HAWKER TEMPEST 37.5% SEMISPAN AIRFOIL (tempest1-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: HAWKER TEMPEST 37.5% SEMISPAN AIRFOIL (tempest1-il) Reynolds number: 500,000 Max Cl/Cd: 62.23 at α=5.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-tempest1-il-500000-n5.txt Download as CSV file: xf-tempest1-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: HAWKER TEMPEST 37.5% SEMISPAN 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
------ -------- --------- --------- -------- -------- --------
-19.250 -0.7457 0.15035 0.14750 -0.0241 1.0000 0.0091
-19.000 -0.7764 0.13900 0.13601 -0.0297 1.0000 0.0091
-18.750 -0.8039 0.12903 0.12592 -0.0347 1.0000 0.0090
-18.500 -0.8286 0.11996 0.11672 -0.0393 1.0000 0.0091
-18.250 -0.8494 0.11199 0.10864 -0.0433 1.0000 0.0090
-18.000 -0.8694 0.10430 0.10083 -0.0472 1.0000 0.0090
-17.750 -0.8928 0.09622 0.09262 -0.0512 1.0000 0.0090
-17.500 -0.9137 0.08870 0.08497 -0.0550 1.0000 0.0090
-17.250 -0.9320 0.08177 0.07790 -0.0586 1.0000 0.0091
-17.000 -0.9484 0.07534 0.07133 -0.0619 1.0000 0.0091
-16.750 -0.9649 0.06922 0.06508 -0.0649 1.0000 0.0091
-16.500 -0.9777 0.06386 0.05958 -0.0675 1.0000 0.0091
-16.250 -0.9892 0.05900 0.05458 -0.0696 1.0000 0.0092
-16.000 -1.0008 0.05443 0.04987 -0.0712 1.0000 0.0092
-15.750 -1.0079 0.05067 0.04598 -0.0723 1.0000 0.0093
-15.500 -1.0141 0.04727 0.04246 -0.0730 1.0000 0.0094
-15.250 -1.0187 0.04427 0.03934 -0.0731 1.0000 0.0094
-15.000 -1.0217 0.04162 0.03656 -0.0729 1.0000 0.0096
-14.750 -1.0242 0.03923 0.03405 -0.0723 1.0000 0.0096
-14.500 -1.0260 0.03707 0.03178 -0.0714 1.0000 0.0097
-14.250 -1.0293 0.03495 0.02956 -0.0699 1.0000 0.0099
-14.000 -1.0314 0.03311 0.02763 -0.0682 1.0000 0.0099
-13.750 -1.0345 0.03135 0.02580 -0.0660 1.0000 0.0102
-13.500 -1.0343 0.02995 0.02433 -0.0636 1.0000 0.0103
-13.250 -1.0332 0.02873 0.02303 -0.0611 1.0000 0.0106
-13.000 -1.0312 0.02769 0.02192 -0.0583 1.0000 0.0107
-12.750 -1.0297 0.02673 0.02088 -0.0552 1.0000 0.0108
-12.500 -1.0283 0.02588 0.01997 -0.0519 1.0000 0.0110
-12.250 -1.0270 0.02516 0.01919 -0.0483 1.0000 0.0113
-12.000 -1.0268 0.02447 0.01844 -0.0443 1.0000 0.0116
-11.750 -1.0054 0.02352 0.01738 -0.0446 0.9981 0.0120
-11.500 -0.9827 0.02271 0.01648 -0.0450 0.9956 0.0124
-11.250 -0.9624 0.02182 0.01550 -0.0449 0.9927 0.0127
-11.000 -0.9431 0.02093 0.01457 -0.0445 0.9893 0.0134
-10.750 -0.9197 0.02023 0.01380 -0.0446 0.9864 0.0138
-10.500 -0.8948 0.01953 0.01305 -0.0450 0.9840 0.0143
-10.250 -0.8712 0.01891 0.01236 -0.0451 0.9810 0.0151
-10.000 -0.8495 0.01837 0.01174 -0.0445 0.9767 0.0157
-9.750 -0.8254 0.01768 0.01101 -0.0446 0.9734 0.0167
-9.500 -0.7982 0.01709 0.01039 -0.0451 0.9711 0.0178
-9.250 -0.7703 0.01658 0.00983 -0.0458 0.9690 0.0195
-9.000 -0.7512 0.01609 0.00929 -0.0445 0.9629 0.0207
-8.750 -0.7243 0.01556 0.00875 -0.0449 0.9596 0.0227
-8.500 -0.6940 0.01508 0.00822 -0.0459 0.9572 0.0249
-8.250 -0.6618 0.01451 0.00766 -0.0474 0.9553 0.0290
-8.000 -0.6419 0.01410 0.00724 -0.0461 0.9480 0.0334
-7.750 -0.6129 0.01361 0.00677 -0.0469 0.9437 0.0403
-7.500 -0.5810 0.01311 0.00631 -0.0482 0.9405 0.0505
-7.250 -0.5599 0.01276 0.00599 -0.0471 0.9327 0.0598
-7.000 -0.5311 0.01236 0.00562 -0.0477 0.9276 0.0716
-6.750 -0.5050 0.01203 0.00531 -0.0477 0.9214 0.0822
-6.500 -0.4799 0.01175 0.00504 -0.0474 0.9145 0.0924
-6.250 -0.4518 0.01146 0.00474 -0.0477 0.9089 0.1035
-6.000 -0.4299 0.01121 0.00452 -0.0467 0.9007 0.1135
-5.750 -0.4031 0.01093 0.00425 -0.0467 0.8945 0.1254
-5.500 -0.3819 0.01071 0.00404 -0.0455 0.8861 0.1378
-5.250 -0.3571 0.01043 0.00380 -0.0450 0.8792 0.1549
-5.000 -0.3362 0.01020 0.00361 -0.0437 0.8708 0.1727
-4.500 -0.2921 0.00969 0.00321 -0.0417 0.8551 0.2184
-4.250 -0.2696 0.00943 0.00302 -0.0407 0.8478 0.2471
-4.000 -0.2501 0.00915 0.00285 -0.0391 0.8394 0.2832
-3.750 -0.2292 0.00886 0.00267 -0.0378 0.8319 0.3214
-3.500 -0.2104 0.00858 0.00253 -0.0361 0.8231 0.3636
-3.250 -0.1912 0.00830 0.00239 -0.0344 0.8153 0.4108
-3.000 -0.1721 0.00807 0.00228 -0.0326 0.8067 0.4524
-2.750 -0.1513 0.00790 0.00218 -0.0312 0.7989 0.4869
-2.500 -0.1312 0.00773 0.00210 -0.0296 0.7904 0.5209
-2.250 -0.1099 0.00760 0.00203 -0.0282 0.7825 0.5502
-2.000 -0.0885 0.00749 0.00197 -0.0268 0.7739 0.5755
-1.750 -0.0665 0.00739 0.00192 -0.0256 0.7655 0.5988
-1.500 -0.0447 0.00730 0.00187 -0.0242 0.7568 0.6226
-1.250 -0.0227 0.00722 0.00184 -0.0230 0.7477 0.6453
-1.000 -0.0016 0.00713 0.00181 -0.0215 0.7388 0.6738
-0.750 0.0186 0.00703 0.00181 -0.0197 0.7289 0.7075
-0.250 0.0631 0.00695 0.00184 -0.0171 0.7096 0.7591
0.000 0.0866 0.00694 0.00186 -0.0161 0.6992 0.7779
0.250 0.1106 0.00695 0.00189 -0.0152 0.6887 0.7948
0.500 0.1348 0.00699 0.00192 -0.0143 0.6775 0.8091
0.750 0.1593 0.00702 0.00195 -0.0136 0.6652 0.8212
1.000 0.1832 0.00707 0.00198 -0.0127 0.6525 0.8324
1.250 0.2084 0.00714 0.00203 -0.0121 0.6399 0.8424
1.500 0.2335 0.00721 0.00208 -0.0115 0.6280 0.8516
1.750 0.2576 0.00729 0.00214 -0.0106 0.6167 0.8613
2.000 0.2848 0.00737 0.00222 -0.0105 0.6050 0.8689
2.500 0.3366 0.00756 0.00238 -0.0097 0.5831 0.8841
2.750 0.3601 0.00766 0.00246 -0.0088 0.5709 0.8924
3.000 0.3879 0.00780 0.00258 -0.0089 0.5556 0.8981
3.500 0.4373 0.00811 0.00280 -0.0076 0.5206 0.9116
3.750 0.4654 0.00829 0.00295 -0.0078 0.5031 0.9169
4.000 0.4854 0.00843 0.00305 -0.0062 0.4857 0.9246
4.250 0.5162 0.00866 0.00324 -0.0070 0.4641 0.9281
4.500 0.5429 0.00891 0.00342 -0.0070 0.4415 0.9329
4.750 0.5612 0.00917 0.00359 -0.0051 0.4139 0.9403
5.000 0.5906 0.00954 0.00385 -0.0058 0.3819 0.9431
5.250 0.6179 0.00993 0.00412 -0.0060 0.3501 0.9468
5.500 0.6379 0.01030 0.00438 -0.0047 0.3210 0.9533
5.750 0.6653 0.01075 0.00471 -0.0050 0.2893 0.9565
6.000 0.6940 0.01127 0.00508 -0.0058 0.2538 0.9591
6.250 0.7187 0.01181 0.00546 -0.0057 0.2189 0.9628
6.500 0.7353 0.01226 0.00579 -0.0037 0.1908 0.9695
6.750 0.7632 0.01280 0.00619 -0.0044 0.1614 0.9715
7.000 0.7901 0.01329 0.00658 -0.0048 0.1391 0.9741
7.250 0.8148 0.01373 0.00695 -0.0047 0.1216 0.9775
7.500 0.8337 0.01417 0.00734 -0.0034 0.1060 0.9825
7.750 0.8615 0.01463 0.00774 -0.0041 0.0915 0.9844
8.000 0.8873 0.01514 0.00818 -0.0045 0.0765 0.9869
8.250 0.9112 0.01567 0.00864 -0.0045 0.0621 0.9899
8.500 0.9337 0.01619 0.00913 -0.0042 0.0516 0.9930
8.750 0.9578 0.01674 0.00964 -0.0043 0.0425 0.9956
9.000 0.9823 0.01732 0.01019 -0.0045 0.0356 0.9980
9.250 1.0071 0.01791 0.01079 -0.0049 0.0305 0.9999
9.500 1.0129 0.01831 0.01121 -0.0012 0.0284 1.0000
9.750 1.0171 0.01876 0.01168 0.0027 0.0260 1.0000
10.000 1.0216 0.01929 0.01222 0.0064 0.0240 1.0000
10.250 1.0287 0.01978 0.01275 0.0097 0.0223 1.0000
10.500 1.0359 0.02034 0.01334 0.0127 0.0211 1.0000
10.750 1.0422 0.02102 0.01404 0.0158 0.0195 1.0000
11.000 1.0505 0.02166 0.01474 0.0185 0.0185 1.0000
11.250 1.0589 0.02236 0.01549 0.0210 0.0176 1.0000
11.500 1.0672 0.02311 0.01628 0.0234 0.0169 1.0000
11.750 1.0744 0.02399 0.01719 0.0258 0.0161 1.0000
12.000 1.0809 0.02497 0.01821 0.0281 0.0154 1.0000
12.250 1.0894 0.02589 0.01921 0.0301 0.0148 1.0000
12.500 1.0980 0.02683 0.02021 0.0319 0.0142 1.0000
12.750 1.1062 0.02786 0.02132 0.0337 0.0136 1.0000
13.000 1.1127 0.02907 0.02259 0.0354 0.0133 1.0000
13.250 1.1191 0.03033 0.02390 0.0370 0.0128 1.0000
13.500 1.1248 0.03171 0.02534 0.0385 0.0124 1.0000
13.750 1.1279 0.03335 0.02705 0.0400 0.0121 1.0000
14.000 1.1325 0.03494 0.02873 0.0412 0.0118 1.0000
14.250 1.1386 0.03647 0.03035 0.0422 0.0114 1.0000
14.500 1.1409 0.03840 0.03237 0.0432 0.0113 1.0000
14.750 1.1456 0.04019 0.03425 0.0440 0.0109 1.0000
15.000 1.1479 0.04227 0.03642 0.0446 0.0107 1.0000
15.250 1.1493 0.04452 0.03876 0.0451 0.0105 1.0000
15.500 1.1522 0.04671 0.04103 0.0454 0.0102 1.0000
15.750 1.1508 0.04945 0.04386 0.0456 0.0102 1.0000
16.000 1.1494 0.05227 0.04677 0.0455 0.0099 1.0000
16.250 1.1476 0.05524 0.04982 0.0452 0.0097 1.0000
16.500 1.1409 0.05892 0.05360 0.0447 0.0095 1.0000
16.750 1.1360 0.06249 0.05726 0.0440 0.0094 1.0000
17.000 1.1336 0.06586 0.06074 0.0432 0.0093 1.0000
17.250 1.1247 0.07018 0.06518 0.0421 0.0093 1.0000
17.500 1.1220 0.07381 0.06893 0.0410 0.0091 1.0000
17.750 1.1138 0.07830 0.07355 0.0395 0.0090 1.0000
18.000 1.1073 0.08266 0.07803 0.0379 0.0089 1.0000
18.250 1.0979 0.08757 0.08306 0.0360 0.0087 1.0000
18.500 1.0902 0.09234 0.08794 0.0340 0.0086 1.0000
18.750 1.0778 0.09791 0.09363 0.0317 0.0085 1.0000
19.000 1.0663 0.10341 0.09925 0.0293 0.0086 1.0000
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