NASA SC(2)-0714 AIRFOIL (sc20714-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: NASA SC(2)-0714 AIRFOIL (sc20714-il) Reynolds number: 1,000,000 Max Cl/Cd: 81.19 at α=-0.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-sc20714-il-1000000.txt Download as CSV file: xf-sc20714-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: NASA SC(2)-0714 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.1686 0.08321 0.07959 -0.0638 1.0000 0.0235
-19.500 -1.1791 0.07802 0.07429 -0.0664 1.0000 0.0236
-19.250 -1.1874 0.07324 0.06939 -0.0688 1.0000 0.0237
-19.000 -1.1933 0.06892 0.06497 -0.0709 1.0000 0.0239
-18.750 -1.1977 0.06495 0.06090 -0.0727 1.0000 0.0240
-18.500 -1.1999 0.06137 0.05722 -0.0742 1.0000 0.0241
-18.250 -1.2001 0.05816 0.05391 -0.0755 1.0000 0.0242
-18.000 -1.1988 0.05527 0.05093 -0.0765 1.0000 0.0243
-17.750 -1.2060 0.05161 0.04718 -0.0774 1.0000 0.0246
-17.500 -1.2099 0.04849 0.04398 -0.0780 1.0000 0.0249
-17.250 -1.2096 0.04596 0.04140 -0.0782 1.0000 0.0252
-17.000 -1.2071 0.04378 0.03918 -0.0782 1.0000 0.0254
-16.750 -1.2039 0.04183 0.03718 -0.0780 1.0000 0.0257
-16.500 -1.1998 0.04011 0.03541 -0.0774 1.0000 0.0259
-16.250 -1.1962 0.03848 0.03373 -0.0766 1.0000 0.0262
-16.000 -1.1927 0.03701 0.03221 -0.0755 1.0000 0.0264
-15.750 -1.1903 0.03564 0.03079 -0.0741 1.0000 0.0266
-15.500 -1.1889 0.03439 0.02950 -0.0722 1.0000 0.0269
-15.250 -1.1883 0.03322 0.02829 -0.0700 1.0000 0.0271
-15.000 -1.1882 0.03214 0.02715 -0.0676 1.0000 0.0274
-14.750 -1.1887 0.03112 0.02608 -0.0650 1.0000 0.0276
-14.500 -1.1896 0.03018 0.02509 -0.0621 1.0000 0.0278
-14.250 -1.1911 0.02929 0.02416 -0.0590 1.0000 0.0280
-14.000 -1.1701 0.02832 0.02312 -0.0600 0.9990 0.0282
-13.750 -1.1556 0.02668 0.02143 -0.0610 0.9972 0.0288
-13.500 -1.1368 0.02550 0.02023 -0.0620 0.9956 0.0294
-13.250 -1.1155 0.02457 0.01928 -0.0630 0.9942 0.0299
-13.000 -1.0909 0.02376 0.01844 -0.0644 0.9931 0.0305
-12.750 -1.0688 0.02299 0.01764 -0.0650 0.9910 0.0310
-12.500 -1.0440 0.02225 0.01688 -0.0661 0.9888 0.0317
-12.250 -1.0164 0.02160 0.01618 -0.0675 0.9871 0.0322
-12.000 -0.9884 0.02085 0.01539 -0.0691 0.9856 0.0329
-11.750 -0.9601 0.01985 0.01439 -0.0713 0.9843 0.0339
-11.500 -0.9291 0.01919 0.01373 -0.0734 0.9834 0.0348
-11.250 -0.8971 0.01863 0.01315 -0.0755 0.9827 0.0357
-11.000 -0.8648 0.01811 0.01261 -0.0775 0.9822 0.0366
-10.750 -0.8318 0.01768 0.01215 -0.0795 0.9816 0.0373
-10.500 -0.7988 0.01683 0.01130 -0.0823 0.9811 0.0389
-10.250 -0.7760 0.01634 0.01081 -0.0823 0.9776 0.0400
-10.000 -0.7453 0.01591 0.01038 -0.0838 0.9759 0.0413
-9.750 -0.7129 0.01552 0.00997 -0.0855 0.9747 0.0425
-9.500 -0.6791 0.01488 0.00933 -0.0880 0.9737 0.0442
-9.250 -0.6449 0.01442 0.00889 -0.0902 0.9729 0.0460
-9.000 -0.6104 0.01405 0.00851 -0.0923 0.9723 0.0476
-8.750 -0.5752 0.01367 0.00812 -0.0945 0.9718 0.0491
-8.500 -0.5391 0.01319 0.00767 -0.0971 0.9713 0.0517
-8.250 -0.5033 0.01286 0.00736 -0.0994 0.9709 0.0539
-8.000 -0.4671 0.01252 0.00701 -0.1018 0.9706 0.0560
-7.750 -0.4305 0.01211 0.00664 -0.1043 0.9702 0.0592
-7.500 -0.3947 0.01182 0.00635 -0.1065 0.9697 0.0620
-7.250 -0.3578 0.01144 0.00600 -0.1090 0.9693 0.0662
-7.000 -0.3214 0.01114 0.00572 -0.1113 0.9688 0.0705
-6.750 -0.2845 0.01079 0.00543 -0.1137 0.9682 0.0770
-6.500 -0.2508 0.01051 0.00520 -0.1154 0.9669 0.0846
-6.250 -0.2207 0.01029 0.00502 -0.1162 0.9644 0.0930
-6.000 -0.1868 0.01000 0.00479 -0.1179 0.9627 0.1043
-5.750 -0.1510 0.00964 0.00455 -0.1202 0.9615 0.1232
-5.500 -0.1149 0.00930 0.00433 -0.1224 0.9603 0.1486
-5.250 -0.0771 0.00888 0.00409 -0.1251 0.9594 0.1868
-5.000 -0.0376 0.00839 0.00382 -0.1283 0.9587 0.2393
-4.750 0.0065 0.00768 0.00348 -0.1329 0.9584 0.3330
-4.500 0.0527 0.00690 0.00313 -0.1380 0.9583 0.4475
-4.250 0.0935 0.00644 0.00300 -0.1413 0.9577 0.5398
-4.000 0.1272 0.00635 0.00295 -0.1425 0.9560 0.5661
-3.750 0.1598 0.00630 0.00290 -0.1432 0.9533 0.5815
-3.500 0.1874 0.00624 0.00287 -0.1429 0.9475 0.5920
-3.250 0.2175 0.00615 0.00276 -0.1430 0.9419 0.6017
-3.000 0.2465 0.00610 0.00272 -0.1428 0.9357 0.6089
-2.750 0.2750 0.00604 0.00264 -0.1426 0.9275 0.6136
-2.500 0.3055 0.00603 0.00256 -0.1428 0.9216 0.6172
-2.250 0.3335 0.00599 0.00257 -0.1425 0.9126 0.6224
-2.000 0.3624 0.00604 0.00259 -0.1423 0.9030 0.6283
-1.750 0.3915 0.00612 0.00264 -0.1422 0.8923 0.6338
-1.500 0.4207 0.00611 0.00263 -0.1422 0.8812 0.6377
-1.250 0.4495 0.00614 0.00264 -0.1420 0.8667 0.6403
-1.000 0.4775 0.00625 0.00272 -0.1417 0.8486 0.6444
-0.750 0.5056 0.00640 0.00280 -0.1414 0.8249 0.6486
-0.500 0.5334 0.00657 0.00281 -0.1410 0.7892 0.6506
-0.250 0.5582 0.00696 0.00288 -0.1401 0.7185 0.6519
0.000 0.5788 0.00773 0.00307 -0.1385 0.5937 0.6532
0.250 0.6005 0.00847 0.00330 -0.1374 0.4740 0.6553
0.500 0.6239 0.00912 0.00355 -0.1365 0.3814 0.6572
0.750 0.6476 0.00975 0.00381 -0.1357 0.2953 0.6589
1.000 0.6727 0.01026 0.00403 -0.1352 0.2302 0.6604
1.250 0.6985 0.01070 0.00423 -0.1348 0.1803 0.6616
1.500 0.7252 0.01105 0.00442 -0.1345 0.1475 0.6627
1.750 0.7525 0.01133 0.00459 -0.1343 0.1263 0.6639
2.000 0.7798 0.01161 0.00476 -0.1341 0.1076 0.6651
2.250 0.8071 0.01188 0.00495 -0.1339 0.0941 0.6663
2.500 0.8347 0.01211 0.00512 -0.1338 0.0846 0.6675
2.750 0.8621 0.01237 0.00532 -0.1336 0.0770 0.6687
3.000 0.8893 0.01263 0.00552 -0.1333 0.0713 0.6697
3.250 0.9168 0.01286 0.00573 -0.1332 0.0675 0.6706
3.500 0.9442 0.01307 0.00592 -0.1330 0.0642 0.6717
3.750 0.9709 0.01334 0.00617 -0.1326 0.0610 0.6733
4.000 0.9984 0.01351 0.00636 -0.1324 0.0593 0.6746
4.250 1.0252 0.01374 0.00658 -0.1321 0.0572 0.6758
4.500 1.0514 0.01404 0.00686 -0.1317 0.0547 0.6770
4.750 1.0778 0.01429 0.00712 -0.1313 0.0531 0.6782
5.000 1.1044 0.01451 0.00736 -0.1309 0.0515 0.6794
5.250 1.1306 0.01477 0.00762 -0.1304 0.0499 0.6806
5.500 1.1556 0.01515 0.00797 -0.1298 0.0478 0.6819
5.750 1.1815 0.01542 0.00826 -0.1293 0.0466 0.6833
6.000 1.2074 0.01568 0.00854 -0.1287 0.0452 0.6848
6.250 1.2327 0.01598 0.00883 -0.1282 0.0437 0.6861
6.500 1.2561 0.01649 0.00932 -0.1272 0.0416 0.6874
6.750 1.2818 0.01671 0.00957 -0.1267 0.0406 0.6884
7.000 1.3068 0.01701 0.00988 -0.1260 0.0393 0.6893
7.250 1.3312 0.01734 0.01021 -0.1253 0.0380 0.6904
7.500 1.3533 0.01788 0.01074 -0.1242 0.0365 0.6924
7.750 1.3775 0.01817 0.01109 -0.1234 0.0357 0.6940
8.000 1.4012 0.01849 0.01145 -0.1225 0.0348 0.6955
8.250 1.4243 0.01885 0.01183 -0.1215 0.0339 0.6969
8.500 1.4466 0.01924 0.01224 -0.1204 0.0330 0.6984
8.750 1.4667 0.01980 0.01281 -0.1189 0.0320 0.6998
9.000 1.4869 0.02030 0.01335 -0.1174 0.0313 0.7014
9.250 1.5081 0.02068 0.01377 -0.1160 0.0307 0.7031
9.500 1.5283 0.02110 0.01423 -0.1145 0.0301 0.7048
9.750 1.5477 0.02156 0.01472 -0.1129 0.0295 0.7064
10.000 1.5661 0.02204 0.01523 -0.1111 0.0290 0.7078
10.250 1.5805 0.02258 0.01579 -0.1086 0.0285 0.7089
10.500 1.5942 0.02327 0.01652 -0.1061 0.0279 0.7106
10.750 1.6060 0.02418 0.01749 -0.1033 0.0273 0.7128
11.000 1.6227 0.02476 0.01814 -0.1014 0.0271 0.7147
11.250 1.6383 0.02540 0.01885 -0.0993 0.0268 0.7164
11.500 1.6534 0.02609 0.01962 -0.0972 0.0264 0.7181
11.750 1.6676 0.02684 0.02043 -0.0950 0.0261 0.7199
12.000 1.6813 0.02763 0.02128 -0.0929 0.0258 0.7218
12.250 1.6944 0.02846 0.02217 -0.0907 0.0254 0.7236
12.500 1.7070 0.02934 0.02311 -0.0884 0.0251 0.7255
12.750 1.7183 0.03030 0.02412 -0.0861 0.0249 0.7273
13.000 1.7286 0.03136 0.02524 -0.0838 0.0246 0.7287
13.250 1.7370 0.03258 0.02652 -0.0814 0.0242 0.7311
13.500 1.7408 0.03415 0.02817 -0.0785 0.0239 0.7332
13.750 1.7397 0.03618 0.03032 -0.0753 0.0235 0.7349
14.000 1.7486 0.03744 0.03168 -0.0732 0.0234 0.7368
14.250 1.7563 0.03882 0.03314 -0.0712 0.0232 0.7388
14.500 1.7627 0.04034 0.03477 -0.0692 0.0231 0.7408
14.750 1.7678 0.04204 0.03656 -0.0672 0.0229 0.7428
15.000 1.7714 0.04392 0.03854 -0.0653 0.0227 0.7446
15.250 1.7735 0.04598 0.04070 -0.0635 0.0226 0.7462
15.500 1.7747 0.04821 0.04304 -0.0618 0.0224 0.7476
15.750 1.7743 0.05070 0.04564 -0.0604 0.0223 0.7499
16.000 1.7734 0.05336 0.04842 -0.0592 0.0221 0.7519
16.250 1.7707 0.05636 0.05154 -0.0583 0.0219 0.7537
16.500 1.7672 0.05960 0.05489 -0.0577 0.0218 0.7556
16.750 1.7617 0.06328 0.05869 -0.0575 0.0217 0.7575
17.000 1.7551 0.06733 0.06286 -0.0578 0.0216 0.7593
17.250 1.7466 0.07186 0.06751 -0.0585 0.0215 0.7611
17.500 1.7358 0.07696 0.07274 -0.0598 0.0214 0.7626
17.750 1.7224 0.08271 0.07862 -0.0618 0.0213 0.7639
18.000 1.7070 0.08905 0.08510 -0.0644 0.0212 0.7649
18.250 1.6882 0.09621 0.09241 -0.0677 0.0211 0.7660
18.500 1.6675 0.10392 0.10028 -0.0717 0.0211 0.7673
18.750 1.6434 0.11238 0.10890 -0.0763 0.0210 0.7683
19.000 1.6181 0.12127 0.11795 -0.0814 0.0210 0.7691
19.250 1.5917 0.13056 0.12740 -0.0871 0.0210 0.7699
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