HAWKER TEMPEST 37.5% SEMISPAN AIRFOIL (tempest1-il) Xfoil prediction polar at RE=50,000 Ncrit=5
| Details | Polar file |
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Airfoil: HAWKER TEMPEST 37.5% SEMISPAN AIRFOIL (tempest1-il) Reynolds number: 50,000 Max Cl/Cd: 30.18 at α=6.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-tempest1-il-50000-n5.txt Download as CSV file: xf-tempest1-il-50000-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 = 0.050 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.750 -0.6450 0.08368 0.07587 -0.0647 1.0000 0.0546
-12.500 -0.6725 0.07736 0.06946 -0.0672 1.0000 0.0543
-12.250 -0.6983 0.07214 0.06412 -0.0682 1.0000 0.0541
-12.000 -0.7261 0.06753 0.05933 -0.0678 1.0000 0.0541
-11.750 -0.7508 0.06375 0.05537 -0.0661 1.0000 0.0543
-11.500 -0.7742 0.06047 0.05185 -0.0632 1.0000 0.0545
-11.250 -0.7868 0.05806 0.04937 -0.0601 1.0000 0.0553
-11.000 -0.7925 0.05636 0.04766 -0.0570 1.0000 0.0566
-10.750 -0.8029 0.05455 0.04576 -0.0530 1.0000 0.0576
-10.500 -0.8141 0.05277 0.04385 -0.0484 1.0000 0.0587
-10.250 -0.8229 0.05081 0.04171 -0.0440 1.0000 0.0602
-10.000 -0.8280 0.04865 0.03930 -0.0400 1.0000 0.0618
-9.750 -0.8311 0.04646 0.03677 -0.0360 1.0000 0.0640
-9.500 -0.8290 0.04463 0.03475 -0.0326 1.0000 0.0665
-9.250 -0.8256 0.04345 0.03359 -0.0294 1.0000 0.0697
-9.000 -0.8202 0.04188 0.03182 -0.0262 1.0000 0.0735
-8.750 -0.8115 0.04017 0.02982 -0.0234 1.0000 0.0781
-8.500 -0.8049 0.03910 0.02878 -0.0204 1.0000 0.0828
-8.250 -0.7948 0.03770 0.02709 -0.0177 1.0000 0.0901
-8.000 -0.7869 0.03667 0.02614 -0.0148 1.0000 0.0966
-7.750 -0.7765 0.03552 0.02487 -0.0122 1.0000 0.1058
-7.500 -0.7667 0.03455 0.02375 -0.0094 1.0000 0.1164
-7.250 -0.7571 0.03360 0.02283 -0.0067 1.0000 0.1272
-7.000 -0.7473 0.03271 0.02192 -0.0040 1.0000 0.1401
-6.750 -0.7370 0.03187 0.02107 -0.0014 1.0000 0.1541
-6.500 -0.7261 0.03108 0.02026 0.0012 1.0000 0.1695
-6.250 -0.7150 0.03032 0.01950 0.0037 1.0000 0.1863
-6.000 -0.7031 0.02960 0.01874 0.0060 1.0000 0.2046
-5.750 -0.6912 0.02887 0.01807 0.0084 1.0000 0.2239
-5.500 -0.6800 0.02814 0.01743 0.0108 1.0000 0.2457
-5.250 -0.6690 0.02742 0.01682 0.0133 1.0000 0.2720
-5.000 -0.6565 0.02666 0.01626 0.0154 0.9992 0.3077
-4.750 -0.6301 0.02587 0.01582 0.0149 0.9928 0.3702
-4.500 -0.6056 0.02524 0.01564 0.0151 0.9860 0.4556
-4.250 -0.5784 0.02497 0.01571 0.0153 0.9796 0.5420
-4.000 -0.5474 0.02501 0.01591 0.0152 0.9732 0.6147
-3.750 -0.5115 0.02533 0.01627 0.0144 0.9677 0.6732
-3.500 -0.4754 0.02576 0.01667 0.0136 0.9613 0.7197
-3.250 -0.4312 0.02643 0.01720 0.0114 0.9565 0.7588
-3.000 -0.3911 0.02708 0.01770 0.0099 0.9505 0.7916
-2.750 -0.3453 0.02788 0.01832 0.0075 0.9452 0.8209
-2.500 -0.2962 0.02866 0.01891 0.0042 0.9409 0.8471
-2.250 -0.2443 0.02930 0.01936 0.0000 0.9356 0.8648
-2.000 -0.1937 0.02973 0.01961 -0.0043 0.9301 0.8802
-1.750 -0.1424 0.03002 0.01971 -0.0091 0.9256 0.8940
-1.500 -0.0979 0.03017 0.01974 -0.0128 0.9182 0.9055
-1.250 -0.0480 0.03025 0.01969 -0.0177 0.9126 0.9157
-1.000 -0.0066 0.03028 0.01962 -0.0210 0.9056 0.9271
-0.500 0.0888 0.03017 0.01936 -0.0302 0.8933 0.9455
-0.250 0.1253 0.03014 0.01930 -0.0328 0.8842 0.9560
0.000 0.1796 0.02991 0.01903 -0.0386 0.8795 0.9628
0.250 0.2167 0.02984 0.01896 -0.0414 0.8697 0.9721
0.500 0.2693 0.02954 0.01866 -0.0469 0.8645 0.9788
0.750 0.3092 0.02939 0.01853 -0.0502 0.8547 0.9869
1.250 0.4019 0.02883 0.01807 -0.0589 0.8390 1.0000
1.500 0.4303 0.02863 0.01790 -0.0596 0.8298 1.0000
1.750 0.4550 0.02849 0.01781 -0.0594 0.8192 1.0000
2.000 0.4724 0.02850 0.01786 -0.0580 0.8068 1.0000
2.250 0.4943 0.02842 0.01783 -0.0572 0.7956 1.0000
2.500 0.5274 0.02809 0.01757 -0.0582 0.7866 1.0000
2.750 0.5434 0.02812 0.01766 -0.0562 0.7732 1.0000
3.000 0.5611 0.02811 0.01771 -0.0545 0.7600 1.0000
3.250 0.5809 0.02805 0.01772 -0.0530 0.7473 1.0000
3.500 0.6041 0.02790 0.01766 -0.0520 0.7349 1.0000
3.750 0.6316 0.02761 0.01745 -0.0516 0.7229 1.0000
4.000 0.6532 0.02747 0.01740 -0.0501 0.7093 1.0000
4.250 0.6710 0.02743 0.01746 -0.0481 0.6946 1.0000
4.500 0.6898 0.02735 0.01747 -0.0461 0.6795 1.0000
4.750 0.7100 0.02721 0.01742 -0.0442 0.6636 1.0000
5.000 0.7320 0.02699 0.01728 -0.0426 0.6468 1.0000
5.250 0.7435 0.02706 0.01745 -0.0393 0.6275 1.0000
5.500 0.7585 0.02702 0.01748 -0.0365 0.6073 1.0000
5.750 0.7783 0.02684 0.01735 -0.0343 0.5864 1.0000
6.000 0.7900 0.02693 0.01750 -0.0310 0.5643 1.0000
6.250 0.8036 0.02697 0.01760 -0.0279 0.5407 1.0000
6.500 0.8130 0.02716 0.01782 -0.0243 0.5161 1.0000
6.750 0.8241 0.02731 0.01797 -0.0209 0.4899 1.0000
7.000 0.8314 0.02759 0.01825 -0.0170 0.4626 1.0000
7.250 0.8369 0.02794 0.01857 -0.0128 0.4336 1.0000
7.500 0.8417 0.02837 0.01894 -0.0086 0.4043 1.0000
7.750 0.8442 0.02889 0.01935 -0.0041 0.3753 1.0000
8.000 0.8447 0.02950 0.01983 0.0005 0.3475 1.0000
8.250 0.8444 0.03024 0.02042 0.0051 0.3207 1.0000
8.500 0.8439 0.03110 0.02116 0.0094 0.2952 1.0000
8.750 0.8435 0.03208 0.02203 0.0135 0.2705 1.0000
9.000 0.8431 0.03317 0.02298 0.0174 0.2480 1.0000
9.250 0.8433 0.03434 0.02411 0.0209 0.2258 1.0000
9.500 0.8435 0.03561 0.02529 0.0241 0.2057 1.0000
9.750 0.8437 0.03697 0.02655 0.0272 0.1878 1.0000
10.000 0.8448 0.03842 0.02795 0.0300 0.1703 1.0000
10.250 0.8466 0.03995 0.02945 0.0325 0.1546 1.0000
10.500 0.8486 0.04157 0.03103 0.0348 0.1404 1.0000
10.750 0.8512 0.04326 0.03267 0.0369 0.1279 1.0000
11.000 0.8534 0.04502 0.03441 0.0389 0.1163 1.0000
11.250 0.8585 0.04682 0.03633 0.0406 0.1056 1.0000
11.500 0.8644 0.04865 0.03821 0.0422 0.0971 1.0000
11.750 0.8699 0.05047 0.04001 0.0436 0.0901 1.0000
12.000 0.8771 0.05248 0.04222 0.0450 0.0832 1.0000
12.250 0.8821 0.05440 0.04413 0.0462 0.0779 1.0000
12.500 0.8897 0.05664 0.04657 0.0474 0.0733 1.0000
12.750 0.8926 0.05903 0.04917 0.0484 0.0693 1.0000
13.000 0.8973 0.06113 0.05126 0.0493 0.0660 1.0000
13.250 0.8988 0.06403 0.05437 0.0501 0.0635 1.0000
13.500 0.8946 0.06753 0.05817 0.0507 0.0616 1.0000
13.750 0.8870 0.07126 0.06216 0.0509 0.0600 1.0000
14.000 0.8775 0.07526 0.06636 0.0507 0.0584 1.0000
14.250 0.8670 0.07949 0.07076 0.0502 0.0573 1.0000
14.500 0.8579 0.08358 0.07495 0.0493 0.0560 1.0000
14.750 0.8480 0.08806 0.07955 0.0482 0.0552 1.0000
15.000 0.8352 0.09319 0.08476 0.0466 0.0544 1.0000
15.250 0.8098 0.10071 0.09248 0.0431 0.0544 1.0000
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