028
-8.500 -0.6962 0.01744 0.01061 -0.0382 0.8341 0.1089
-8.250 -0.6778 0.01704 0.01020 -0.0372 0.8332 0.1154
-8.000 -0.6595 0.01664 0.00984 -0.0362 0.8324 0.1228
-7.750 -0.6413 0.01626 0.00948 -0.0351 0.8316 0.1311
-7.500 -0.6224 0.01593 0.00916 -0.0341 0.8309 0.1403
-7.250 -0.6053 0.01553 0.00883 -0.0329 0.8301 0.1513
-7.000 -0.5877 0.01518 0.00853 -0.0316 0.8294 0.1634
-6.750 -0.5704 0.01486 0.00827 -0.0303 0.8286 0.1776
-6.500 -0.5536 0.01447 0.00796 -0.0290 0.8280 0.1944
-6.250 -0.5378 0.01405 0.00765 -0.0275 0.8273 0.2157
-6.000 -0.5236 0.01361 0.00734 -0.0257 0.8262 0.2404
-5.750 -0.5119 0.01318 0.00706 -0.0235 0.8251 0.2699
-5.500 -0.5046 0.01281 0.00685 -0.0203 0.8240 0.3036
-5.250 -0.5004 0.01246 0.00670 -0.0164 0.8228 0.3428
-5.000 -0.4939 0.01202 0.00650 -0.0130 0.8217 0.3940
-4.750 -0.4881 0.01149 0.00626 -0.0094 0.8202 0.4571
-4.500 -0.4826 0.01087 0.00601 -0.0056 0.8187 0.5330
-4.250 -0.4745 0.01037 0.00602 -0.0020 0.8176 0.6290
-4.000 -0.4501 0.01068 0.00654 -0.0011 0.8168 0.6877
-3.750 -0.4237 0.01092 0.00675 -0.0008 0.8159 0.7087
-3.500 -0.3963 0.01118 0.00697 -0.0006 0.8150 0.7205
-3.250 -0.3700 0.01144 0.00716 -0.0003 0.8142 0.7306
-3.000 -0.3404 0.01183 0.00756 -0.0005 0.8136 0.7372
-2.750 -0.3149 0.01210 0.00776 -0.0001 0.8126 0.7449
-2.500 -0.2851 0.01248 0.00817 -0.0003 0.8116 0.7490
-2.250 -0.2558 0.01283 0.00855 -0.0007 0.8104 0.7534
-2.000 -0.2292 0.01310 0.00881 -0.0007 0.8085 0.7590
-1.750 -0.2028 0.01331 0.00901 -0.0006 0.8066 0.7633
-1.500 -0.1734 0.01361 0.00934 -0.0008 0.8048 0.7662
-1.250 -0.1441 0.01393 0.00968 -0.0009 0.8032 0.7699
-1.000 -0.1162 0.01416 0.00991 -0.0008 0.8016 0.7750
-0.750 -0.0886 0.01433 0.01007 -0.0006 0.8001 0.7804
-0.500 -0.0561 0.01481 0.01060 -0.0006 0.7988 0.7845
-0.250 -0.0249 0.01518 0.01099 -0.0005 0.7974 0.7892
0.000 0.0000 0.01525 0.01099 0.0000 0.7952 0.7952
0.250 0.0249 0.01518 0.01099 0.0005 0.7892 0.7974
0.500 0.0561 0.01481 0.01060 0.0006 0.7845 0.7988
0.750 0.0885 0.01434 0.01007 0.0006 0.7804 0.8001
1.000 0.1162 0.01417 0.00991 0.0008 0.7750 0.8016
1.250 0.1441 0.01393 0.00968 0.0009 0.7700 0.8032
1.500 0.1734 0.01361 0.00933 0.0008 0.7662 0.8048
1.750 0.2027 0.01331 0.00901 0.0006 0.7634 0.8066
2.000 0.2291 0.01310 0.00881 0.0007 0.7589 0.8085
2.250 0.2558 0.01283 0.00855 0.0007 0.7534 0.8104
2.500 0.2851 0.01248 0.00816 0.0003 0.7489 0.8116
2.750 0.3149 0.01210 0.00776 0.0001 0.7449 0.8126
3.000 0.3404 0.01183 0.00757 0.0005 0.7372 0.8136
3.250 0.3700 0.01144 0.00716 0.0003 0.7306 0.8142
3.500 0.3963 0.01119 0.00698 0.0006 0.7206 0.8150
3.750 0.4237 0.01092 0.00675 0.0008 0.7086 0.8159
4.000 0.4501 0.01068 0.00655 0.0010 0.6881 0.8168
4.250 0.4745 0.01037 0.00603 0.0020 0.6296 0.8176
4.500 0.4831 0.01086 0.00600 0.0055 0.5351 0.8187
4.750 0.4881 0.01149 0.00626 0.0094 0.4570 0.8202
5.000 0.4939 0.01202 0.00650 0.0130 0.3941 0.8217
5.250 0.5003 0.01246 0.00670 0.0164 0.3426 0.8228
5.500 0.5044 0.01281 0.00685 0.0203 0.3029 0.8240
5.750 0.5119 0.01318 0.00706 0.0234 0.2697 0.8251
6.000 0.5235 0.01361 0.00734 0.0257 0.2401 0.8262
6.250 0.5379 0.01405 0.00765 0.0275 0.2156 0.8273
6.500 0.5537 0.01447 0.00796 0.0290 0.1944 0.8280
6.750 0.5705 0.01486 0.00827 0.0303 0.1774 0.8286
7.000 0.5877 0.01519 0.00853 0.0316 0.1630 0.8294
7.250 0.6054 0.01553 0.00883 0.0328 0.1512 0.8301
7.500 0.6225 0.01592 0.00917 0.0341 0.1402 0.8309
7.750 0.6414 0.01626 0.00948 0.0351 0.1310 0.8317
8.000 0.6597 0.01664 0.00984 0.0362 0.1229 0.8324
8.250 0.6780 0.01703 0.01020 0.0372 0.1154 0.8332
8.500 0.6964 0.01743 0.01060 0.0382 0.1089 0.8341
8.750 0.7150 0.01783 0.01098 0.0391 0.1026 0.8352
9.000 0.7322 0.01832 0.01145 0.0403 0.0970 0.8362
9.250 0.7518 0.01868 0.01183 0.0410 0.0921 0.8371
9.500 0.7679 0.01925 0.01236 0.0422 0.0867 0.8380
9.750 0.7874 0.01964 0.01279 0.0429 0.0829 0.8389
10.000 0.8062 0.02007 0.01322 0.0437 0.0789 0.8399
10.250 0.8204 0.02077 0.01388 0.0450 0.0743 0.8409
10.500 0.8405 0.02115 0.01432 0.0456 0.0716 0.8418
10.750 0.8589 0.02164 0.01482 0.0464 0.0682 0.8427
11.000 0.8729 0.02238 0.01553 0.0475 0.0648 0.8436
11.250 0.8905 0.02294 0.01613 0.0483 0.0624 0.8445
11.500 0.9088 0.02342 0.01665 0.0490 0.0596 0.8455
11.750 0.9242 0.02405 0.01728 0.0500 0.0570 0.8466
12.000 0.9360 0.02494 0.01820 0.0514 0.0545 0.8479
12.250 0.9534 0.02548 0.01882 0.0521 0.0525 0.8491
12.500 0.9694 0.02612 0.01950 0.0529 0.0504 0.8503
12.750 0.9816 0.02701 0.02039 0.0541 0.0483 0.8518
13.000 0.9928 0.02800 0.02143 0.0553 0.0464 0.8535
13.250 1.0083 0.02871 0.02222 0.0560 0.0447 0.8552
13.500 1.0220 0.02956 0.02311 0.0568 0.0429 0.8567
13.750 1.0334 0.03057 0.02414 0.0578 0.0415 0.8583
14.000 1.0409 0.03192 0.02552 0.0590 0.0398 0.8599
14.250 1.0538 0.03290 0.02660 0.0597 0.0386 0.8614
14.500 1.0654 0.03393 0.02771 0.0604 0.0373 0.8634
14.750 1.0763 0.03501 0.02886 0.0612 0.0360 0.8655
15.000 1.0828 0.03650 0.03038 0.0621 0.0349 0.8677
15.250 1.0866 0.03828 0.03223 0.0630 0.0337 0.8701
15.500 1.0965 0.03961 0.03367 0.0636 0.0329 0.8726
15.750 1.1042 0.04117 0.03534 0.0641 0.0320 0.8753
16.000 1.1108 0.04287 0.03712 0.0645 0.0312 0.8781
16.250 1.1159 0.04469 0.03903 0.0649 0.0304 0.8815
16.500 1.1190 0.04678 0.04119 0.0652 0.0297 0.8856
16.750 1.1188 0.04927 0.04376 0.0654 0.0291 0.8901
17.000 1.1194 0.05182 0.04643 0.0654 0.0285 0.8954
17.250 1.1222 0.05419 0.04899 0.0652 0.0278 0.9032
17.500 1.1240 0.05681 0.05178 0.0648 0.0273 0.9149
17.750 1.1304 0.05992 0.05509 0.0626 0.0266 0.9352
18.000 1.1418 0.06381 0.05915 0.0581 0.0260 0.9648
18.250 1.1387 0.06727 0.06268 0.0569 0.0256 1.0000
18.500 1.1363 0.07104 0.06652 0.0552 0.0252 1.0000
18.750 1.1307 0.07525 0.07079 0.0534 0.0248 1.0000
19.000 1.1232 0.07971 0.07531 0.0515 0.0243 1.0000
19.250 1.1157 0.08444 0.08017 0.0493 0.0241 1.0000
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