HAWKER TEMPEST 61% SEMISPAN AIRFOIL (tempest2-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: HAWKER TEMPEST 61% SEMISPAN AIRFOIL (tempest2-il) Reynolds number: 1,000,000 Max Cl/Cd: 69.26 at α=8.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-tempest2-il-1000000-n5.txt Download as CSV file: xf-tempest2-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: HAWKER TEMPEST 61% SEMISPAN 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
------ -------- --------- --------- -------- -------- --------
-17.500 -0.8029 0.12981 0.12777 -0.0188 1.0000 0.0046
-17.250 -0.8511 0.11544 0.11328 -0.0259 1.0000 0.0045
-17.000 -0.8976 0.10217 0.09991 -0.0326 1.0000 0.0045
-16.750 -0.9619 0.08588 0.08343 -0.0411 1.0000 0.0044
-16.500 -1.0085 0.07266 0.07002 -0.0486 1.0000 0.0044
-16.250 -1.0429 0.06219 0.05935 -0.0551 1.0000 0.0042
-16.000 -1.0589 0.05570 0.05272 -0.0592 1.0000 0.0043
-15.750 -1.0880 0.04810 0.04490 -0.0633 1.0000 0.0043
-15.500 -1.0971 0.04398 0.04064 -0.0649 1.0000 0.0043
-15.250 -1.1029 0.04068 0.03722 -0.0656 1.0000 0.0044
-15.000 -1.1045 0.03810 0.03453 -0.0657 1.0000 0.0044
-14.750 -1.1076 0.03563 0.03194 -0.0652 1.0000 0.0045
-14.500 -1.1184 0.03276 0.02890 -0.0637 1.0000 0.0045
-14.250 -1.1128 0.03143 0.02749 -0.0625 1.0000 0.0046
-14.000 -1.1147 0.02966 0.02559 -0.0605 1.0000 0.0046
-13.750 -1.1127 0.02829 0.02412 -0.0583 1.0000 0.0046
-13.500 -1.1061 0.02732 0.02307 -0.0562 1.0000 0.0047
-13.250 -1.1034 0.02621 0.02185 -0.0534 1.0000 0.0048
-13.000 -1.1019 0.02514 0.02066 -0.0502 1.0000 0.0048
-12.750 -1.1001 0.02423 0.01965 -0.0466 1.0000 0.0049
-12.500 -1.0981 0.02349 0.01884 -0.0428 1.0000 0.0049
-12.250 -1.1000 0.02279 0.01805 -0.0380 1.0000 0.0050
-12.000 -1.1075 0.02203 0.01720 -0.0320 0.9999 0.0051
-11.750 -1.0860 0.02098 0.01605 -0.0320 0.9983 0.0052
-11.500 -1.0622 0.02013 0.01512 -0.0323 0.9963 0.0054
-11.250 -1.0366 0.01943 0.01437 -0.0327 0.9943 0.0056
-11.000 -1.0151 0.01860 0.01344 -0.0323 0.9918 0.0057
-10.750 -0.9906 0.01798 0.01276 -0.0323 0.9894 0.0059
-10.500 -0.9652 0.01735 0.01205 -0.0325 0.9871 0.0061
-10.250 -0.9386 0.01673 0.01136 -0.0329 0.9852 0.0063
-10.000 -0.9110 0.01614 0.01071 -0.0335 0.9837 0.0065
-9.750 -0.8850 0.01560 0.01010 -0.0337 0.9816 0.0068
-9.500 -0.8618 0.01509 0.00953 -0.0332 0.9778 0.0069
-9.250 -0.8351 0.01462 0.00900 -0.0334 0.9751 0.0071
-9.000 -0.8080 0.01399 0.00831 -0.0338 0.9728 0.0076
-8.750 -0.7783 0.01346 0.00775 -0.0347 0.9712 0.0080
-8.500 -0.7465 0.01302 0.00727 -0.0360 0.9698 0.0084
-8.250 -0.7218 0.01265 0.00687 -0.0357 0.9649 0.0089
-8.000 -0.6930 0.01226 0.00643 -0.0362 0.9610 0.0093
-7.750 -0.6615 0.01189 0.00602 -0.0373 0.9578 0.0098
-7.500 -0.6315 0.01146 0.00555 -0.0381 0.9537 0.0107
-7.250 -0.6048 0.01113 0.00520 -0.0382 0.9469 0.0116
-7.000 -0.5744 0.01080 0.00483 -0.0390 0.9416 0.0125
-6.750 -0.5484 0.01054 0.00453 -0.0388 0.9342 0.0133
-6.500 -0.5211 0.01023 0.00421 -0.0389 0.9273 0.0157
-6.250 -0.4961 0.00999 0.00394 -0.0385 0.9195 0.0179
-6.000 -0.4701 0.00974 0.00366 -0.0382 0.9119 0.0210
-5.750 -0.4458 0.00951 0.00343 -0.0376 0.9033 0.0251
-5.500 -0.4213 0.00927 0.00319 -0.0370 0.8949 0.0321
-5.250 -0.3979 0.00901 0.00296 -0.0362 0.8859 0.0439
-5.000 -0.3746 0.00874 0.00274 -0.0354 0.8773 0.0607
-4.750 -0.3505 0.00855 0.00256 -0.0347 0.8687 0.0744
-4.500 -0.3264 0.00837 0.00241 -0.0341 0.8600 0.0873
-4.250 -0.3025 0.00818 0.00225 -0.0333 0.8511 0.1045
-4.000 -0.2785 0.00801 0.00211 -0.0326 0.8420 0.1199
-3.750 -0.2546 0.00784 0.00197 -0.0319 0.8331 0.1387
-3.250 -0.2087 0.00737 0.00170 -0.0301 0.8153 0.2055
-3.000 -0.1854 0.00717 0.00158 -0.0292 0.8064 0.2386
-2.750 -0.1629 0.00693 0.00146 -0.0282 0.7972 0.2822
-2.500 -0.1397 0.00673 0.00136 -0.0273 0.7882 0.3222
-2.250 -0.1171 0.00652 0.00126 -0.0264 0.7787 0.3656
-2.000 -0.0950 0.00629 0.00118 -0.0252 0.7685 0.4176
-1.750 -0.0724 0.00610 0.00111 -0.0242 0.7582 0.4631
-1.500 -0.0493 0.00597 0.00105 -0.0233 0.7481 0.5003
-1.250 -0.0265 0.00583 0.00100 -0.0222 0.7368 0.5391
-1.000 -0.0027 0.00575 0.00097 -0.0214 0.7249 0.5660
-0.750 0.0205 0.00567 0.00094 -0.0204 0.7123 0.5966
-0.500 0.0434 0.00559 0.00092 -0.0194 0.6994 0.6276
-0.250 0.0657 0.00551 0.00090 -0.0182 0.6845 0.6609
0.000 0.0853 0.00539 0.00090 -0.0164 0.6680 0.7109
0.250 0.1060 0.00532 0.00092 -0.0148 0.6517 0.7520
0.500 0.1288 0.00531 0.00094 -0.0137 0.6361 0.7784
0.750 0.1520 0.00531 0.00098 -0.0126 0.6212 0.8011
1.000 0.1762 0.00533 0.00101 -0.0118 0.6077 0.8208
1.250 0.2009 0.00537 0.00106 -0.0111 0.5944 0.8359
1.500 0.2259 0.00542 0.00110 -0.0105 0.5809 0.8489
1.750 0.2509 0.00548 0.00116 -0.0099 0.5653 0.8601
2.000 0.2752 0.00559 0.00122 -0.0091 0.5444 0.8707
2.250 0.2995 0.00571 0.00129 -0.0084 0.5208 0.8813
2.500 0.3248 0.00583 0.00137 -0.0079 0.5004 0.8902
2.750 0.3498 0.00596 0.00145 -0.0073 0.4774 0.8988
3.000 0.3749 0.00612 0.00155 -0.0068 0.4530 0.9073
3.250 0.3999 0.00632 0.00167 -0.0063 0.4232 0.9148
3.500 0.4239 0.00656 0.00180 -0.0056 0.3880 0.9228
3.750 0.4490 0.00684 0.00196 -0.0052 0.3526 0.9293
4.000 0.4739 0.00714 0.00214 -0.0048 0.3153 0.9362
4.250 0.4976 0.00752 0.00234 -0.0042 0.2704 0.9424
4.500 0.5240 0.00797 0.00259 -0.0043 0.2208 0.9474
4.750 0.5462 0.00837 0.00282 -0.0034 0.1805 0.9542
5.000 0.5756 0.00876 0.00307 -0.0041 0.1466 0.9575
5.250 0.6047 0.00921 0.00336 -0.0049 0.1124 0.9607
5.500 0.6317 0.00958 0.00363 -0.0050 0.0886 0.9651
5.750 0.6574 0.00991 0.00389 -0.0048 0.0713 0.9699
6.000 0.6896 0.01032 0.00421 -0.0062 0.0529 0.9715
6.250 0.7195 0.01073 0.00454 -0.0071 0.0379 0.9735
6.500 0.7482 0.01110 0.00487 -0.0076 0.0286 0.9757
6.750 0.7753 0.01145 0.00520 -0.0078 0.0230 0.9784
7.000 0.7990 0.01176 0.00550 -0.0073 0.0196 0.9821
7.250 0.8275 0.01212 0.00585 -0.0078 0.0164 0.9837
7.500 0.8572 0.01245 0.00620 -0.0086 0.0145 0.9850
7.750 0.8855 0.01287 0.00661 -0.0092 0.0123 0.9866
8.000 0.9136 0.01320 0.00698 -0.0097 0.0117 0.9884
8.250 0.9406 0.01358 0.00737 -0.0099 0.0107 0.9905
8.500 0.9662 0.01400 0.00780 -0.0100 0.0099 0.9927
8.750 0.9913 0.01451 0.00834 -0.0099 0.0090 0.9947
9.000 1.0190 0.01492 0.00880 -0.0104 0.0086 0.9963
9.250 1.0464 0.01534 0.00925 -0.0109 0.0081 0.9979
9.500 1.0735 0.01578 0.00972 -0.0114 0.0075 0.9992
9.750 1.0951 0.01627 0.01024 -0.0107 0.0072 1.0000
10.000 1.0999 0.01661 0.01064 -0.0064 0.0071 1.0000
10.250 1.1031 0.01699 0.01105 -0.0018 0.0068 1.0000
10.500 1.1061 0.01755 0.01167 0.0026 0.0064 1.0000
10.750 1.1149 0.01799 0.01215 0.0058 0.0063 1.0000
11.000 1.1255 0.01843 0.01265 0.0086 0.0061 1.0000
11.250 1.1356 0.01897 0.01324 0.0113 0.0061 1.0000
11.500 1.1463 0.01955 0.01388 0.0139 0.0058 1.0000
11.750 1.1576 0.02014 0.01453 0.0162 0.0056 1.0000
12.000 1.1678 0.02085 0.01530 0.0185 0.0056 1.0000
12.250 1.1790 0.02153 0.01605 0.0206 0.0053 1.0000
12.500 1.1893 0.02230 0.01689 0.0226 0.0052 1.0000
12.750 1.1994 0.02313 0.01777 0.0246 0.0050 1.0000
13.000 1.2095 0.02400 0.01870 0.0264 0.0049 1.0000
13.250 1.2174 0.02505 0.01982 0.0283 0.0048 1.0000
13.500 1.2253 0.02615 0.02098 0.0300 0.0046 1.0000
13.750 1.2308 0.02748 0.02240 0.0318 0.0045 1.0000
14.000 1.2330 0.02912 0.02414 0.0337 0.0043 1.0000
14.250 1.2402 0.03044 0.02554 0.0349 0.0043 1.0000
14.500 1.2424 0.03223 0.02744 0.0363 0.0042 1.0000
14.750 1.2471 0.03390 0.02922 0.0373 0.0042 1.0000
15.000 1.2506 0.03575 0.03116 0.0382 0.0041 1.0000
15.250 1.2533 0.03774 0.03325 0.0389 0.0041 1.0000
15.500 1.2523 0.04022 0.03584 0.0394 0.0041 1.0000
15.750 1.2533 0.04259 0.03832 0.0396 0.0039 1.0000
16.000 1.2525 0.04527 0.04110 0.0396 0.0039 1.0000
16.250 1.2452 0.04887 0.04484 0.0392 0.0039 1.0000
16.500 1.2439 0.05190 0.04797 0.0386 0.0039 1.0000
16.750 1.2385 0.05559 0.05178 0.0376 0.0038 1.0000
17.000 1.2274 0.06027 0.05659 0.0361 0.0038 1.0000
17.250 1.2157 0.06525 0.06171 0.0343 0.0038 1.0000
17.500 1.2043 0.07040 0.06698 0.0321 0.0037 1.0000
17.750 1.1906 0.07616 0.07287 0.0295 0.0037 1.0000
18.000 1.1736 0.08267 0.07952 0.0264 0.0037 1.0000
18.250 1.1493 0.09068 0.08768 0.0225 0.0038 1.0000
18.500 1.1240 0.09923 0.09637 0.0182 0.0037 1.0000
18.750 1.1063 0.10646 0.10371 0.0146 0.0036 1.0000
19.000 1.0717 0.11714 0.11456 0.0093 0.0038 1.0000
19.250 1.0418 0.12720 0.12474 0.0043 0.0038 1.0000
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