CLARK YM-15 AIRFOIL (clarym15-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: CLARK YM-15 AIRFOIL (clarym15-il) Reynolds number: 1,000,000 Max Cl/Cd: 105.13 at α=7.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-clarym15-il-1000000-n5.txt Download as CSV file: xf-clarym15-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: CLARK YM-15 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
------ -------- --------- --------- -------- -------- --------
-18.500 -0.8657 0.10974 0.10715 -0.0487 1.0000 0.0216
-18.250 -0.9050 0.09907 0.09635 -0.0548 1.0000 0.0217
-18.000 -0.9388 0.08978 0.08692 -0.0602 1.0000 0.0217
-17.750 -0.9767 0.08034 0.07735 -0.0659 1.0000 0.0218
-17.500 -1.0139 0.07130 0.06817 -0.0714 1.0000 0.0218
-17.250 -1.0479 0.06269 0.05942 -0.0768 1.0000 0.0218
-17.000 -1.0765 0.05458 0.05115 -0.0822 1.0000 0.0219
-16.750 -1.0958 0.04753 0.04395 -0.0875 1.0000 0.0219
-16.500 -1.1065 0.04185 0.03812 -0.0921 1.0000 0.0220
-16.250 -1.1110 0.03751 0.03365 -0.0955 1.0000 0.0221
-16.000 -1.1119 0.03423 0.03025 -0.0977 1.0000 0.0222
-15.750 -1.1106 0.03175 0.02766 -0.0987 1.0000 0.0223
-15.500 -1.1084 0.02980 0.02562 -0.0987 1.0000 0.0224
-15.250 -1.1073 0.02828 0.02401 -0.0975 1.0000 0.0224
-15.000 -1.1112 0.02711 0.02277 -0.0946 1.0000 0.0225
-14.500 -1.0816 0.02420 0.01968 -0.0955 0.9926 0.0230
-14.250 -1.0636 0.02323 0.01866 -0.0953 0.9870 0.0232
-14.000 -1.0406 0.02236 0.01773 -0.0958 0.9833 0.0234
-13.750 -1.0193 0.02159 0.01691 -0.0957 0.9784 0.0236
-13.500 -0.9971 0.02088 0.01614 -0.0956 0.9731 0.0238
-13.250 -0.9743 0.02022 0.01541 -0.0954 0.9682 0.0240
-13.000 -0.9535 0.01963 0.01477 -0.0948 0.9616 0.0242
-12.750 -0.9309 0.01908 0.01416 -0.0943 0.9558 0.0245
-12.500 -0.9097 0.01856 0.01359 -0.0936 0.9489 0.0247
-12.250 -0.8878 0.01804 0.01300 -0.0929 0.9422 0.0249
-12.000 -0.8658 0.01753 0.01242 -0.0921 0.9353 0.0251
-11.750 -0.8435 0.01705 0.01187 -0.0914 0.9278 0.0253
-11.500 -0.8205 0.01659 0.01133 -0.0908 0.9209 0.0255
-11.250 -0.7972 0.01615 0.01083 -0.0902 0.9129 0.0257
-11.000 -0.7735 0.01574 0.01034 -0.0896 0.9055 0.0259
-10.750 -0.7493 0.01535 0.00988 -0.0891 0.8972 0.0260
-10.500 -0.7248 0.01499 0.00945 -0.0886 0.8892 0.0262
-10.250 -0.6999 0.01464 0.00904 -0.0882 0.8807 0.0264
-10.000 -0.6766 0.01414 0.00846 -0.0876 0.8722 0.0268
-9.750 -0.6521 0.01372 0.00799 -0.0871 0.8631 0.0271
-9.500 -0.6271 0.01337 0.00757 -0.0866 0.8546 0.0274
-9.250 -0.6016 0.01305 0.00720 -0.0863 0.8455 0.0277
-9.000 -0.5759 0.01276 0.00684 -0.0859 0.8372 0.0280
-8.750 -0.5499 0.01248 0.00651 -0.0856 0.8289 0.0283
-8.500 -0.5238 0.01222 0.00620 -0.0853 0.8213 0.0286
-8.250 -0.4973 0.01197 0.00590 -0.0850 0.8137 0.0290
-8.000 -0.4709 0.01174 0.00561 -0.0847 0.8061 0.0293
-7.750 -0.4440 0.01150 0.00533 -0.0845 0.7994 0.0296
-7.500 -0.4172 0.01129 0.00507 -0.0843 0.7922 0.0300
-7.250 -0.3903 0.01109 0.00482 -0.0841 0.7855 0.0303
-7.000 -0.3630 0.01090 0.00459 -0.0839 0.7783 0.0305
-6.500 -0.3094 0.01046 0.00408 -0.0834 0.7628 0.0320
-6.000 -0.2553 0.01012 0.00367 -0.0830 0.7443 0.0335
-5.750 -0.2283 0.00999 0.00348 -0.0828 0.7356 0.0343
-5.500 -0.2006 0.00985 0.00331 -0.0826 0.7272 0.0351
-5.250 -0.1737 0.00971 0.00313 -0.0824 0.7181 0.0364
-5.000 -0.1462 0.00956 0.00297 -0.0823 0.7094 0.0383
-4.750 -0.1190 0.00945 0.00282 -0.0820 0.7009 0.0404
-4.500 -0.0915 0.00929 0.00267 -0.0819 0.6924 0.0447
-4.250 -0.0645 0.00916 0.00254 -0.0817 0.6833 0.0519
-4.000 -0.0371 0.00903 0.00243 -0.0815 0.6740 0.0608
-3.750 -0.0099 0.00894 0.00233 -0.0813 0.6635 0.0684
-3.500 0.0173 0.00886 0.00224 -0.0811 0.6517 0.0752
-3.250 0.0449 0.00879 0.00216 -0.0810 0.6419 0.0803
-3.000 0.0721 0.00874 0.00208 -0.0808 0.6306 0.0859
-2.750 0.0994 0.00870 0.00201 -0.0806 0.6177 0.0906
-2.500 0.1268 0.00864 0.00195 -0.0804 0.6068 0.0974
-2.250 0.1540 0.00860 0.00189 -0.0802 0.5956 0.1053
-2.000 0.1809 0.00854 0.00183 -0.0800 0.5833 0.1185
-1.750 0.2077 0.00843 0.00178 -0.0798 0.5720 0.1424
-1.500 0.2342 0.00832 0.00175 -0.0795 0.5615 0.1770
-1.250 0.2611 0.00824 0.00173 -0.0793 0.5505 0.2024
-1.000 0.2883 0.00821 0.00172 -0.0791 0.5400 0.2215
-0.750 0.3152 0.00821 0.00172 -0.0789 0.5288 0.2391
-0.500 0.3424 0.00819 0.00172 -0.0787 0.5173 0.2594
-0.250 0.3694 0.00819 0.00174 -0.0785 0.5057 0.2788
0.000 0.3962 0.00823 0.00176 -0.0783 0.4922 0.2949
0.250 0.4227 0.00827 0.00179 -0.0780 0.4767 0.3127
0.500 0.4489 0.00830 0.00183 -0.0777 0.4600 0.3396
0.750 0.4746 0.00828 0.00188 -0.0773 0.4425 0.3828
1.000 0.4997 0.00827 0.00194 -0.0769 0.4227 0.4385
1.250 0.5242 0.00824 0.00203 -0.0763 0.4008 0.5067
1.500 0.5481 0.00820 0.00213 -0.0756 0.3807 0.5863
1.750 0.5723 0.00817 0.00224 -0.0750 0.3648 0.6604
2.000 0.5974 0.00818 0.00234 -0.0744 0.3530 0.7115
2.250 0.6222 0.00821 0.00246 -0.0738 0.3429 0.7595
2.500 0.6474 0.00821 0.00257 -0.0732 0.3349 0.8054
2.750 0.6721 0.00828 0.00270 -0.0725 0.3270 0.8424
3.000 0.6976 0.00832 0.00282 -0.0719 0.3222 0.8740
3.250 0.7227 0.00839 0.00294 -0.0712 0.3175 0.9054
3.500 0.7482 0.00850 0.00308 -0.0706 0.3130 0.9310
3.750 0.7756 0.00863 0.00321 -0.0704 0.3086 0.9501
4.000 0.8064 0.00876 0.00334 -0.0710 0.3051 0.9680
4.250 0.8410 0.00893 0.00348 -0.0725 0.2998 0.9817
4.500 0.8764 0.00916 0.00366 -0.0743 0.2919 0.9904
5.000 0.9537 0.00957 0.00398 -0.0793 0.2773 1.0000
5.250 0.9746 0.00969 0.00409 -0.0780 0.2729 1.0000
5.500 0.9960 0.00981 0.00420 -0.0767 0.2690 1.0000
5.750 1.0173 0.00995 0.00433 -0.0754 0.2649 1.0000
6.000 1.0388 0.01012 0.00447 -0.0742 0.2611 1.0000
6.250 1.0614 0.01027 0.00462 -0.0732 0.2578 1.0000
6.500 1.0847 0.01041 0.00477 -0.0724 0.2539 1.0000
6.750 1.1075 0.01059 0.00493 -0.0715 0.2484 1.0000
7.000 1.1298 0.01081 0.00512 -0.0705 0.2430 1.0000
7.250 1.1533 0.01097 0.00529 -0.0698 0.2387 1.0000
7.500 1.1758 0.01119 0.00549 -0.0689 0.2321 1.0000
7.750 1.1973 0.01143 0.00570 -0.0679 0.2248 1.0000
8.000 1.2170 0.01173 0.00594 -0.0665 0.2145 1.0000
8.250 1.2367 0.01202 0.00621 -0.0651 0.2043 1.0000
8.500 1.2548 0.01241 0.00653 -0.0636 0.1915 1.0000
8.750 1.2717 0.01287 0.00692 -0.0619 0.1772 1.0000
9.000 1.2871 0.01343 0.00738 -0.0600 0.1613 1.0000
9.250 1.3016 0.01406 0.00792 -0.0580 0.1455 1.0000
9.500 1.3161 0.01470 0.00848 -0.0562 0.1313 1.0000
9.750 1.3320 0.01528 0.00901 -0.0546 0.1206 1.0000
10.000 1.3481 0.01587 0.00956 -0.0530 0.1120 1.0000
10.500 1.3807 0.01704 0.01068 -0.0502 0.0991 1.0000
10.750 1.3963 0.01768 0.01130 -0.0488 0.0940 1.0000
11.000 1.4128 0.01828 0.01191 -0.0475 0.0897 1.0000
11.250 1.4282 0.01896 0.01259 -0.0462 0.0854 1.0000
11.500 1.4427 0.01971 0.01333 -0.0448 0.0813 1.0000
11.750 1.4589 0.02037 0.01401 -0.0437 0.0788 1.0000
12.000 1.4737 0.02112 0.01478 -0.0425 0.0759 1.0000
12.250 1.4872 0.02199 0.01565 -0.0412 0.0728 1.0000
12.500 1.5015 0.02282 0.01650 -0.0400 0.0705 1.0000
12.750 1.5157 0.02366 0.01737 -0.0389 0.0681 1.0000
13.000 1.5282 0.02465 0.01838 -0.0377 0.0653 1.0000
13.250 1.5392 0.02577 0.01950 -0.0365 0.0626 1.0000
13.500 1.5521 0.02676 0.02054 -0.0355 0.0607 1.0000
13.750 1.5630 0.02793 0.02173 -0.0344 0.0578 1.0000
14.000 1.5708 0.02937 0.02316 -0.0331 0.0542 1.0000
14.250 1.5791 0.03080 0.02462 -0.0320 0.0503 1.0000
14.500 1.5844 0.03250 0.02633 -0.0308 0.0461 1.0000
14.750 1.5875 0.03446 0.02828 -0.0296 0.0411 1.0000
15.000 1.5874 0.03677 0.03059 -0.0285 0.0345 1.0000
15.250 1.5710 0.04070 0.03447 -0.0268 0.0213 1.0000
15.500 1.5640 0.04393 0.03774 -0.0259 0.0169 1.0000
15.750 1.5638 0.04661 0.04047 -0.0253 0.0154 1.0000
16.000 1.5624 0.04946 0.04339 -0.0249 0.0143 1.0000
16.250 1.5627 0.05221 0.04621 -0.0246 0.0136 1.0000
16.500 1.5621 0.05514 0.04922 -0.0245 0.0131 1.0000
16.750 1.5600 0.05831 0.05246 -0.0245 0.0126 1.0000
17.000 1.5567 0.06168 0.05591 -0.0246 0.0122 1.0000
17.250 1.5520 0.06527 0.05958 -0.0248 0.0118 1.0000
17.500 1.5482 0.06883 0.06323 -0.0252 0.0116 1.0000
17.750 1.5440 0.07250 0.06699 -0.0257 0.0113 1.0000
18.000 1.5384 0.07640 0.07098 -0.0262 0.0111 1.0000
18.250 1.5314 0.08052 0.07519 -0.0270 0.0108 1.0000
18.500 1.5233 0.08487 0.07963 -0.0278 0.0106 1.0000
18.750 1.5144 0.08940 0.08425 -0.0289 0.0104 1.0000
19.000 1.5045 0.09412 0.08907 -0.0300 0.0102 1.0000
19.250 1.4936 0.09902 0.09407 -0.0313 0.0100 1.0000
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