WHITCOMB INTEGRAL SUPERCRITICAL AIRFOIL (whitcomb-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: WHITCOMB INTEGRAL SUPERCRITICAL AIRFOIL (whitcomb-il) Reynolds number: 1,000,000 Max Cl/Cd: 76.88 at α=7.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-whitcomb-il-1000000-n5.txt Download as CSV file: xf-whitcomb-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WHITCOMB INTEGRAL SUPERCRITICAL 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
------ -------- --------- --------- -------- -------- --------
-19.000 -1.0902 0.10811 0.10502 -0.0412 1.0000 0.0156
-18.750 -1.1234 0.09847 0.09523 -0.0463 1.0000 0.0156
-18.500 -1.1543 0.08933 0.08595 -0.0511 1.0000 0.0155
-18.250 -1.1829 0.08076 0.07723 -0.0557 1.0000 0.0155
-18.000 -1.2067 0.07318 0.06951 -0.0597 1.0000 0.0155
-17.750 -1.2267 0.06656 0.06274 -0.0631 1.0000 0.0156
-17.500 -1.2430 0.06083 0.05689 -0.0657 1.0000 0.0156
-17.250 -1.2563 0.05596 0.05189 -0.0676 1.0000 0.0157
-17.000 -1.2672 0.05175 0.04758 -0.0688 1.0000 0.0157
-16.750 -1.2752 0.04825 0.04397 -0.0694 1.0000 0.0158
-16.500 -1.2818 0.04516 0.04080 -0.0695 1.0000 0.0159
-16.250 -1.2865 0.04253 0.03808 -0.0691 1.0000 0.0159
-16.000 -1.2900 0.04022 0.03570 -0.0683 1.0000 0.0160
-15.750 -1.2927 0.03819 0.03359 -0.0672 1.0000 0.0161
-15.500 -1.2945 0.03639 0.03172 -0.0659 1.0000 0.0162
-15.250 -1.2864 0.03461 0.02987 -0.0662 0.9995 0.0163
-15.000 -1.2756 0.03294 0.02813 -0.0667 0.9989 0.0164
-14.750 -1.2624 0.03146 0.02659 -0.0673 0.9980 0.0166
-14.500 -1.2489 0.03007 0.02514 -0.0678 0.9972 0.0167
-14.250 -1.2337 0.02884 0.02384 -0.0682 0.9963 0.0169
-14.000 -1.2176 0.02767 0.02261 -0.0688 0.9955 0.0170
-13.750 -1.1998 0.02660 0.02148 -0.0693 0.9947 0.0172
-13.500 -1.1806 0.02560 0.02043 -0.0700 0.9941 0.0173
-13.250 -1.1666 0.02468 0.01946 -0.0695 0.9926 0.0175
-13.000 -1.1523 0.02384 0.01858 -0.0689 0.9906 0.0177
-12.750 -1.1354 0.02304 0.01772 -0.0687 0.9888 0.0179
-12.500 -1.1138 0.02224 0.01687 -0.0693 0.9875 0.0181
-12.250 -1.0894 0.02149 0.01607 -0.0702 0.9865 0.0183
-12.000 -1.0635 0.02078 0.01532 -0.0714 0.9856 0.0185
-11.750 -1.0369 0.02002 0.01452 -0.0728 0.9849 0.0188
-11.500 -1.0097 0.01927 0.01374 -0.0742 0.9844 0.0192
-11.250 -0.9818 0.01863 0.01308 -0.0756 0.9839 0.0196
-11.000 -0.9657 0.01806 0.01249 -0.0745 0.9814 0.0199
-10.750 -0.9426 0.01752 0.01193 -0.0746 0.9796 0.0203
-10.500 -0.9165 0.01699 0.01138 -0.0753 0.9785 0.0208
-10.250 -0.8890 0.01650 0.01086 -0.0763 0.9775 0.0213
-10.000 -0.8605 0.01603 0.01037 -0.0773 0.9767 0.0217
-9.750 -0.8314 0.01556 0.00988 -0.0785 0.9761 0.0223
-9.500 -0.8016 0.01509 0.00941 -0.0797 0.9755 0.0232
-9.250 -0.7714 0.01467 0.00899 -0.0810 0.9750 0.0241
-9.000 -0.7404 0.01429 0.00859 -0.0824 0.9746 0.0250
-8.750 -0.7088 0.01393 0.00822 -0.0838 0.9742 0.0259
-8.500 -0.6769 0.01353 0.00784 -0.0853 0.9738 0.0272
-8.250 -0.6447 0.01318 0.00750 -0.0868 0.9735 0.0286
-8.000 -0.6125 0.01288 0.00718 -0.0882 0.9732 0.0298
-7.750 -0.5800 0.01255 0.00686 -0.0897 0.9730 0.0313
-7.500 -0.5477 0.01225 0.00658 -0.0911 0.9727 0.0331
-7.250 -0.5156 0.01200 0.00633 -0.0924 0.9725 0.0347
-7.000 -0.4985 0.01176 0.00610 -0.0905 0.9692 0.0360
-6.750 -0.4695 0.01150 0.00586 -0.0911 0.9682 0.0380
-6.500 -0.4395 0.01127 0.00564 -0.0919 0.9673 0.0397
-6.250 -0.4085 0.01104 0.00542 -0.0928 0.9666 0.0417
-6.000 -0.3769 0.01080 0.00520 -0.0939 0.9660 0.0443
-5.750 -0.3451 0.01059 0.00501 -0.0950 0.9654 0.0469
-5.500 -0.3129 0.01035 0.00482 -0.0962 0.9649 0.0516
-5.250 -0.2804 0.01012 0.00465 -0.0975 0.9645 0.0587
-5.000 -0.2476 0.00988 0.00448 -0.0988 0.9642 0.0681
-4.750 -0.2147 0.00967 0.00433 -0.1001 0.9638 0.0769
-4.500 -0.1817 0.00947 0.00419 -0.1015 0.9635 0.0865
-4.250 -0.1487 0.00929 0.00406 -0.1028 0.9632 0.0968
-3.750 -0.0810 0.00887 0.00381 -0.1058 0.9627 0.1271
-3.500 -0.0447 0.00861 0.00366 -0.1078 0.9623 0.1495
-3.250 -0.0062 0.00832 0.00349 -0.1102 0.9618 0.1725
-3.000 0.0337 0.00800 0.00329 -0.1130 0.9613 0.2045
-2.750 0.0791 0.00752 0.00298 -0.1170 0.9605 0.2447
-2.500 0.1116 0.00701 0.00268 -0.1181 0.9537 0.2985
-2.250 0.1640 0.00602 0.00212 -0.1241 0.9487 0.4233
-2.000 0.2073 0.00529 0.00177 -0.1280 0.9416 0.5348
-1.750 0.2446 0.00504 0.00175 -0.1298 0.9314 0.6074
-1.500 0.2775 0.00502 0.00175 -0.1305 0.9143 0.6263
-1.250 0.2927 0.00641 0.00181 -0.1272 0.6066 0.6359
-1.000 0.3103 0.00749 0.00213 -0.1250 0.4102 0.6423
-0.750 0.3356 0.00795 0.00229 -0.1244 0.3336 0.6470
-0.500 0.3625 0.00831 0.00241 -0.1241 0.2798 0.6520
-0.250 0.3886 0.00869 0.00259 -0.1236 0.2290 0.6557
0.000 0.4142 0.00906 0.00284 -0.1229 0.1899 0.6592
0.250 0.4404 0.00941 0.00306 -0.1222 0.1604 0.6631
0.500 0.4676 0.00970 0.00323 -0.1219 0.1337 0.6661
0.750 0.4955 0.00994 0.00334 -0.1218 0.1117 0.6676
1.000 0.5237 0.01013 0.00345 -0.1217 0.0975 0.6685
1.250 0.5517 0.01033 0.00357 -0.1216 0.0844 0.6694
1.500 0.5795 0.01050 0.00367 -0.1214 0.0721 0.6705
1.750 0.6073 0.01067 0.00379 -0.1212 0.0632 0.6712
2.000 0.6351 0.01086 0.00391 -0.1211 0.0560 0.6717
2.250 0.6629 0.01103 0.00405 -0.1209 0.0505 0.6722
2.500 0.6909 0.01119 0.00418 -0.1208 0.0467 0.6726
2.750 0.7187 0.01138 0.00433 -0.1206 0.0433 0.6730
3.000 0.7466 0.01154 0.00448 -0.1204 0.0412 0.6734
3.250 0.7743 0.01172 0.00464 -0.1202 0.0389 0.6737
3.500 0.8019 0.01193 0.00482 -0.1200 0.0367 0.6741
3.750 0.8295 0.01210 0.00499 -0.1198 0.0351 0.6746
4.000 0.8569 0.01231 0.00518 -0.1195 0.0333 0.6751
4.250 0.8842 0.01254 0.00539 -0.1192 0.0317 0.6756
4.500 0.9116 0.01273 0.00559 -0.1190 0.0306 0.6760
4.750 0.9390 0.01294 0.00579 -0.1187 0.0294 0.6764
5.000 0.9660 0.01318 0.00602 -0.1184 0.0281 0.6768
5.250 0.9930 0.01344 0.00627 -0.1181 0.0271 0.6772
5.500 1.0200 0.01366 0.00651 -0.1177 0.0263 0.6776
5.750 1.0468 0.01391 0.00676 -0.1174 0.0254 0.6779
6.000 1.0735 0.01418 0.00702 -0.1170 0.0246 0.6783
6.250 1.0998 0.01448 0.00732 -0.1166 0.0237 0.6787
6.500 1.1261 0.01478 0.00763 -0.1161 0.0231 0.6791
6.750 1.1524 0.01506 0.00793 -0.1157 0.0226 0.6794
7.000 1.1785 0.01536 0.00825 -0.1152 0.0221 0.6798
7.250 1.2044 0.01568 0.00859 -0.1147 0.0216 0.6802
7.500 1.2301 0.01600 0.00892 -0.1141 0.0211 0.6806
7.750 1.2555 0.01635 0.00928 -0.1135 0.0206 0.6811
8.000 1.2806 0.01675 0.00969 -0.1129 0.0201 0.6816
8.250 1.3053 0.01717 0.01014 -0.1122 0.0197 0.6819
8.500 1.3302 0.01754 0.01055 -0.1115 0.0195 0.6822
8.750 1.3549 0.01793 0.01098 -0.1108 0.0192 0.6825
9.000 1.3792 0.01834 0.01142 -0.1100 0.0190 0.6828
9.250 1.4033 0.01876 0.01189 -0.1092 0.0187 0.6831
9.500 1.4271 0.01920 0.01237 -0.1083 0.0184 0.6834
9.750 1.4505 0.01965 0.01286 -0.1074 0.0182 0.6837
10.000 1.4736 0.02012 0.01337 -0.1065 0.0180 0.6840
10.250 1.4963 0.02062 0.01391 -0.1055 0.0178 0.6842
10.500 1.5186 0.02113 0.01447 -0.1044 0.0176 0.6845
10.750 1.5404 0.02168 0.01506 -0.1033 0.0174 0.6847
11.000 1.5615 0.02227 0.01570 -0.1020 0.0172 0.6849
11.250 1.5817 0.02292 0.01640 -0.1006 0.0170 0.6852
11.500 1.6007 0.02365 0.01720 -0.0991 0.0168 0.6854
11.750 1.6184 0.02448 0.01809 -0.0973 0.0166 0.6856
12.000 1.6372 0.02513 0.01882 -0.0957 0.0165 0.6859
12.250 1.6552 0.02582 0.01959 -0.0941 0.0164 0.6865
12.500 1.6724 0.02652 0.02039 -0.0923 0.0164 0.6870
12.750 1.6885 0.02727 0.02122 -0.0903 0.0163 0.6874
13.000 1.7032 0.02807 0.02211 -0.0881 0.0162 0.6877
13.250 1.7156 0.02890 0.02303 -0.0856 0.0161 0.6881
13.500 1.7232 0.02974 0.02397 -0.0822 0.0160 0.6884
13.750 1.7317 0.03067 0.02500 -0.0792 0.0160 0.6887
14.000 1.7395 0.03169 0.02611 -0.0761 0.0159 0.6890
14.250 1.7464 0.03277 0.02730 -0.0731 0.0158 0.6894
14.500 1.7519 0.03397 0.02860 -0.0700 0.0157 0.6897
14.750 1.7563 0.03528 0.03002 -0.0669 0.0157 0.6900
15.000 1.7600 0.03667 0.03151 -0.0640 0.0156 0.6903
15.250 1.7627 0.03818 0.03313 -0.0611 0.0155 0.6905
15.500 1.7636 0.03987 0.03494 -0.0583 0.0154 0.6908
15.750 1.7637 0.04173 0.03691 -0.0557 0.0153 0.6911
16.000 1.7612 0.04389 0.03919 -0.0533 0.0153 0.6914
16.250 1.7576 0.04631 0.04173 -0.0512 0.0152 0.6917
16.500 1.7508 0.04923 0.04479 -0.0495 0.0151 0.6919
16.750 1.7413 0.05270 0.04840 -0.0485 0.0151 0.6921
17.000 1.7279 0.05710 0.05296 -0.0485 0.0151 0.6924
17.250 1.7111 0.06266 0.05868 -0.0500 0.0150 0.6926
17.500 1.6866 0.07054 0.06676 -0.0541 0.0150 0.6927
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