WORTMANN FX 76-120 (fx76120-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: WORTMANN FX 76-120 (fx76120-il) Reynolds number: 200,000 Max Cl/Cd: 49.29 at α=6.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx76120-il-200000.txt Download as CSV file: xf-fx76120-il-200000.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 76-120
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
------ -------- --------- --------- -------- -------- --------
-15.250 -0.8257 0.10872 0.10456 -0.0190 1.0000 0.0443
-15.000 -0.8777 0.09393 0.08966 -0.0279 1.0000 0.0434
-14.750 -0.9248 0.08151 0.07704 -0.0364 1.0000 0.0426
-14.500 -0.9638 0.07185 0.06715 -0.0431 1.0000 0.0422
-14.250 -0.9934 0.06474 0.05981 -0.0473 1.0000 0.0420
-14.000 -1.0189 0.05891 0.05374 -0.0498 1.0000 0.0418
-13.750 -1.0386 0.05443 0.04903 -0.0507 1.0000 0.0419
-13.500 -1.0555 0.05063 0.04499 -0.0505 1.0000 0.0421
-13.250 -1.0705 0.04759 0.04170 -0.0493 1.0000 0.0427
-13.000 -1.0817 0.04506 0.03892 -0.0472 1.0000 0.0432
-12.750 -1.0920 0.04288 0.03648 -0.0443 1.0000 0.0437
-12.500 -1.1019 0.04145 0.03478 -0.0404 1.0000 0.0442
-12.250 -1.0949 0.03846 0.03175 -0.0391 1.0000 0.0457
-12.000 -1.0869 0.03716 0.03044 -0.0369 1.0000 0.0469
-11.750 -1.0807 0.03573 0.02889 -0.0344 1.0000 0.0479
-11.500 -1.0728 0.03431 0.02732 -0.0320 1.0000 0.0494
-11.250 -1.0641 0.03295 0.02574 -0.0296 1.0000 0.0508
-11.000 -1.0561 0.03197 0.02450 -0.0268 1.0000 0.0523
-10.750 -1.0402 0.02980 0.02234 -0.0258 1.0000 0.0544
-10.500 -1.0254 0.02877 0.02130 -0.0241 1.0000 0.0564
-10.250 -1.0106 0.02770 0.02012 -0.0222 1.0000 0.0585
-10.000 -0.9960 0.02678 0.01902 -0.0201 1.0000 0.0608
-9.750 -0.9801 0.02530 0.01750 -0.0185 1.0000 0.0634
-9.500 -0.9644 0.02438 0.01662 -0.0167 1.0000 0.0663
-9.250 -0.9482 0.02356 0.01573 -0.0148 1.0000 0.0696
-9.000 -0.9318 0.02267 0.01472 -0.0129 1.0000 0.0728
-8.750 -0.9170 0.02161 0.01374 -0.0109 1.0000 0.0767
-8.500 -0.9006 0.02092 0.01300 -0.0089 1.0000 0.0813
-8.250 -0.8859 0.01999 0.01208 -0.0067 1.0000 0.0863
-8.000 -0.8703 0.01933 0.01143 -0.0046 1.0000 0.0925
-7.750 -0.8558 0.01853 0.01066 -0.0023 1.0000 0.0999
-7.500 -0.8392 0.01798 0.01006 -0.0002 1.0000 0.1091
-7.250 -0.8248 0.01729 0.00946 0.0021 1.0000 0.1212
-7.000 -0.8093 0.01672 0.00895 0.0043 1.0000 0.1361
-6.750 -0.7936 0.01621 0.00850 0.0065 1.0000 0.1529
-6.500 -0.7773 0.01577 0.00815 0.0086 1.0000 0.1699
-6.250 -0.7602 0.01542 0.00784 0.0105 1.0000 0.1866
-6.000 -0.7426 0.01511 0.00755 0.0124 1.0000 0.2023
-5.750 -0.7246 0.01483 0.00727 0.0142 1.0000 0.2173
-5.500 -0.7062 0.01457 0.00702 0.0159 1.0000 0.2317
-5.250 -0.6876 0.01434 0.00680 0.0176 1.0000 0.2463
-5.000 -0.6689 0.01411 0.00659 0.0192 1.0000 0.2606
-4.750 -0.6503 0.01387 0.00639 0.0209 1.0000 0.2755
-4.500 -0.6317 0.01363 0.00621 0.0225 1.0000 0.2910
-4.250 -0.6131 0.01341 0.00605 0.0241 1.0000 0.3075
-4.000 -0.5945 0.01319 0.00589 0.0257 1.0000 0.3252
-3.750 -0.5762 0.01297 0.00576 0.0273 1.0000 0.3443
-3.500 -0.5583 0.01274 0.00565 0.0290 1.0000 0.3654
-3.250 -0.5405 0.01255 0.00557 0.0306 1.0000 0.3898
-3.000 -0.4994 0.01238 0.00558 0.0276 0.9940 0.4277
-2.750 -0.4586 0.01216 0.00560 0.0247 0.9877 0.4711
-2.500 -0.4202 0.01190 0.00560 0.0224 0.9804 0.5206
-2.250 -0.3831 0.01165 0.00558 0.0206 0.9725 0.5738
-2.000 -0.3448 0.01138 0.00556 0.0186 0.9643 0.6280
-1.750 -0.3011 0.01111 0.00554 0.0158 0.9573 0.6810
-1.500 -0.2643 0.01087 0.00549 0.0145 0.9474 0.7285
-1.250 -0.2177 0.01068 0.00547 0.0114 0.9415 0.7710
-1.000 -0.1778 0.01055 0.00545 0.0098 0.9323 0.8054
-0.750 -0.1251 0.01044 0.00541 0.0056 0.9278 0.8346
-0.500 -0.0874 0.01037 0.00539 0.0045 0.9160 0.8590
-0.250 -0.0459 0.01031 0.00535 0.0027 0.9047 0.8787
0.000 -0.0005 0.01028 0.00533 0.0001 0.8937 0.8943
0.250 0.0457 0.01032 0.00536 -0.0026 0.8789 0.9049
0.500 0.0874 0.01037 0.00539 -0.0045 0.8592 0.9160
0.750 0.1254 0.01044 0.00542 -0.0056 0.8346 0.9279
1.000 0.1780 0.01055 0.00545 -0.0098 0.8055 0.9323
1.250 0.2178 0.01068 0.00547 -0.0115 0.7709 0.9413
1.750 0.3010 0.01111 0.00553 -0.0158 0.6809 0.9573
2.000 0.3446 0.01138 0.00556 -0.0186 0.6279 0.9642
2.250 0.3830 0.01164 0.00558 -0.0205 0.5736 0.9724
2.500 0.4203 0.01190 0.00559 -0.0224 0.5205 0.9804
2.750 0.4586 0.01216 0.00560 -0.0247 0.4710 0.9877
3.000 0.4990 0.01238 0.00558 -0.0275 0.4279 0.9939
3.250 0.5405 0.01255 0.00557 -0.0306 0.3899 1.0000
3.500 0.5583 0.01274 0.00565 -0.0290 0.3655 1.0000
3.750 0.5762 0.01297 0.00576 -0.0273 0.3449 1.0000
4.000 0.5945 0.01319 0.00589 -0.0257 0.3254 1.0000
4.250 0.6130 0.01340 0.00604 -0.0241 0.3073 1.0000
4.500 0.6317 0.01363 0.00621 -0.0225 0.2910 1.0000
4.750 0.6503 0.01386 0.00639 -0.0208 0.2755 1.0000
5.000 0.6688 0.01412 0.00659 -0.0192 0.2609 1.0000
5.250 0.6875 0.01434 0.00679 -0.0176 0.2463 1.0000
5.500 0.7062 0.01457 0.00702 -0.0159 0.2318 1.0000
5.750 0.7246 0.01482 0.00727 -0.0142 0.2174 1.0000
6.000 0.7425 0.01511 0.00755 -0.0124 0.2023 1.0000
6.250 0.7601 0.01542 0.00783 -0.0105 0.1865 1.0000
6.500 0.7773 0.01577 0.00814 -0.0086 0.1700 1.0000
6.750 0.7935 0.01621 0.00851 -0.0065 0.1529 1.0000
7.000 0.8092 0.01673 0.00895 -0.0043 0.1362 1.0000
7.250 0.8247 0.01730 0.00947 -0.0021 0.1213 1.0000
7.500 0.8394 0.01796 0.01005 0.0002 0.1094 1.0000
7.750 0.8558 0.01853 0.01065 0.0023 0.0998 1.0000
8.000 0.8704 0.01931 0.01141 0.0046 0.0925 1.0000
8.250 0.8859 0.01998 0.01207 0.0067 0.0863 1.0000
8.500 0.9006 0.02092 0.01300 0.0089 0.0813 1.0000
8.750 0.9170 0.02161 0.01374 0.0109 0.0767 1.0000
9.000 0.9316 0.02271 0.01475 0.0129 0.0726 1.0000
9.250 0.9481 0.02355 0.01572 0.0148 0.0694 1.0000
9.500 0.9644 0.02438 0.01662 0.0167 0.0663 1.0000
9.750 0.9802 0.02531 0.01751 0.0185 0.0634 1.0000
10.000 0.9961 0.02678 0.01903 0.0201 0.0608 1.0000
10.250 1.0108 0.02771 0.02013 0.0221 0.0585 1.0000
10.500 1.0252 0.02873 0.02125 0.0241 0.0562 1.0000
10.750 1.0403 0.02981 0.02235 0.0257 0.0544 1.0000
11.000 1.0561 0.03196 0.02450 0.0269 0.0522 1.0000
11.250 1.0647 0.03299 0.02578 0.0295 0.0509 1.0000
11.500 1.0729 0.03434 0.02735 0.0320 0.0493 1.0000
11.750 1.0812 0.03578 0.02895 0.0343 0.0481 1.0000
12.000 1.0874 0.03710 0.03036 0.0369 0.0468 1.0000
12.250 1.0968 0.03840 0.03164 0.0388 0.0454 1.0000
12.500 1.1024 0.04152 0.03487 0.0403 0.0443 1.0000
12.750 1.0923 0.04289 0.03650 0.0443 0.0437 1.0000
13.000 1.0832 0.04525 0.03911 0.0470 0.0434 1.0000
13.250 1.0705 0.04766 0.04178 0.0492 0.0427 1.0000
13.500 1.0563 0.05070 0.04505 0.0504 0.0422 1.0000
13.750 1.0397 0.05438 0.04898 0.0506 0.0418 1.0000
14.000 1.0199 0.05890 0.05373 0.0496 0.0418 1.0000
14.250 0.9952 0.06459 0.05965 0.0471 0.0418 1.0000
14.500 0.9644 0.07190 0.06721 0.0427 0.0419 1.0000
14.750 0.9240 0.08187 0.07742 0.0358 0.0423 1.0000
15.000 0.8773 0.09431 0.09005 0.0274 0.0433 1.0000
15.250 0.8305 0.10800 0.10385 0.0192 0.0442 1.0000
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