SD8000-089-88 (sd8000-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
|---|---|
|
Airfoil: SD8000-089-88 (sd8000-il) Reynolds number: 1,000,000 Max Cl/Cd: 92.24 at α=5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-sd8000-il-1000000.txt Download as CSV file: xf-sd8000-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: SD8000-089-88
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
------ -------- --------- --------- -------- -------- --------
-13.000 -0.7809 0.08153 0.07960 -0.0246 1.0000 0.0066
-12.750 -0.8177 0.07010 0.06810 -0.0315 1.0000 0.0066
-12.500 -0.8400 0.06116 0.05907 -0.0373 1.0000 0.0065
-12.250 -0.8657 0.04990 0.04766 -0.0464 1.0000 0.0065
-11.750 -0.8992 0.03707 0.03450 -0.0583 1.0000 0.0064
-11.500 -0.9157 0.03364 0.03086 -0.0572 1.0000 0.0064
-11.250 -0.9207 0.03019 0.02712 -0.0565 1.0000 0.0065
-11.000 -0.9259 0.02608 0.02261 -0.0553 1.0000 0.0067
-10.750 -0.9172 0.02362 0.01989 -0.0542 1.0000 0.0068
-10.500 -0.9028 0.02199 0.01810 -0.0532 1.0000 0.0070
-10.250 -0.8863 0.02075 0.01672 -0.0521 1.0000 0.0071
-10.000 -0.8687 0.01983 0.01571 -0.0509 1.0000 0.0073
-9.750 -0.8520 0.01889 0.01467 -0.0495 1.0000 0.0075
-9.500 -0.8362 0.01801 0.01368 -0.0477 1.0000 0.0076
-9.250 -0.8203 0.01725 0.01281 -0.0459 1.0000 0.0078
-9.000 -0.8045 0.01644 0.01189 -0.0440 1.0000 0.0080
-8.750 -0.7780 0.01562 0.01095 -0.0443 0.9990 0.0083
-8.500 -0.7466 0.01480 0.01002 -0.0455 0.9974 0.0086
-8.250 -0.7144 0.01411 0.00923 -0.0468 0.9958 0.0088
-8.000 -0.6823 0.01324 0.00823 -0.0481 0.9944 0.0092
-7.750 -0.6521 0.01239 0.00730 -0.0490 0.9923 0.0101
-7.500 -0.6203 0.01198 0.00686 -0.0500 0.9902 0.0110
-7.250 -0.5877 0.01153 0.00635 -0.0512 0.9884 0.0118
-7.000 -0.5548 0.01084 0.00559 -0.0525 0.9867 0.0133
-6.750 -0.5207 0.01044 0.00516 -0.0540 0.9854 0.0149
-6.500 -0.4865 0.00996 0.00465 -0.0554 0.9841 0.0174
-6.250 -0.4551 0.00965 0.00434 -0.0562 0.9816 0.0202
-6.000 -0.4251 0.00927 0.00395 -0.0567 0.9780 0.0238
-5.750 -0.3939 0.00904 0.00371 -0.0575 0.9748 0.0270
-5.500 -0.3633 0.00870 0.00339 -0.0580 0.9715 0.0325
-5.250 -0.3364 0.00849 0.00316 -0.0577 0.9660 0.0371
-5.000 -0.3097 0.00825 0.00295 -0.0574 0.9605 0.0433
-4.750 -0.2831 0.00803 0.00274 -0.0570 0.9554 0.0508
-4.500 -0.2572 0.00787 0.00257 -0.0565 0.9490 0.0572
-4.250 -0.2314 0.00766 0.00239 -0.0559 0.9434 0.0666
-4.000 -0.2052 0.00746 0.00221 -0.0554 0.9369 0.0764
-3.750 -0.1791 0.00729 0.00205 -0.0549 0.9304 0.0876
-3.500 -0.1526 0.00710 0.00191 -0.0545 0.9236 0.1021
-3.250 -0.1261 0.00692 0.00176 -0.0540 0.9163 0.1192
-3.000 -0.0994 0.00672 0.00163 -0.0537 0.9090 0.1420
-2.750 -0.0728 0.00651 0.00150 -0.0533 0.9009 0.1711
-2.500 -0.0458 0.00630 0.00139 -0.0530 0.8925 0.2050
-2.250 -0.0191 0.00609 0.00127 -0.0527 0.8840 0.2459
-2.000 0.0081 0.00588 0.00119 -0.0525 0.8743 0.2886
-1.750 0.0350 0.00566 0.00110 -0.0523 0.8644 0.3419
-1.500 0.0619 0.00546 0.00103 -0.0520 0.8530 0.3940
-1.250 0.0889 0.00528 0.00097 -0.0517 0.8399 0.4489
-1.000 0.1158 0.00509 0.00093 -0.0515 0.8259 0.5095
-0.750 0.1428 0.00495 0.00090 -0.0512 0.8108 0.5620
-0.500 0.1697 0.00483 0.00087 -0.0508 0.7942 0.6139
-0.250 0.1965 0.00473 0.00087 -0.0505 0.7752 0.6631
0.000 0.2231 0.00468 0.00087 -0.0500 0.7536 0.7083
0.250 0.2495 0.00464 0.00088 -0.0495 0.7303 0.7516
0.500 0.2755 0.00464 0.00091 -0.0490 0.7057 0.7929
0.750 0.3011 0.00464 0.00094 -0.0482 0.6793 0.8327
1.000 0.3260 0.00467 0.00099 -0.0474 0.6515 0.8711
1.250 0.3500 0.00473 0.00104 -0.0463 0.6220 0.9086
1.500 0.3745 0.00482 0.00108 -0.0452 0.5905 0.9460
1.750 0.4082 0.00497 0.00113 -0.0464 0.5535 0.9769
2.000 0.4462 0.00518 0.00117 -0.0486 0.5144 0.9963
2.250 0.4745 0.00540 0.00124 -0.0488 0.4775 1.0000
2.500 0.5002 0.00561 0.00132 -0.0483 0.4453 1.0000
2.750 0.5259 0.00587 0.00142 -0.0479 0.4098 1.0000
3.000 0.5519 0.00610 0.00153 -0.0476 0.3768 1.0000
3.250 0.5780 0.00635 0.00164 -0.0472 0.3455 1.0000
3.500 0.6040 0.00662 0.00178 -0.0469 0.3130 1.0000
3.750 0.6301 0.00690 0.00192 -0.0466 0.2821 1.0000
4.000 0.6563 0.00716 0.00207 -0.0463 0.2548 1.0000
4.250 0.6825 0.00743 0.00223 -0.0460 0.2297 1.0000
4.500 0.7086 0.00772 0.00242 -0.0457 0.2058 1.0000
4.750 0.7349 0.00797 0.00259 -0.0455 0.1863 1.0000
5.000 0.7610 0.00825 0.00279 -0.0452 0.1666 1.0000
5.250 0.7871 0.00855 0.00300 -0.0449 0.1481 1.0000
5.500 0.8131 0.00884 0.00322 -0.0446 0.1305 1.0000
5.750 0.8388 0.00917 0.00346 -0.0443 0.1125 1.0000
6.000 0.8647 0.00947 0.00370 -0.0440 0.0998 1.0000
6.250 0.8907 0.00975 0.00395 -0.0437 0.0893 1.0000
6.500 0.9165 0.01006 0.00422 -0.0433 0.0795 1.0000
6.750 0.9419 0.01040 0.00451 -0.0430 0.0693 1.0000
7.000 0.9675 0.01072 0.00480 -0.0426 0.0610 1.0000
7.250 0.9930 0.01104 0.00511 -0.0423 0.0535 1.0000
7.500 1.0179 0.01142 0.00545 -0.0419 0.0458 1.0000
7.750 1.0426 0.01184 0.00583 -0.0414 0.0382 1.0000
8.000 1.0671 0.01225 0.00621 -0.0409 0.0317 1.0000
8.250 1.0912 0.01274 0.00668 -0.0404 0.0254 1.0000
8.500 1.1147 0.01327 0.00722 -0.0397 0.0211 1.0000
8.750 1.1383 0.01377 0.00772 -0.0391 0.0185 1.0000
9.000 1.1607 0.01444 0.00843 -0.0383 0.0166 1.0000
9.250 1.1844 0.01489 0.00893 -0.0377 0.0158 1.0000
9.500 1.2076 0.01538 0.00949 -0.0371 0.0149 1.0000
9.750 1.2300 0.01594 0.01008 -0.0363 0.0140 1.0000
10.000 1.2498 0.01680 0.01101 -0.0352 0.0129 1.0000
10.250 1.2698 0.01759 0.01188 -0.0341 0.0124 1.0000
10.500 1.2912 0.01816 0.01252 -0.0333 0.0120 1.0000
10.750 1.3116 0.01881 0.01324 -0.0323 0.0116 1.0000
11.000 1.3317 0.01944 0.01395 -0.0313 0.0111 1.0000
11.250 1.3506 0.02015 0.01473 -0.0302 0.0107 1.0000
11.500 1.3688 0.02088 0.01551 -0.0290 0.0102 1.0000
11.750 1.3807 0.02211 0.01682 -0.0271 0.0096 1.0000
12.000 1.3852 0.02383 0.01871 -0.0242 0.0092 1.0000
12.250 1.4004 0.02445 0.01941 -0.0225 0.0091 1.0000
12.500 1.4095 0.02533 0.02037 -0.0200 0.0089 1.0000
12.750 1.4182 0.02622 0.02135 -0.0177 0.0087 1.0000
13.000 1.4256 0.02724 0.02248 -0.0154 0.0085 1.0000
13.250 1.4305 0.02849 0.02383 -0.0131 0.0083 1.0000
13.500 1.4339 0.02993 0.02537 -0.0110 0.0081 1.0000
13.750 1.4411 0.03115 0.02667 -0.0094 0.0078 1.0000
14.000 1.4428 0.03290 0.02852 -0.0078 0.0077 1.0000
14.250 1.4441 0.03480 0.03051 -0.0065 0.0075 1.0000
14.500 1.4435 0.03703 0.03285 -0.0055 0.0074 1.0000
14.750 1.4390 0.03987 0.03579 -0.0050 0.0072 1.0000
15.000 1.4324 0.04321 0.03924 -0.0051 0.0070 1.0000
15.250 1.4183 0.04784 0.04402 -0.0062 0.0069 1.0000
15.500 1.4068 0.05262 0.04896 -0.0079 0.0069 1.0000
15.750 1.3823 0.05986 0.05638 -0.0113 0.0068 1.0000
16.000 1.3697 0.06579 0.06246 -0.0144 0.0068 1.0000
16.250 1.3460 0.07400 0.07083 -0.0190 0.0067 1.0000
16.500 1.3210 0.08289 0.07989 -0.0242 0.0067 1.0000
16.750 1.3107 0.08932 0.08643 -0.0279 0.0068 1.0000
17.000 1.2847 0.09898 0.09625 -0.0335 0.0067 1.0000
17.250 1.2686 0.10692 0.10430 -0.0382 0.0068 1.0000
|
Polar data table (+)
Polar graphs
<< Back to SD8000-089-88 (sd8000-il)