TH 25816 HALE AIRFOIL (th25816-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: TH 25816 HALE AIRFOIL (th25816-il) Reynolds number: 500,000 Max Cl/Cd: 54.73 at α=8.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-th25816-il-500000.txt Download as CSV file: xf-th25816-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: TH 25816 HALE AIRFOIL
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
------ -------- --------- --------- -------- -------- --------
-17.500 -0.2014 0.08750 0.08427 -0.1808 0.9166 0.0237
-17.250 -0.2301 0.08073 0.07735 -0.1834 0.9152 0.0236
-17.000 -0.2554 0.07420 0.07067 -0.1856 0.9143 0.0233
-16.750 -0.2752 0.06831 0.06463 -0.1876 0.9135 0.0231
-16.500 -0.2994 0.06212 0.05825 -0.1891 0.9128 0.0229
-16.250 -0.3192 0.05644 0.05236 -0.1900 0.9121 0.0225
-16.000 -0.3328 0.05168 0.04742 -0.1909 0.9115 0.0225
-15.750 -0.3442 0.04710 0.04263 -0.1914 0.9110 0.0224
-15.500 -0.3686 0.04470 0.04010 -0.1865 0.9041 0.0222
-15.250 -0.3772 0.04136 0.03658 -0.1854 0.9016 0.0223
-15.000 -0.3755 0.03819 0.03323 -0.1853 0.9003 0.0221
-14.750 -0.3699 0.03534 0.03022 -0.1856 0.8995 0.0221
-14.500 -0.3591 0.03264 0.02734 -0.1860 0.8988 0.0221
-14.250 -0.3468 0.03044 0.02501 -0.1867 0.8982 0.0225
-14.000 -0.3293 0.02841 0.02285 -0.1876 0.8977 0.0227
-13.750 -0.3102 0.02653 0.02085 -0.1887 0.8973 0.0230
-13.500 -0.2874 0.02487 0.01908 -0.1899 0.8970 0.0231
-13.250 -0.3832 0.03781 0.03165 -0.1808 0.8891 0.0227
-13.000 -0.3607 0.03661 0.03034 -0.1813 0.8877 0.0231
-12.750 -0.3334 0.03555 0.02920 -0.1825 0.8869 0.0231
-12.500 -0.3080 0.03449 0.02806 -0.1836 0.8861 0.0234
-12.250 -0.2806 0.03349 0.02699 -0.1848 0.8854 0.0236
-12.000 -0.2538 0.03250 0.02594 -0.1860 0.8848 0.0239
-11.750 -0.2562 0.03206 0.02545 -0.1813 0.8775 0.0240
-11.500 -0.2316 0.03125 0.02465 -0.1813 0.8754 0.0244
-11.250 -0.2096 0.03028 0.02369 -0.1818 0.8739 0.0249
-11.000 -0.1865 0.02926 0.02265 -0.1826 0.8726 0.0253
-10.750 -0.1619 0.02824 0.02161 -0.1838 0.8715 0.0257
-10.500 -0.1355 0.02716 0.02049 -0.1854 0.8706 0.0262
-10.250 -0.1382 0.02674 0.02004 -0.1808 0.8627 0.0266
-10.000 -0.1171 0.02581 0.01905 -0.1812 0.8600 0.0272
-9.750 -0.0893 0.02479 0.01798 -0.1831 0.8584 0.0278
-9.500 -0.0597 0.02369 0.01683 -0.1856 0.8570 0.0287
-9.250 -0.0492 0.02296 0.01606 -0.1839 0.8521 0.0296
-9.000 -0.0376 0.02234 0.01541 -0.1823 0.8470 0.0302
-8.750 -0.0080 0.02151 0.01452 -0.1844 0.8446 0.0317
-8.250 0.0383 0.02015 0.01308 -0.1859 0.8375 0.0353
-8.000 0.0454 0.01978 0.01267 -0.1830 0.8320 0.0369
-7.750 0.0732 0.01911 0.01198 -0.1847 0.8292 0.0432
-7.500 0.0953 0.01787 0.01099 -0.1863 0.8264 0.0956
-7.250 0.0706 0.01767 0.01087 -0.1767 0.8196 0.1132
-7.000 0.0610 0.01681 0.01026 -0.1713 0.8146 0.1729
-6.750 0.0598 0.01537 0.00921 -0.1685 0.8109 0.2742
-6.500 0.0276 0.01525 0.00916 -0.1572 0.8047 0.2892
-6.250 0.0025 0.01463 0.00870 -0.1480 0.7995 0.3339
-6.000 -0.0129 0.01365 0.00794 -0.1413 0.7958 0.3976
-5.750 -0.0461 0.01327 0.00769 -0.1300 0.7909 0.4287
-5.500 -0.0808 0.01318 0.00764 -0.1179 0.7854 0.4402
-5.250 -0.1168 0.01263 0.00721 -0.1058 0.7809 0.4748
-5.000 -0.1268 0.01179 0.00662 -0.0993 0.7778 0.5505
-4.750 -0.1581 0.01192 0.00685 -0.0875 0.7726 0.5683
-4.500 -0.1530 0.01182 0.00684 -0.0834 0.7692 0.6019
-4.250 -0.1316 0.01171 0.00674 -0.0826 0.7668 0.6295
-4.000 -0.1026 0.01163 0.00662 -0.0834 0.7650 0.6480
-3.750 -0.0695 0.01158 0.00654 -0.0849 0.7634 0.6641
-3.500 -0.0323 0.01159 0.00653 -0.0873 0.7617 0.6797
-3.250 -0.0240 0.01188 0.00688 -0.0835 0.7586 0.6947
-3.000 -0.0237 0.01223 0.00728 -0.0780 0.7546 0.7076
-2.750 -0.0046 0.01246 0.00748 -0.0766 0.7520 0.7194
-2.500 0.0254 0.01256 0.00759 -0.0773 0.7501 0.7243
-2.250 0.0591 0.01267 0.00767 -0.0788 0.7484 0.7296
-2.000 0.0941 0.01265 0.00758 -0.0809 0.7470 0.7344
-1.750 0.1312 0.01260 0.00744 -0.0834 0.7455 0.7381
-1.500 0.1733 0.01261 0.00740 -0.0869 0.7440 0.7399
-1.250 0.1487 0.01308 0.00798 -0.0765 0.7390 0.7435
-1.000 0.1650 0.01322 0.00811 -0.0747 0.7361 0.7464
-0.750 0.1911 0.01323 0.00808 -0.0750 0.7340 0.7493
-0.500 0.2222 0.01318 0.00797 -0.0764 0.7323 0.7522
-0.250 0.2564 0.01310 0.00783 -0.0784 0.7308 0.7549
0.000 0.2936 0.01307 0.00777 -0.0808 0.7295 0.7568
0.250 0.3337 0.01308 0.00774 -0.0840 0.7282 0.7585
0.500 0.3299 0.01348 0.00820 -0.0780 0.7244 0.7616
0.750 0.3292 0.01382 0.00857 -0.0728 0.7205 0.7651
1.000 0.3506 0.01391 0.00865 -0.0722 0.7181 0.7685
1.250 0.3797 0.01390 0.00859 -0.0732 0.7162 0.7716
1.500 0.4126 0.01389 0.00857 -0.0748 0.7148 0.7736
1.750 0.4497 0.01385 0.00852 -0.0773 0.7134 0.7753
2.000 0.4888 0.01384 0.00849 -0.0802 0.7121 0.7772
2.250 0.5304 0.01387 0.00849 -0.0836 0.7107 0.7791
2.500 0.4887 0.01471 0.00944 -0.0703 0.7048 0.7844
2.750 0.5036 0.01491 0.00962 -0.0685 0.7018 0.7883
3.000 0.5305 0.01496 0.00969 -0.0689 0.6998 0.7905
3.250 0.5637 0.01495 0.00969 -0.0705 0.6982 0.7924
3.500 0.6002 0.01492 0.00965 -0.0729 0.6969 0.7944
3.750 0.6391 0.01488 0.00960 -0.0757 0.6956 0.7964
4.000 0.6809 0.01486 0.00956 -0.0792 0.6943 0.7986
4.250 0.6302 0.01599 0.01078 -0.0645 0.6871 0.8051
4.500 0.6485 0.01617 0.01100 -0.0633 0.6843 0.8075
4.750 0.6793 0.01616 0.01101 -0.0644 0.6824 0.8095
5.000 0.7157 0.01608 0.01092 -0.0667 0.6809 0.8115
5.250 0.7552 0.01596 0.01080 -0.0696 0.6795 0.8135
5.500 0.7979 0.01584 0.01067 -0.0732 0.6780 0.8157
5.750 0.7476 0.01720 0.01212 -0.0590 0.6702 0.8222
6.000 0.7696 0.01727 0.01221 -0.0585 0.6672 0.8246
6.250 0.8036 0.01713 0.01209 -0.0603 0.6652 0.8264
6.500 0.8426 0.01692 0.01189 -0.0630 0.6635 0.8281
6.750 0.8852 0.01671 0.01168 -0.0664 0.6617 0.8300
7.000 0.8421 0.01816 0.01324 -0.0538 0.6541 0.8355
7.250 0.8645 0.01825 0.01333 -0.0536 0.6506 0.8391
7.500 0.9014 0.01797 0.01304 -0.0559 0.6482 0.8414
7.750 0.9414 0.01765 0.01273 -0.0587 0.6459 0.8429
8.000 0.9185 0.01878 0.01395 -0.0500 0.6391 0.8462
8.250 0.9297 0.01911 0.01432 -0.0476 0.6342 0.8491
8.500 0.9639 0.01887 0.01407 -0.0494 0.6310 0.8518
8.750 1.0087 0.01843 0.01362 -0.0531 0.6282 0.8543
9.000 0.9719 0.02009 0.01537 -0.0425 0.6196 0.8591
9.250 0.9955 0.02001 0.01530 -0.0423 0.6147 0.8611
9.500 1.0143 0.02016 0.01547 -0.0413 0.6092 0.8633
9.750 1.0008 0.02137 0.01675 -0.0349 0.6009 0.8668
10.000 1.0321 0.02114 0.01650 -0.0362 0.5960 0.8695
10.250 1.0156 0.02269 0.01810 -0.0298 0.5860 0.8737
10.500 1.0396 0.02264 0.01804 -0.0298 0.5795 0.8761
10.750 1.0238 0.02416 0.01964 -0.0234 0.5692 0.8790
11.000 1.0476 0.02414 0.01959 -0.0234 0.5621 0.8812
11.250 1.0353 0.02577 0.02129 -0.0180 0.5503 0.8845
11.500 1.0429 0.02660 0.02212 -0.0158 0.5401 0.8874
11.750 1.0539 0.02734 0.02285 -0.0143 0.5298 0.8902
12.000 1.0514 0.02857 0.02410 -0.0106 0.5167 0.8928
12.250 1.0535 0.02961 0.02515 -0.0075 0.5038 0.8952
12.500 1.0571 0.03065 0.02616 -0.0049 0.4895 0.8977
12.750 1.0572 0.03195 0.02742 -0.0019 0.4725 0.9003
13.000 1.0600 0.03319 0.02861 0.0005 0.4567 0.9029
13.250 1.0605 0.03466 0.03002 0.0031 0.4398 0.9052
13.500 1.0589 0.03606 0.03138 0.0061 0.4225 0.9075
13.750 1.0561 0.03759 0.03286 0.0092 0.4060 0.9097
14.000 1.0546 0.03914 0.03436 0.0119 0.3890 0.9120
14.250 1.0522 0.04085 0.03602 0.0146 0.3722 0.9142
14.500 1.0517 0.04252 0.03764 0.0168 0.3555 0.9164
14.750 1.0487 0.04445 0.03951 0.0192 0.3372 0.9186
15.000 1.0485 0.04624 0.04125 0.0211 0.3206 0.9204
15.250 1.0464 0.04801 0.04298 0.0234 0.3051 0.9223
15.500 1.0452 0.04980 0.04473 0.0255 0.2888 0.9243
15.750 1.0432 0.05174 0.04662 0.0275 0.2731 0.9264
16.000 1.0431 0.05360 0.04843 0.0291 0.2578 0.9284
16.250 1.0431 0.05557 0.05036 0.0306 0.2427 0.9304
16.750 1.0452 0.05951 0.05421 0.0329 0.2128 0.9338
17.000 1.0463 0.06135 0.05602 0.0342 0.1991 0.9357
17.250 1.0450 0.06346 0.05809 0.0355 0.1843 0.9377
17.500 1.0474 0.06536 0.05996 0.0364 0.1741 0.9396
17.750 1.0473 0.06755 0.06211 0.0373 0.1623 0.9414
18.000 1.0503 0.06955 0.06410 0.0379 0.1510 0.9432
18.250 1.0543 0.07148 0.06602 0.0384 0.1415 0.9450
18.500 1.0542 0.07385 0.06836 0.0389 0.1328 0.9465
18.750 1.0605 0.07563 0.07016 0.0391 0.1251 0.9483
19.000 1.0618 0.07792 0.07245 0.0394 0.1187 0.9499
19.250 1.0684 0.07974 0.07430 0.0394 0.1127 0.9517
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