TH 25816 HALE AIRFOIL (th25816-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: TH 25816 HALE AIRFOIL (th25816-il) Reynolds number: 1,000,000 Max Cl/Cd: 74.91 at α=6° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-th25816-il-1000000.txt Download as CSV file: xf-th25816-il-1000000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -0.3244 0.07344 0.06986 -0.2284 0.9506 0.0143
-19.500 -0.3981 0.07341 0.06977 -0.2121 0.9428 0.0141
-19.250 -0.4029 0.07017 0.06645 -0.2132 0.9419 0.0142
-19.000 -0.4045 0.06691 0.06310 -0.2149 0.9412 0.0143
-18.750 -0.4103 0.06304 0.05907 -0.2166 0.9407 0.0143
-18.500 -0.4057 0.06016 0.05610 -0.2186 0.9404 0.0144
-18.250 -0.4033 0.05715 0.05297 -0.2203 0.9400 0.0144
-18.000 -0.3909 0.05498 0.05076 -0.2227 0.9396 0.0146
-17.750 -0.3851 0.05223 0.04787 -0.2244 0.9393 0.0145
-17.500 -0.3754 0.04983 0.04537 -0.2261 0.9391 0.0146
-17.250 -0.3604 0.04794 0.04341 -0.2283 0.9388 0.0147
-17.000 -0.3464 0.04600 0.04139 -0.2301 0.9386 0.0148
-16.750 -0.3315 0.04424 0.03955 -0.2317 0.9383 0.0149
-16.500 -0.3153 0.04260 0.03784 -0.2334 0.9379 0.0152
-16.250 -0.2979 0.04100 0.03616 -0.2351 0.9376 0.0153
-16.000 -0.2781 0.03956 0.03466 -0.2370 0.9372 0.0155
-15.750 -0.2590 0.03818 0.03321 -0.2386 0.9368 0.0157
-15.500 -0.2859 0.03801 0.03301 -0.2294 0.9312 0.0157
-15.250 -0.2771 0.03692 0.03187 -0.2285 0.9292 0.0160
-15.000 -0.2579 0.03585 0.03075 -0.2293 0.9283 0.0159
-14.750 -0.2388 0.03468 0.02952 -0.2305 0.9275 0.0161
-14.500 -0.2168 0.03356 0.02834 -0.2319 0.9268 0.0163
-14.250 -0.1948 0.03243 0.02714 -0.2336 0.9261 0.0165
-14.000 -0.1709 0.03139 0.02606 -0.2353 0.9255 0.0166
-13.750 -0.1491 0.03030 0.02494 -0.2362 0.9249 0.0169
-13.500 -0.1263 0.02921 0.02382 -0.2377 0.9242 0.0170
-13.250 -0.1039 0.02813 0.02271 -0.2393 0.9235 0.0172
-13.000 -0.0812 0.02714 0.02171 -0.2409 0.9225 0.0177
-12.750 -0.1056 0.02679 0.02135 -0.2316 0.9159 0.0177
-12.500 -0.0877 0.02589 0.02043 -0.2318 0.9141 0.0179
-12.250 -0.0660 0.02492 0.01942 -0.2328 0.9126 0.0182
-12.000 -0.0429 0.02398 0.01845 -0.2341 0.9112 0.0186
-11.750 -0.0191 0.02312 0.01754 -0.2355 0.9098 0.0188
-11.500 -0.0397 0.02276 0.01717 -0.2268 0.9017 0.0190
-11.250 -0.0220 0.02203 0.01640 -0.2266 0.8985 0.0193
-11.000 -0.0351 0.02159 0.01593 -0.2195 0.8891 0.0194
-10.750 -0.0126 0.02086 0.01515 -0.2202 0.8844 0.0197
-10.500 -0.0165 0.02037 0.01459 -0.2151 0.8728 0.0199
-10.250 0.0025 0.01982 0.01398 -0.2149 0.8643 0.0201
-10.000 0.0180 0.01896 0.01300 -0.2146 0.8550 0.0207
-9.750 0.0253 0.01851 0.01246 -0.2118 0.8438 0.0211
-9.500 0.0304 0.01816 0.01204 -0.2085 0.8340 0.0216
-9.000 0.0398 0.01758 0.01132 -0.2016 0.8183 0.0224
-8.750 0.0486 0.01728 0.01096 -0.1990 0.8120 0.0230
-8.500 0.0521 0.01705 0.01069 -0.1951 0.8066 0.0235
-8.000 0.0623 0.01651 0.01005 -0.1881 0.7966 0.0247
-7.750 0.0696 0.01621 0.00973 -0.1852 0.7923 0.0258
-7.500 0.0641 0.01601 0.00952 -0.1793 0.7877 0.0271
-7.250 0.0698 0.01581 0.00929 -0.1758 0.7836 0.0279
-7.000 0.0797 0.01552 0.00897 -0.1733 0.7799 0.0306
-6.750 0.0854 0.01509 0.00860 -0.1702 0.7763 0.0458
-6.500 0.0722 0.01475 0.00836 -0.1630 0.7727 0.0655
-6.250 0.0574 0.01424 0.00800 -0.1557 0.7689 0.1012
-6.000 0.0519 0.01379 0.00765 -0.1502 0.7652 0.1324
-5.750 0.0473 0.01305 0.00711 -0.1454 0.7612 0.1909
-5.500 0.0285 0.01268 0.00686 -0.1369 0.7580 0.2186
-5.250 0.0041 0.01222 0.00654 -0.1274 0.7543 0.2565
-5.000 -0.0147 0.01179 0.00622 -0.1189 0.7509 0.2883
-4.750 -0.0394 0.01121 0.00577 -0.1093 0.7472 0.3314
-4.500 -0.0581 0.01068 0.00533 -0.1007 0.7436 0.3677
-4.250 -0.0870 0.00999 0.00492 -0.0901 0.7406 0.4328
-4.000 -0.0957 0.00921 0.00451 -0.0836 0.7375 0.5215
-3.750 -0.0837 0.00880 0.00432 -0.0811 0.7349 0.5836
-3.500 -0.0614 0.00867 0.00425 -0.0806 0.7326 0.6122
-3.250 -0.0340 0.00861 0.00418 -0.0811 0.7306 0.6308
-3.000 -0.0016 0.00855 0.00412 -0.0826 0.7284 0.6451
-2.750 0.0246 0.00854 0.00413 -0.0828 0.7264 0.6603
-2.500 0.0426 0.00859 0.00423 -0.0812 0.7245 0.6765
-2.250 0.0634 0.00865 0.00431 -0.0802 0.7223 0.6904
-2.000 0.0869 0.00871 0.00436 -0.0798 0.7201 0.6969
-1.750 0.1112 0.00875 0.00436 -0.0796 0.7178 0.7006
-1.500 0.1366 0.00877 0.00436 -0.0796 0.7157 0.7053
-1.250 0.1661 0.00878 0.00436 -0.0805 0.7136 0.7090
-1.000 0.2005 0.00880 0.00433 -0.0824 0.7115 0.7132
-0.750 0.2270 0.00885 0.00436 -0.0827 0.7096 0.7161
-0.500 0.2445 0.00895 0.00445 -0.0812 0.7076 0.7186
-0.250 0.2652 0.00901 0.00451 -0.0802 0.7055 0.7216
0.000 0.2877 0.00905 0.00458 -0.0797 0.7031 0.7245
0.250 0.3117 0.00910 0.00462 -0.0795 0.7009 0.7274
0.500 0.3376 0.00915 0.00465 -0.0797 0.6988 0.7301
0.750 0.3671 0.00918 0.00465 -0.0807 0.6968 0.7328
1.000 0.4017 0.00920 0.00462 -0.0827 0.6948 0.7352
1.250 0.4267 0.00927 0.00469 -0.0827 0.6929 0.7379
1.500 0.4440 0.00937 0.00484 -0.0812 0.6908 0.7414
1.750 0.4639 0.00947 0.00497 -0.0801 0.6884 0.7445
2.000 0.4864 0.00956 0.00506 -0.0796 0.6861 0.7476
2.250 0.5096 0.00965 0.00514 -0.0793 0.6839 0.7506
2.500 0.5352 0.00973 0.00519 -0.0795 0.6820 0.7534
2.750 0.5649 0.00975 0.00521 -0.0805 0.6798 0.7563
3.000 0.6018 0.00975 0.00520 -0.0831 0.6776 0.7591
3.250 0.6154 0.00994 0.00544 -0.0808 0.6754 0.7627
3.500 0.6316 0.01011 0.00564 -0.0791 0.6729 0.7664
3.750 0.6523 0.01025 0.00578 -0.0783 0.6704 0.7698
4.000 0.6741 0.01036 0.00590 -0.0777 0.6678 0.7730
4.250 0.6975 0.01045 0.00602 -0.0774 0.6654 0.7762
4.500 0.7269 0.01050 0.00607 -0.0784 0.6628 0.7791
4.750 0.7558 0.01059 0.00614 -0.0793 0.6602 0.7822
5.000 0.7640 0.01089 0.00649 -0.0761 0.6571 0.7861
5.250 0.7801 0.01110 0.00673 -0.0744 0.6538 0.7895
5.500 0.7984 0.01128 0.00694 -0.0732 0.6506 0.7930
5.750 0.8227 0.01140 0.00706 -0.0731 0.6475 0.7960
6.000 0.8555 0.01142 0.00706 -0.0748 0.6442 0.7988
6.250 0.8617 0.01183 0.00752 -0.0713 0.6410 0.8026
6.500 0.8749 0.01215 0.00787 -0.0692 0.6371 0.8056
6.750 0.8914 0.01239 0.00814 -0.0676 0.6329 0.8089
7.000 0.9171 0.01249 0.00823 -0.0679 0.6292 0.8115
7.250 0.9302 0.01286 0.00865 -0.0658 0.6252 0.8147
7.500 0.9401 0.01331 0.00915 -0.0631 0.6206 0.8182
7.750 0.9568 0.01363 0.00946 -0.0618 0.6161 0.8212
8.000 0.9819 0.01375 0.00954 -0.0620 0.6114 0.8234
8.250 0.9842 0.01442 0.01030 -0.0580 0.6060 0.8268
8.500 0.9965 0.01488 0.01079 -0.0559 0.6000 0.8293
8.750 1.0084 0.01536 0.01127 -0.0537 0.5931 0.8320
9.000 1.0188 0.01595 0.01190 -0.0514 0.5871 0.8349
9.250 1.0316 0.01645 0.01239 -0.0495 0.5802 0.8377
9.500 1.0392 0.01718 0.01314 -0.0468 0.5719 0.8401
9.750 1.0474 0.01784 0.01378 -0.0442 0.5628 0.8429
10.000 1.0567 0.01854 0.01453 -0.0419 0.5550 0.8452
10.250 1.0648 0.01928 0.01527 -0.0394 0.5461 0.8475
10.500 1.0714 0.02014 0.01615 -0.0367 0.5353 0.8499
10.750 1.0757 0.02110 0.01709 -0.0338 0.5229 0.8525
11.000 1.0770 0.02223 0.01819 -0.0304 0.5101 0.8550
11.250 1.0777 0.02344 0.01935 -0.0271 0.4945 0.8571
11.500 1.0740 0.02484 0.02070 -0.0232 0.4773 0.8594
11.750 1.0686 0.02636 0.02218 -0.0192 0.4578 0.8616
12.000 1.0663 0.02779 0.02357 -0.0157 0.4403 0.8636
12.250 1.0626 0.02937 0.02509 -0.0122 0.4231 0.8655
12.500 1.0616 0.03086 0.02653 -0.0091 0.4054 0.8676
12.750 1.0589 0.03249 0.02812 -0.0060 0.3883 0.8697
13.000 1.0587 0.03403 0.02960 -0.0033 0.3708 0.8716
13.250 1.0557 0.03580 0.03129 -0.0004 0.3516 0.8733
13.500 1.0579 0.03730 0.03274 0.0017 0.3358 0.8745
13.750 1.0571 0.03897 0.03435 0.0042 0.3184 0.8763
14.000 1.0584 0.04054 0.03586 0.0063 0.3009 0.8780
14.250 1.0578 0.04228 0.03755 0.0086 0.2838 0.8795
14.500 1.0607 0.04382 0.03904 0.0104 0.2676 0.8811
14.750 1.0606 0.04563 0.04078 0.0124 0.2502 0.8826
15.000 1.0642 0.04721 0.04231 0.0139 0.2350 0.8841
15.250 1.0665 0.04894 0.04397 0.0155 0.2186 0.8856
15.500 1.0694 0.05066 0.04563 0.0169 0.2043 0.8870
15.750 1.0742 0.05227 0.04719 0.0180 0.1906 0.8883
16.000 1.0766 0.05410 0.04896 0.0193 0.1764 0.8895
16.250 1.0818 0.05575 0.05056 0.0202 0.1644 0.8905
16.500 1.0894 0.05718 0.05198 0.0210 0.1544 0.8920
16.750 1.0926 0.05900 0.05376 0.0220 0.1435 0.8934
17.000 1.0959 0.06080 0.05552 0.0230 0.1320 0.8947
17.250 1.1039 0.06228 0.05700 0.0236 0.1247 0.8960
17.500 1.1084 0.06409 0.05880 0.0243 0.1172 0.8973
17.750 1.1145 0.06576 0.06046 0.0249 0.1099 0.8987
18.000 1.1218 0.06737 0.06207 0.0253 0.1041 0.9000
18.250 1.1276 0.06917 0.06388 0.0257 0.0988 0.9013
18.500 1.1328 0.07102 0.06572 0.0261 0.0928 0.9025
18.750 1.1415 0.07258 0.06731 0.0262 0.0885 0.9036
19.000 1.1451 0.07468 0.06939 0.0265 0.0835 0.9046
19.250 1.1532 0.07636 0.07111 0.0265 0.0807 0.9054
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