TH 25816 HALE AIRFOIL (th25816-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: TH 25816 HALE AIRFOIL (th25816-il) Reynolds number: 500,000 Max Cl/Cd: 47.87 at α=6.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-th25816-il-500000-n5.txt Download as CSV file: xf-th25816-il-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -0.3379 0.08237 0.07775 -0.2099 0.9396 0.0130
-19.500 -0.3439 0.07791 0.07316 -0.2126 0.9391 0.0131
-19.250 -0.3472 0.07373 0.06882 -0.2154 0.9387 0.0132
-19.000 -0.3466 0.07008 0.06503 -0.2180 0.9383 0.0132
-18.750 -0.3452 0.06664 0.06145 -0.2204 0.9379 0.0133
-18.500 -0.3407 0.06365 0.05834 -0.2226 0.9376 0.0133
-18.250 -0.3371 0.06060 0.05517 -0.2247 0.9372 0.0135
-18.000 -0.3875 0.06125 0.05585 -0.2110 0.9297 0.0135
-17.750 -0.3877 0.05919 0.05370 -0.2106 0.9280 0.0134
-17.500 -0.3848 0.05687 0.05129 -0.2110 0.9271 0.0136
-17.250 -0.3763 0.05481 0.04917 -0.2121 0.9263 0.0137
-17.000 -0.3663 0.05274 0.04705 -0.2134 0.9257 0.0139
-16.750 -0.3544 0.05083 0.04506 -0.2147 0.9251 0.0139
-16.500 -0.3403 0.04895 0.04312 -0.2164 0.9247 0.0142
-16.250 -0.3252 0.04718 0.04129 -0.2181 0.9242 0.0144
-16.000 -0.3649 0.04723 0.04132 -0.2066 0.9159 0.0143
-15.750 -0.3569 0.04578 0.03982 -0.2063 0.9141 0.0144
-15.500 -0.3442 0.04428 0.03826 -0.2068 0.9131 0.0146
-15.250 -0.3294 0.04278 0.03670 -0.2077 0.9123 0.0148
-15.000 -0.3128 0.04134 0.03518 -0.2087 0.9116 0.0148
-14.750 -0.2948 0.03994 0.03373 -0.2099 0.9109 0.0149
-14.500 -0.2762 0.03856 0.03228 -0.2112 0.9103 0.0152
-14.250 -0.2559 0.03729 0.03095 -0.2127 0.9097 0.0154
-13.250 -0.3271 0.03568 0.02922 -0.1841 0.8747 0.0156
-13.000 -0.3123 0.03460 0.02808 -0.1838 0.8720 0.0159
-12.750 -0.2944 0.03342 0.02683 -0.1843 0.8702 0.0160
-12.500 -0.2915 0.03274 0.02609 -0.1814 0.8630 0.0161
-12.250 -0.2740 0.03169 0.02499 -0.1815 0.8599 0.0163
-12.000 -0.2519 0.03061 0.02383 -0.1826 0.8575 0.0166
-11.750 -0.2308 0.02938 0.02255 -0.1837 0.8550 0.0167
-11.500 -0.2184 0.02835 0.02148 -0.1830 0.8492 0.0171
-11.250 -0.1952 0.02732 0.02041 -0.1843 0.8454 0.0174
-11.000 -0.1677 0.02629 0.01931 -0.1864 0.8424 0.0179
-10.750 -0.1458 0.02550 0.01847 -0.1871 0.8379 0.0182
-10.500 -0.1272 0.02475 0.01764 -0.1872 0.8326 0.0186
-10.250 -0.1015 0.02402 0.01684 -0.1887 0.8284 0.0192
-10.000 -0.0813 0.02335 0.01610 -0.1889 0.8237 0.0196
-9.750 -0.0701 0.02288 0.01556 -0.1871 0.8174 0.0199
-9.500 -0.0515 0.02229 0.01490 -0.1870 0.8125 0.0204
-9.250 -0.0381 0.02179 0.01434 -0.1857 0.8078 0.0208
-9.000 -0.0334 0.02143 0.01396 -0.1824 0.8025 0.0212
-8.750 -0.0211 0.02102 0.01349 -0.1807 0.7981 0.0219
-8.500 -0.0021 0.02059 0.01300 -0.1803 0.7945 0.0226
-8.250 0.0004 0.02031 0.01269 -0.1765 0.7899 0.0233
-8.000 0.0055 0.02006 0.01240 -0.1731 0.7853 0.0238
-7.750 0.0158 0.01970 0.01201 -0.1708 0.7814 0.0251
-7.500 0.0310 0.01932 0.01159 -0.1695 0.7783 0.0271
-7.250 0.0356 0.01906 0.01132 -0.1660 0.7749 0.0291
-7.000 0.0367 0.01880 0.01108 -0.1618 0.7712 0.0326
-6.750 0.0378 0.01844 0.01075 -0.1576 0.7674 0.0435
-6.500 0.0427 0.01802 0.01038 -0.1544 0.7640 0.0605
-6.250 0.0492 0.01748 0.00992 -0.1515 0.7610 0.0873
-6.000 0.0428 0.01719 0.00970 -0.1457 0.7576 0.1035
-5.750 0.0349 0.01681 0.00943 -0.1398 0.7540 0.1285
-5.500 0.0298 0.01642 0.00912 -0.1343 0.7507 0.1546
-5.250 0.0223 0.01585 0.00870 -0.1286 0.7476 0.1945
-5.000 0.0177 0.01524 0.00822 -0.1234 0.7448 0.2379
-4.750 -0.0036 0.01478 0.00790 -0.1147 0.7412 0.2737
-4.500 -0.0282 0.01443 0.00766 -0.1050 0.7371 0.2998
-4.250 -0.0593 0.01397 0.00730 -0.0941 0.7333 0.3310
-4.000 -0.0747 0.01347 0.00687 -0.0862 0.7303 0.3627
-3.750 -0.0878 0.01240 0.00615 -0.0792 0.7277 0.4510
-3.500 -0.0942 0.01175 0.00584 -0.0733 0.7249 0.5282
-3.250 -0.0904 0.01141 0.00579 -0.0691 0.7220 0.5983
-3.000 -0.0758 0.01131 0.00585 -0.0669 0.7193 0.6438
-2.750 -0.0547 0.01132 0.00589 -0.0660 0.7168 0.6687
-2.500 -0.0293 0.01134 0.00589 -0.0660 0.7147 0.6811
-2.250 -0.0008 0.01133 0.00583 -0.0666 0.7129 0.6865
-2.000 0.0296 0.01132 0.00580 -0.0676 0.7113 0.6918
-1.750 0.0534 0.01138 0.00582 -0.0674 0.7093 0.6980
-1.500 0.0716 0.01148 0.00590 -0.0660 0.7070 0.7028
-1.250 0.0918 0.01157 0.00600 -0.0650 0.7044 0.7052
-1.000 0.1132 0.01166 0.00608 -0.0643 0.7020 0.7079
-0.750 0.1368 0.01171 0.00611 -0.0640 0.6996 0.7109
-0.500 0.1637 0.01173 0.00608 -0.0644 0.6975 0.7138
-0.250 0.1930 0.01173 0.00602 -0.0653 0.6959 0.7165
0.000 0.2247 0.01172 0.00594 -0.0667 0.6943 0.7190
0.250 0.2439 0.01185 0.00609 -0.0655 0.6922 0.7216
0.500 0.2606 0.01202 0.00630 -0.0639 0.6896 0.7245
0.750 0.2800 0.01216 0.00645 -0.0628 0.6869 0.7276
1.000 0.3018 0.01227 0.00655 -0.0622 0.6844 0.7306
1.250 0.3266 0.01234 0.00659 -0.0623 0.6822 0.7335
1.500 0.3543 0.01237 0.00658 -0.0629 0.6804 0.7363
1.750 0.3837 0.01239 0.00659 -0.0638 0.6787 0.7387
2.000 0.4140 0.01242 0.00660 -0.0649 0.6771 0.7414
2.250 0.4247 0.01272 0.00696 -0.0621 0.6742 0.7449
2.500 0.4404 0.01295 0.00722 -0.0604 0.6712 0.7485
2.750 0.4604 0.01313 0.00739 -0.0596 0.6685 0.7519
3.000 0.4835 0.01325 0.00751 -0.0593 0.6663 0.7549
3.250 0.5094 0.01333 0.00760 -0.0596 0.6644 0.7574
3.500 0.5381 0.01337 0.00764 -0.0604 0.6625 0.7602
3.750 0.5686 0.01339 0.00765 -0.0615 0.6606 0.7632
4.000 0.5769 0.01380 0.00811 -0.0585 0.6574 0.7674
4.250 0.5915 0.01411 0.00844 -0.0567 0.6542 0.7714
4.500 0.6094 0.01436 0.00873 -0.0554 0.6511 0.7741
4.750 0.6327 0.01450 0.00889 -0.0552 0.6486 0.7770
5.000 0.6603 0.01455 0.00894 -0.0559 0.6463 0.7800
5.250 0.6899 0.01457 0.00895 -0.0569 0.6441 0.7831
5.500 0.6935 0.01516 0.00960 -0.0531 0.6398 0.7873
5.750 0.7063 0.01556 0.01005 -0.0510 0.6359 0.7904
6.000 0.7263 0.01579 0.01030 -0.0503 0.6324 0.7933
6.250 0.7531 0.01585 0.01036 -0.0507 0.6296 0.7963
6.500 0.7721 0.01613 0.01066 -0.0499 0.6262 0.7997
6.750 0.7767 0.01681 0.01139 -0.0465 0.6209 0.8036
7.000 0.7934 0.01716 0.01175 -0.0452 0.6167 0.8065
7.250 0.8174 0.01728 0.01189 -0.0452 0.6133 0.8087
7.500 0.8325 0.01770 0.01234 -0.0437 0.6090 0.8114
7.750 0.8381 0.01844 0.01315 -0.0406 0.6030 0.8148
8.000 0.8561 0.01877 0.01347 -0.0396 0.5979 0.8180
8.250 0.8732 0.01915 0.01386 -0.0386 0.5927 0.8213
8.500 0.8795 0.01994 0.01470 -0.0358 0.5859 0.8241
8.750 0.8966 0.02031 0.01508 -0.0347 0.5801 0.8262
9.000 0.9049 0.02106 0.01588 -0.0323 0.5732 0.8286
9.250 0.9154 0.02173 0.01658 -0.0302 0.5652 0.8312
9.500 0.9244 0.02250 0.01736 -0.0280 0.5564 0.8341
9.750 0.9354 0.02319 0.01804 -0.0262 0.5469 0.8370
10.000 0.9418 0.02414 0.01900 -0.0237 0.5361 0.8399
10.250 0.9497 0.02499 0.01983 -0.0215 0.5235 0.8420
10.500 0.9527 0.02607 0.02089 -0.0185 0.5082 0.8440
10.750 0.9565 0.02716 0.02194 -0.0158 0.4920 0.8461
11.000 0.9567 0.02847 0.02320 -0.0127 0.4740 0.8484
11.250 0.9557 0.02988 0.02453 -0.0095 0.4538 0.8509
11.500 0.9561 0.03130 0.02590 -0.0066 0.4367 0.8534
11.750 0.9555 0.03281 0.02734 -0.0037 0.4179 0.8558
12.000 0.9558 0.03435 0.02881 -0.0011 0.4004 0.8578
12.250 0.9542 0.03598 0.03038 0.0017 0.3819 0.8594
12.500 0.9573 0.03738 0.03176 0.0039 0.3676 0.8610
12.750 0.9570 0.03904 0.03337 0.0064 0.3495 0.8627
13.000 0.9592 0.04059 0.03489 0.0084 0.3348 0.8646
13.250 0.9622 0.04213 0.03638 0.0103 0.3193 0.8665
13.500 0.9616 0.04395 0.03814 0.0125 0.3010 0.8684
13.750 0.9670 0.04542 0.03958 0.0139 0.2884 0.8700
14.000 0.9699 0.04712 0.04123 0.0155 0.2738 0.8718
14.250 0.9728 0.04884 0.04289 0.0170 0.2577 0.8734
14.500 0.9789 0.05039 0.04441 0.0181 0.2444 0.8748
14.750 0.9822 0.05208 0.04607 0.0195 0.2298 0.8763
15.000 0.9865 0.05371 0.04766 0.0207 0.2159 0.8776
15.250 0.9919 0.05533 0.04927 0.0218 0.2056 0.8790
15.500 0.9958 0.05707 0.05099 0.0229 0.1930 0.8804
15.750 1.0028 0.05862 0.05252 0.0237 0.1814 0.8819
16.000 1.0083 0.06032 0.05422 0.0245 0.1715 0.8834
16.250 1.0134 0.06208 0.05594 0.0252 0.1613 0.8850
16.500 1.0175 0.06395 0.05777 0.0260 0.1488 0.8864
16.750 1.0253 0.06556 0.05941 0.0264 0.1421 0.8880
17.000 1.0302 0.06744 0.06125 0.0269 0.1328 0.8893
17.250 1.0349 0.06938 0.06316 0.0274 0.1223 0.8904
17.500 1.0420 0.07108 0.06489 0.0277 0.1174 0.8916
17.750 1.0484 0.07282 0.06665 0.0281 0.1104 0.8929
18.000 1.0526 0.07481 0.06864 0.0285 0.1035 0.8940
18.250 1.0587 0.07665 0.07051 0.0288 0.0980 0.8951
18.500 1.0639 0.07860 0.07246 0.0290 0.0929 0.8961
18.750 1.0703 0.08046 0.07437 0.0290 0.0881 0.8972
19.000 1.0764 0.08239 0.07632 0.0290 0.0846 0.8983
19.250 1.0815 0.08442 0.07837 0.0290 0.0804 0.8996
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