TH 25816 HALE AIRFOIL (th25816-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: TH 25816 HALE AIRFOIL (th25816-il) Reynolds number: 1,000,000 Max Cl/Cd: 59.62 at α=6.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-th25816-il-1000000-n5.txt Download as CSV file: xf-th25816-il-1000000-n5.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 = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -0.3036 0.05818 0.05362 -0.2518 0.9407 0.0107
-19.500 -0.3047 0.05563 0.05101 -0.2524 0.9401 0.0108
-19.250 -0.3021 0.05336 0.04867 -0.2533 0.9393 0.0109
-19.000 -0.2962 0.05138 0.04664 -0.2541 0.9386 0.0110
-18.750 -0.2928 0.04933 0.04453 -0.2547 0.9380 0.0111
-18.500 -0.2866 0.04758 0.04273 -0.2552 0.9375 0.0111
-18.250 -0.2806 0.04583 0.04093 -0.2557 0.9368 0.0113
-18.000 -0.2719 0.04424 0.03928 -0.2563 0.9360 0.0113
-17.750 -0.2707 0.04285 0.03784 -0.2551 0.9350 0.0113
-17.500 -0.2719 0.04154 0.03650 -0.2532 0.9339 0.0114
-17.250 -0.2691 0.04042 0.03535 -0.2517 0.9323 0.0115
-17.000 -0.2653 0.03921 0.03410 -0.2505 0.9309 0.0116
-16.750 -0.2601 0.03798 0.03283 -0.2496 0.9297 0.0116
-16.500 -0.2510 0.03687 0.03168 -0.2491 0.9284 0.0118
-16.250 -0.2400 0.03574 0.03051 -0.2491 0.9272 0.0120
-16.000 -0.2293 0.03457 0.02929 -0.2490 0.9260 0.0120
-15.750 -0.2164 0.03351 0.02819 -0.2491 0.9250 0.0122
-15.500 -0.2043 0.03241 0.02704 -0.2491 0.9240 0.0123
-15.250 -0.1876 0.03145 0.02603 -0.2497 0.9229 0.0125
-15.000 -0.1877 0.03048 0.02502 -0.2471 0.9211 0.0124
-14.750 -0.1864 0.02981 0.02434 -0.2441 0.9187 0.0125
-14.500 -0.1787 0.02912 0.02362 -0.2423 0.9164 0.0127
-14.250 -0.1689 0.02831 0.02278 -0.2412 0.9142 0.0128
-14.000 -0.1566 0.02747 0.02190 -0.2405 0.9122 0.0129
-13.750 -0.1397 0.02666 0.02104 -0.2406 0.9105 0.0130
-13.500 -0.1325 0.02593 0.02028 -0.2387 0.9077 0.0131
-13.250 -0.1361 0.02549 0.01982 -0.2341 0.9024 0.0131
-13.000 -0.1235 0.02489 0.01918 -0.2330 0.8987 0.0133
-12.750 -0.1107 0.02420 0.01845 -0.2320 0.8951 0.0134
-12.500 -0.1114 0.02370 0.01792 -0.2279 0.8869 0.0134
-12.250 -0.1020 0.02289 0.01706 -0.2264 0.8787 0.0137
-12.000 -0.0887 0.02213 0.01622 -0.2255 0.8677 0.0141
-11.750 -0.0746 0.02158 0.01556 -0.2245 0.8535 0.0141
-11.500 -0.0666 0.02115 0.01501 -0.2220 0.8394 0.0144
-11.250 -0.0619 0.02082 0.01458 -0.2188 0.8274 0.0146
-11.000 -0.0594 0.02049 0.01418 -0.2151 0.8173 0.0148
-10.750 -0.0627 0.02027 0.01389 -0.2099 0.8084 0.0149
-10.500 -0.0659 0.01998 0.01354 -0.2049 0.8006 0.0151
-10.000 -0.0631 0.01941 0.01289 -0.1968 0.7893 0.0155
-9.750 -0.0609 0.01912 0.01255 -0.1929 0.7842 0.0157
-9.500 -0.0609 0.01889 0.01228 -0.1884 0.7789 0.0159
-9.250 -0.0577 0.01865 0.01201 -0.1846 0.7748 0.0161
-9.000 -0.0538 0.01840 0.01173 -0.1809 0.7705 0.0163
-8.750 -0.0511 0.01815 0.01145 -0.1770 0.7663 0.0165
-8.500 -0.0471 0.01792 0.01118 -0.1733 0.7624 0.0168
-8.250 -0.0420 0.01762 0.01086 -0.1699 0.7593 0.0173
-8.000 -0.0370 0.01735 0.01058 -0.1665 0.7563 0.0175
-7.750 -0.0314 0.01712 0.01033 -0.1631 0.7529 0.0180
-7.500 -0.0261 0.01689 0.01008 -0.1596 0.7493 0.0186
-7.250 -0.0202 0.01667 0.00983 -0.1562 0.7459 0.0189
-7.000 -0.0121 0.01646 0.00958 -0.1532 0.7432 0.0192
-6.750 -0.0051 0.01624 0.00936 -0.1500 0.7408 0.0200
-6.500 0.0007 0.01600 0.00913 -0.1466 0.7381 0.0208
-6.250 0.0069 0.01577 0.00888 -0.1432 0.7353 0.0223
-6.000 0.0145 0.01557 0.00867 -0.1400 0.7324 0.0233
-5.750 0.0191 0.01534 0.00842 -0.1363 0.7293 0.0268
-5.500 0.0233 0.01507 0.00817 -0.1325 0.7265 0.0344
-5.250 0.0219 0.01472 0.00790 -0.1276 0.7241 0.0528
-5.000 0.0205 0.01442 0.00765 -0.1227 0.7214 0.0665
-4.750 0.0173 0.01406 0.00738 -0.1174 0.7186 0.0878
-4.500 0.0130 0.01371 0.00709 -0.1119 0.7158 0.1095
-4.250 0.0004 0.01326 0.00674 -0.1047 0.7128 0.1420
-4.000 -0.0065 0.01298 0.00649 -0.0985 0.7099 0.1582
-3.500 -0.0377 0.01221 0.00591 -0.0825 0.7041 0.2147
-3.250 -0.0371 0.01165 0.00556 -0.0779 0.7015 0.2746
-3.000 -0.0323 0.01103 0.00521 -0.0743 0.6990 0.3463
-2.750 -0.0319 0.00996 0.00468 -0.0700 0.6965 0.4781
-2.500 -0.0195 0.00925 0.00440 -0.0679 0.6942 0.5902
-2.250 0.0011 0.00909 0.00441 -0.0670 0.6925 0.6364
-2.000 0.0238 0.00907 0.00446 -0.0665 0.6906 0.6580
-1.750 0.0483 0.00912 0.00449 -0.0664 0.6884 0.6643
-1.500 0.0729 0.00917 0.00451 -0.0663 0.6860 0.6687
-1.250 0.0971 0.00921 0.00455 -0.0661 0.6836 0.6739
-1.000 0.1222 0.00926 0.00458 -0.0661 0.6815 0.6785
-0.750 0.1477 0.00932 0.00460 -0.0662 0.6794 0.6825
-0.500 0.1737 0.00936 0.00461 -0.0664 0.6773 0.6864
-0.250 0.1985 0.00941 0.00468 -0.0663 0.6757 0.6893
0.000 0.2232 0.00948 0.00474 -0.0663 0.6737 0.6919
0.250 0.2478 0.00955 0.00481 -0.0662 0.6714 0.6946
0.500 0.2722 0.00963 0.00487 -0.0661 0.6690 0.6972
0.750 0.2961 0.00972 0.00495 -0.0659 0.6667 0.6998
1.250 0.3441 0.00990 0.00509 -0.0656 0.6624 0.7052
1.500 0.3689 0.00998 0.00517 -0.0656 0.6604 0.7081
1.750 0.3924 0.01008 0.00529 -0.0654 0.6583 0.7110
2.000 0.4163 0.01018 0.00540 -0.0652 0.6562 0.7139
2.250 0.4403 0.01029 0.00551 -0.0651 0.6538 0.7167
2.500 0.4646 0.01040 0.00560 -0.0650 0.6516 0.7192
2.750 0.4879 0.01050 0.00572 -0.0648 0.6492 0.7223
3.000 0.5114 0.01061 0.00583 -0.0646 0.6469 0.7257
3.250 0.5354 0.01073 0.00594 -0.0645 0.6443 0.7292
3.500 0.5567 0.01090 0.00613 -0.0638 0.6422 0.7327
3.750 0.5790 0.01106 0.00631 -0.0634 0.6397 0.7357
4.000 0.6009 0.01121 0.00649 -0.0630 0.6368 0.7388
4.250 0.6227 0.01137 0.00666 -0.0624 0.6338 0.7423
4.500 0.6445 0.01154 0.00683 -0.0619 0.6309 0.7458
4.750 0.6666 0.01171 0.00699 -0.0615 0.6277 0.7498
5.000 0.6870 0.01193 0.00724 -0.0608 0.6248 0.7534
5.250 0.7065 0.01216 0.00751 -0.0599 0.6214 0.7570
5.500 0.7255 0.01240 0.00778 -0.0589 0.6173 0.7610
5.750 0.7448 0.01265 0.00802 -0.0580 0.6133 0.7649
6.000 0.7650 0.01289 0.00827 -0.0573 0.6098 0.7686
6.250 0.7846 0.01316 0.00857 -0.0565 0.6060 0.7719
6.500 0.8013 0.01350 0.00894 -0.0551 0.6014 0.7754
6.750 0.8181 0.01384 0.00928 -0.0538 0.5965 0.7793
7.000 0.8365 0.01416 0.00962 -0.0528 0.5920 0.7833
7.250 0.8523 0.01457 0.01005 -0.0514 0.5859 0.7870
7.500 0.8656 0.01504 0.01052 -0.0495 0.5798 0.7903
7.750 0.8827 0.01542 0.01093 -0.0484 0.5745 0.7935
8.000 0.8977 0.01588 0.01142 -0.0469 0.5676 0.7969
8.250 0.9077 0.01651 0.01204 -0.0445 0.5597 0.8003
8.500 0.9207 0.01708 0.01260 -0.0428 0.5503 0.8034
8.750 0.9271 0.01789 0.01339 -0.0400 0.5384 0.8064
9.000 0.9338 0.01871 0.01419 -0.0372 0.5274 0.8094
9.250 0.9347 0.01979 0.01525 -0.0336 0.5117 0.8125
9.500 0.9382 0.02079 0.01622 -0.0305 0.4959 0.8157
9.750 0.9336 0.02220 0.01755 -0.0262 0.4751 0.8186
10.000 0.9261 0.02381 0.01906 -0.0217 0.4513 0.8212
10.250 0.9214 0.02534 0.02049 -0.0177 0.4298 0.8234
10.500 0.9206 0.02672 0.02184 -0.0144 0.4125 0.8259
10.750 0.9196 0.02816 0.02322 -0.0112 0.3941 0.8284
11.000 0.9185 0.02965 0.02465 -0.0081 0.3740 0.8308
11.250 0.9213 0.03100 0.02595 -0.0056 0.3581 0.8331
11.500 0.9229 0.03244 0.02732 -0.0031 0.3398 0.8351
11.750 0.9269 0.03380 0.02862 -0.0009 0.3234 0.8370
12.000 0.9309 0.03518 0.02995 0.0011 0.3084 0.8387
12.250 0.9376 0.03644 0.03114 0.0027 0.2930 0.8402
12.500 0.9409 0.03791 0.03257 0.0048 0.2767 0.8420
12.750 0.9471 0.03921 0.03383 0.0064 0.2621 0.8438
13.000 0.9553 0.04042 0.03502 0.0077 0.2493 0.8455
13.250 0.9607 0.04185 0.03641 0.0093 0.2365 0.8471
13.500 0.9679 0.04316 0.03768 0.0106 0.2241 0.8486
13.750 0.9732 0.04463 0.03909 0.0120 0.2084 0.8501
14.000 0.9807 0.04601 0.04044 0.0132 0.1970 0.8517
14.250 0.9897 0.04728 0.04169 0.0141 0.1866 0.8532
14.500 0.9966 0.04873 0.04308 0.0152 0.1737 0.8547
14.750 1.0027 0.05028 0.04460 0.0163 0.1631 0.8559
15.000 1.0114 0.05165 0.04592 0.0171 0.1524 0.8570
15.250 1.0171 0.05325 0.04746 0.0181 0.1387 0.8580
15.500 1.0242 0.05476 0.04896 0.0189 0.1310 0.8594
15.750 1.0325 0.05619 0.05038 0.0196 0.1225 0.8608
16.000 1.0407 0.05763 0.05181 0.0203 0.1139 0.8621
16.250 1.0465 0.05932 0.05348 0.0211 0.1062 0.8635
16.500 1.0565 0.06069 0.05487 0.0215 0.1011 0.8648
16.750 1.0648 0.06219 0.05636 0.0220 0.0954 0.8661
17.000 1.0720 0.06383 0.05801 0.0225 0.0886 0.8674
17.250 1.0798 0.06543 0.05961 0.0229 0.0842 0.8688
17.500 1.0892 0.06691 0.06109 0.0231 0.0803 0.8701
17.750 1.0978 0.06848 0.06268 0.0234 0.0762 0.8713
18.000 1.1047 0.07025 0.06446 0.0237 0.0728 0.8724
18.250 1.1139 0.07180 0.06603 0.0238 0.0696 0.8734
18.500 1.1227 0.07342 0.06767 0.0238 0.0664 0.8742
18.750 1.1280 0.07539 0.06964 0.0240 0.0628 0.8748
19.000 1.1361 0.07708 0.07136 0.0241 0.0597 0.8759
19.250 1.1449 0.07867 0.07300 0.0240 0.0579 0.8770
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