NASA SC(2)-0414 AIRFOIL (sc20414-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: NASA SC(2)-0414 AIRFOIL (sc20414-il) Reynolds number: 1,000,000 Max Cl/Cd: 78.82 at α=8.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-sc20414-il-1000000-n5.txt Download as CSV file: xf-sc20414-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NASA SC(2)-0414 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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.3443 0.08572 0.08180 -0.0361 1.0000 0.0190
-19.500 -1.3587 0.07982 0.07577 -0.0390 1.0000 0.0191
-19.250 -1.3696 0.07463 0.07046 -0.0415 1.0000 0.0192
-19.000 -1.3772 0.07003 0.06575 -0.0435 1.0000 0.0193
-18.750 -1.3820 0.06594 0.06155 -0.0453 1.0000 0.0193
-18.500 -1.3873 0.06193 0.05745 -0.0468 1.0000 0.0195
-18.250 -1.3927 0.05800 0.05342 -0.0483 1.0000 0.0197
-18.000 -1.3954 0.05455 0.04989 -0.0494 1.0000 0.0199
-17.750 -1.3955 0.05154 0.04680 -0.0502 1.0000 0.0200
-17.500 -1.3936 0.04884 0.04403 -0.0508 1.0000 0.0202
-17.250 -1.3901 0.04637 0.04150 -0.0513 1.0000 0.0204
-17.000 -1.3855 0.04410 0.03916 -0.0517 1.0000 0.0206
-16.750 -1.3794 0.04207 0.03707 -0.0519 1.0000 0.0208
-16.500 -1.3724 0.04016 0.03509 -0.0520 1.0000 0.0211
-16.250 -1.3645 0.03839 0.03327 -0.0520 1.0000 0.0213
-16.000 -1.3561 0.03675 0.03157 -0.0519 1.0000 0.0215
-15.750 -1.3470 0.03520 0.02997 -0.0518 1.0000 0.0218
-15.500 -1.3367 0.03379 0.02850 -0.0515 1.0000 0.0220
-15.250 -1.3261 0.03243 0.02708 -0.0513 1.0000 0.0222
-15.000 -1.3142 0.03118 0.02578 -0.0510 1.0000 0.0225
-14.750 -1.3019 0.02999 0.02453 -0.0507 1.0000 0.0227
-14.500 -1.2892 0.02885 0.02335 -0.0503 1.0000 0.0229
-14.250 -1.2776 0.02762 0.02208 -0.0499 1.0000 0.0233
-14.000 -1.2647 0.02652 0.02095 -0.0494 1.0000 0.0236
-13.750 -1.2508 0.02553 0.01993 -0.0489 1.0000 0.0240
-13.500 -1.2365 0.02459 0.01897 -0.0483 1.0000 0.0244
-13.250 -1.2217 0.02374 0.01809 -0.0477 1.0000 0.0249
-13.000 -1.2071 0.02292 0.01724 -0.0470 1.0000 0.0254
-12.750 -1.1930 0.02215 0.01645 -0.0460 1.0000 0.0258
-12.500 -1.1809 0.02144 0.01570 -0.0446 1.0000 0.0261
-12.250 -1.1740 0.02078 0.01501 -0.0421 1.0000 0.0264
-12.000 -1.1644 0.02009 0.01431 -0.0402 1.0000 0.0268
-11.750 -1.1526 0.01941 0.01361 -0.0386 1.0000 0.0273
-11.500 -1.1323 0.01875 0.01295 -0.0386 0.9994 0.0280
-11.250 -1.1032 0.01811 0.01230 -0.0401 0.9979 0.0287
-11.000 -1.0734 0.01752 0.01168 -0.0417 0.9963 0.0295
-10.750 -1.0427 0.01696 0.01111 -0.0434 0.9947 0.0302
-10.500 -1.0112 0.01641 0.01054 -0.0452 0.9934 0.0311
-10.250 -0.9803 0.01586 0.01000 -0.0469 0.9917 0.0323
-10.000 -0.9497 0.01536 0.00950 -0.0484 0.9895 0.0335
-9.750 -0.9180 0.01491 0.00904 -0.0500 0.9874 0.0345
-9.500 -0.8855 0.01447 0.00859 -0.0517 0.9856 0.0355
-9.250 -0.8528 0.01401 0.00814 -0.0535 0.9837 0.0369
-9.000 -0.8195 0.01361 0.00774 -0.0552 0.9819 0.0383
-8.750 -0.7880 0.01326 0.00738 -0.0565 0.9791 0.0397
-8.500 -0.7580 0.01290 0.00703 -0.0575 0.9751 0.0411
-8.250 -0.7265 0.01255 0.00669 -0.0588 0.9717 0.0430
-8.000 -0.6942 0.01223 0.00638 -0.0601 0.9686 0.0447
-7.750 -0.6637 0.01194 0.00608 -0.0610 0.9638 0.0462
-7.500 -0.6330 0.01162 0.00578 -0.0620 0.9583 0.0483
-7.000 -0.5718 0.01109 0.00526 -0.0638 0.9475 0.0527
-6.750 -0.5414 0.01082 0.00501 -0.0646 0.9417 0.0555
-6.500 -0.5111 0.01060 0.00478 -0.0653 0.9362 0.0580
-6.250 -0.4809 0.01037 0.00455 -0.0660 0.9296 0.0607
-6.000 -0.4506 0.01014 0.00434 -0.0667 0.9231 0.0642
-5.750 -0.4203 0.00993 0.00414 -0.0674 0.9166 0.0682
-5.500 -0.3898 0.00972 0.00395 -0.0681 0.9100 0.0732
-5.250 -0.3592 0.00952 0.00376 -0.0689 0.9041 0.0791
-5.000 -0.3284 0.00933 0.00359 -0.0697 0.8974 0.0856
-4.750 -0.2976 0.00913 0.00342 -0.0704 0.8901 0.0939
-4.500 -0.2666 0.00893 0.00326 -0.0712 0.8835 0.1024
-4.250 -0.2355 0.00875 0.00311 -0.0720 0.8765 0.1125
-3.750 -0.1726 0.00836 0.00282 -0.0738 0.8621 0.1428
-3.500 -0.1410 0.00816 0.00268 -0.0748 0.8542 0.1627
-3.250 -0.1085 0.00790 0.00253 -0.0760 0.8472 0.1945
-3.000 -0.0757 0.00762 0.00238 -0.0773 0.8389 0.2325
-2.750 -0.0421 0.00730 0.00222 -0.0789 0.8292 0.2827
-2.500 -0.0071 0.00685 0.00201 -0.0809 0.8138 0.3604
-2.250 0.0281 0.00644 0.00181 -0.0829 0.7974 0.4368
-2.000 0.0631 0.00608 0.00169 -0.0847 0.7820 0.5154
-1.750 0.0946 0.00603 0.00168 -0.0855 0.7633 0.5496
-1.500 0.1248 0.00609 0.00168 -0.0858 0.7404 0.5687
-1.250 0.1550 0.00615 0.00169 -0.0862 0.7164 0.5837
-1.000 0.1849 0.00624 0.00171 -0.0864 0.6896 0.5947
-0.750 0.2140 0.00643 0.00175 -0.0866 0.6468 0.6040
-0.500 0.2430 0.00665 0.00179 -0.0867 0.6007 0.6116
-0.250 0.2704 0.00711 0.00193 -0.0866 0.5124 0.6195
0.000 0.2980 0.00758 0.00208 -0.0867 0.4282 0.6254
0.250 0.3258 0.00801 0.00221 -0.0867 0.3560 0.6293
0.500 0.3539 0.00838 0.00236 -0.0868 0.2942 0.6326
0.750 0.3822 0.00872 0.00249 -0.0869 0.2435 0.6357
1.000 0.4106 0.00902 0.00261 -0.0870 0.2044 0.6389
1.250 0.4393 0.00928 0.00273 -0.0871 0.1739 0.6416
1.500 0.4683 0.00948 0.00283 -0.0873 0.1543 0.6434
1.750 0.4973 0.00968 0.00294 -0.0874 0.1370 0.6448
2.000 0.5261 0.00987 0.00305 -0.0876 0.1219 0.6463
2.250 0.5550 0.01005 0.00318 -0.0877 0.1102 0.6480
2.750 0.6126 0.01040 0.00344 -0.0879 0.0920 0.6512
3.000 0.6414 0.01058 0.00358 -0.0880 0.0860 0.6528
3.250 0.6701 0.01075 0.00373 -0.0881 0.0813 0.6545
3.500 0.6987 0.01093 0.00388 -0.0881 0.0770 0.6561
3.750 0.7274 0.01110 0.00403 -0.0882 0.0728 0.6577
4.000 0.7558 0.01130 0.00420 -0.0882 0.0684 0.6594
4.250 0.7842 0.01149 0.00436 -0.0882 0.0648 0.6610
4.500 0.8124 0.01170 0.00453 -0.0882 0.0610 0.6624
4.750 0.8406 0.01189 0.00471 -0.0882 0.0579 0.6641
5.000 0.8685 0.01211 0.00491 -0.0881 0.0546 0.6661
5.250 0.8965 0.01231 0.00512 -0.0880 0.0525 0.6681
5.500 0.9243 0.01253 0.00534 -0.0879 0.0502 0.6699
5.750 0.9517 0.01278 0.00557 -0.0878 0.0480 0.6717
6.000 0.9794 0.01300 0.00580 -0.0877 0.0464 0.6733
6.250 1.0067 0.01324 0.00603 -0.0875 0.0445 0.6750
6.500 1.0337 0.01351 0.00629 -0.0873 0.0426 0.6767
6.750 1.0608 0.01376 0.00655 -0.0871 0.0413 0.6784
7.000 1.0878 0.01402 0.00681 -0.0868 0.0400 0.6800
7.500 1.1408 0.01460 0.00739 -0.0862 0.0372 0.6835
7.750 1.1673 0.01488 0.00769 -0.0859 0.0362 0.6853
8.000 1.1935 0.01516 0.00800 -0.0856 0.0350 0.6870
8.250 1.2194 0.01547 0.00831 -0.0852 0.0338 0.6888
8.500 1.2448 0.01582 0.00866 -0.0847 0.0327 0.6907
8.750 1.2702 0.01615 0.00902 -0.0842 0.0319 0.6925
9.000 1.2956 0.01648 0.00937 -0.0837 0.0311 0.6944
9.250 1.3205 0.01683 0.00974 -0.0832 0.0303 0.6961
9.500 1.3451 0.01719 0.01011 -0.0826 0.0295 0.6978
9.750 1.3692 0.01759 0.01052 -0.0819 0.0287 0.6992
10.000 1.3927 0.01804 0.01097 -0.0811 0.0279 0.7007
10.250 1.4167 0.01840 0.01139 -0.0804 0.0274 0.7029
10.500 1.4401 0.01879 0.01182 -0.0797 0.0268 0.7051
10.750 1.4630 0.01921 0.01228 -0.0788 0.0262 0.7072
11.000 1.4853 0.01966 0.01276 -0.0779 0.0257 0.7094
11.250 1.5070 0.02013 0.01326 -0.0769 0.0252 0.7114
11.500 1.5280 0.02065 0.01380 -0.0758 0.0247 0.7134
11.750 1.5478 0.02122 0.01441 -0.0745 0.0242 0.7153
12.000 1.5678 0.02173 0.01496 -0.0732 0.0239 0.7171
12.250 1.5870 0.02224 0.01552 -0.0718 0.0236 0.7187
12.500 1.6050 0.02278 0.01612 -0.0702 0.0233 0.7206
12.750 1.6216 0.02334 0.01675 -0.0684 0.0230 0.7227
13.000 1.6349 0.02392 0.01739 -0.0660 0.0227 0.7249
13.250 1.6478 0.02457 0.01810 -0.0637 0.0224 0.7271
13.500 1.6613 0.02529 0.01887 -0.0616 0.0221 0.7293
13.750 1.6744 0.02605 0.01969 -0.0595 0.0218 0.7316
14.000 1.6868 0.02689 0.02058 -0.0575 0.0215 0.7338
14.250 1.6982 0.02782 0.02156 -0.0554 0.0212 0.7360
14.500 1.7083 0.02887 0.02266 -0.0533 0.0209 0.7378
14.750 1.7172 0.03002 0.02389 -0.0512 0.0205 0.7401
15.000 1.7276 0.03108 0.02504 -0.0494 0.0204 0.7427
15.250 1.7375 0.03223 0.02628 -0.0477 0.0203 0.7454
15.500 1.7462 0.03349 0.02763 -0.0460 0.0201 0.7481
15.750 1.7541 0.03488 0.02910 -0.0443 0.0199 0.7506
16.000 1.7611 0.03638 0.03068 -0.0428 0.0198 0.7529
16.250 1.7670 0.03802 0.03240 -0.0413 0.0196 0.7549
16.500 1.7721 0.03979 0.03427 -0.0400 0.0194 0.7569
16.750 1.7760 0.04174 0.03632 -0.0388 0.0193 0.7592
17.000 1.7786 0.04389 0.03857 -0.0378 0.0191 0.7615
17.250 1.7797 0.04625 0.04103 -0.0369 0.0190 0.7638
17.500 1.7794 0.04888 0.04376 -0.0363 0.0188 0.7661
17.750 1.7776 0.05177 0.04675 -0.0358 0.0187 0.7684
18.000 1.7736 0.05504 0.05013 -0.0357 0.0186 0.7705
18.250 1.7678 0.05871 0.05391 -0.0359 0.0184 0.7724
18.500 1.7596 0.06291 0.05824 -0.0367 0.0183 0.7743
18.750 1.7487 0.06773 0.06319 -0.0380 0.0182 0.7764
19.000 1.7340 0.07336 0.06897 -0.0399 0.0181 0.7784
19.250 1.7147 0.08009 0.07586 -0.0428 0.0181 0.7802
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