HAWKER TEMPEST 61% SEMISPAN AIRFOIL (tempest2-il) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
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Airfoil: HAWKER TEMPEST 61% SEMISPAN AIRFOIL (tempest2-il) Reynolds number: 100,000 Max Cl/Cd: 47.28 at α=5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-tempest2-il-100000-n5.txt Download as CSV file: xf-tempest2-il-100000-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 = 0.100 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.500 -0.5823 0.09954 0.09422 -0.0399 1.0000 0.0241
-12.250 -0.6008 0.09048 0.08518 -0.0446 1.0000 0.0239
-12.000 -0.6245 0.08084 0.07551 -0.0508 1.0000 0.0236
-11.750 -0.6454 0.07347 0.06810 -0.0555 1.0000 0.0231
-11.500 -0.6716 0.06684 0.06134 -0.0593 1.0000 0.0229
-11.250 -0.6968 0.06174 0.05609 -0.0607 1.0000 0.0228
-11.000 -0.7183 0.05791 0.05211 -0.0600 1.0000 0.0227
-10.750 -0.7409 0.05458 0.04859 -0.0576 1.0000 0.0227
-10.500 -0.7613 0.05187 0.04569 -0.0537 1.0000 0.0227
-10.250 -0.7816 0.04958 0.04320 -0.0486 1.0000 0.0228
-10.000 -0.7958 0.04718 0.04056 -0.0438 1.0000 0.0229
-9.750 -0.8079 0.04475 0.03779 -0.0390 1.0000 0.0235
-9.500 -0.8145 0.04251 0.03520 -0.0346 1.0000 0.0239
-9.250 -0.8174 0.04029 0.03273 -0.0306 1.0000 0.0246
-9.000 -0.8145 0.03860 0.03095 -0.0274 1.0000 0.0255
-8.750 -0.8101 0.03686 0.02901 -0.0241 1.0000 0.0260
-8.500 -0.8039 0.03518 0.02712 -0.0209 1.0000 0.0267
-8.250 -0.7958 0.03349 0.02519 -0.0179 1.0000 0.0275
-8.000 -0.7857 0.03185 0.02332 -0.0151 1.0000 0.0283
-7.750 -0.7742 0.03032 0.02153 -0.0124 1.0000 0.0295
-7.500 -0.7616 0.02903 0.02001 -0.0099 1.0000 0.0310
-7.250 -0.7499 0.02776 0.01863 -0.0073 1.0000 0.0329
-7.000 -0.7384 0.02676 0.01760 -0.0048 1.0000 0.0350
-6.750 -0.7257 0.02580 0.01655 -0.0023 1.0000 0.0371
-6.500 -0.7130 0.02483 0.01544 0.0003 1.0000 0.0396
-6.250 -0.7013 0.02388 0.01442 0.0029 1.0000 0.0428
-6.000 -0.6774 0.02306 0.01353 0.0031 0.9971 0.0490
-5.750 -0.6488 0.02209 0.01254 0.0023 0.9924 0.0577
-5.500 -0.6201 0.02127 0.01172 0.0016 0.9872 0.0742
-5.250 -0.5893 0.02052 0.01106 0.0003 0.9827 0.0998
-5.000 -0.5626 0.01989 0.01048 0.0000 0.9766 0.1289
-4.750 -0.5323 0.01927 0.00998 -0.0011 0.9715 0.1639
-4.500 -0.5055 0.01863 0.00953 -0.0015 0.9656 0.2064
-4.250 -0.4791 0.01791 0.00909 -0.0019 0.9594 0.2670
-4.000 -0.4515 0.01710 0.00871 -0.0024 0.9546 0.3599
-3.750 -0.4318 0.01642 0.00849 -0.0011 0.9468 0.4632
-3.500 -0.4021 0.01595 0.00837 -0.0013 0.9421 0.5625
-3.250 -0.3760 0.01570 0.00832 -0.0007 0.9355 0.6347
-3.000 -0.3422 0.01559 0.00834 -0.0014 0.9306 0.6949
-2.500 -0.2685 0.01570 0.00845 -0.0041 0.9215 0.7816
-2.250 -0.2291 0.01585 0.00856 -0.0059 0.9170 0.8134
-2.000 -0.1837 0.01609 0.00874 -0.0088 0.9141 0.8436
-1.750 -0.1364 0.01637 0.00892 -0.0120 0.9119 0.8693
-1.500 -0.0975 0.01663 0.00911 -0.0138 0.9055 0.8859
-1.250 -0.0536 0.01675 0.00913 -0.0168 0.9012 0.8983
-1.000 -0.0028 0.01680 0.00910 -0.0214 0.8983 0.9057
-0.750 0.0355 0.01685 0.00909 -0.0235 0.8913 0.9145
-0.500 0.0797 0.01682 0.00901 -0.0269 0.8860 0.9212
-0.250 0.1213 0.01676 0.00890 -0.0297 0.8804 0.9282
0.000 0.1624 0.01672 0.00884 -0.0325 0.8728 0.9343
0.250 0.2014 0.01661 0.00871 -0.0348 0.8662 0.9414
0.500 0.2433 0.01652 0.00862 -0.0378 0.8575 0.9463
0.750 0.2803 0.01642 0.00853 -0.0398 0.8487 0.9532
1.000 0.3221 0.01625 0.00838 -0.0426 0.8401 0.9579
1.250 0.3602 0.01614 0.00830 -0.0449 0.8288 0.9633
1.500 0.3949 0.01603 0.00823 -0.0463 0.8170 0.9697
1.750 0.4355 0.01583 0.00807 -0.0489 0.8041 0.9739
2.000 0.4722 0.01568 0.00796 -0.0507 0.7896 0.9791
2.250 0.5079 0.01555 0.00788 -0.0523 0.7736 0.9843
2.500 0.5449 0.01539 0.00777 -0.0543 0.7568 0.9890
2.750 0.5800 0.01528 0.00772 -0.0558 0.7391 0.9940
3.000 0.6160 0.01513 0.00762 -0.0575 0.7187 0.9987
3.250 0.6397 0.01510 0.00759 -0.0566 0.6954 1.0000
3.500 0.6585 0.01512 0.00761 -0.0547 0.6710 1.0000
3.750 0.6774 0.01517 0.00766 -0.0528 0.6462 1.0000
4.000 0.6956 0.01525 0.00774 -0.0508 0.6202 1.0000
4.250 0.7131 0.01538 0.00785 -0.0487 0.5920 1.0000
4.500 0.7299 0.01555 0.00799 -0.0464 0.5612 1.0000
4.750 0.7454 0.01577 0.00818 -0.0439 0.5259 1.0000
5.000 0.7593 0.01606 0.00837 -0.0412 0.4826 1.0000
5.250 0.7708 0.01647 0.00859 -0.0380 0.4293 1.0000
5.500 0.7794 0.01705 0.00888 -0.0344 0.3670 1.0000
5.750 0.7864 0.01779 0.00928 -0.0307 0.3053 1.0000
6.000 0.7934 0.01857 0.00978 -0.0272 0.2509 1.0000
6.250 0.8007 0.01939 0.01037 -0.0237 0.2009 1.0000
6.500 0.8084 0.02021 0.01097 -0.0204 0.1596 1.0000
6.750 0.8159 0.02107 0.01163 -0.0170 0.1264 1.0000
7.000 0.8233 0.02195 0.01237 -0.0137 0.0988 1.0000
7.250 0.8313 0.02281 0.01315 -0.0104 0.0788 1.0000
7.500 0.8385 0.02372 0.01401 -0.0069 0.0653 1.0000
7.750 0.8453 0.02465 0.01494 -0.0034 0.0561 1.0000
8.000 0.8514 0.02562 0.01591 0.0001 0.0504 1.0000
8.250 0.8576 0.02660 0.01696 0.0036 0.0457 1.0000
8.500 0.8637 0.02749 0.01791 0.0071 0.0416 1.0000
8.750 0.8661 0.02859 0.01899 0.0109 0.0389 1.0000
9.000 0.8727 0.02972 0.02023 0.0142 0.0369 1.0000
9.250 0.8813 0.03093 0.02157 0.0171 0.0347 1.0000
9.500 0.8904 0.03212 0.02285 0.0197 0.0327 1.0000
9.750 0.8979 0.03337 0.02414 0.0222 0.0307 1.0000
10.000 0.9084 0.03502 0.02584 0.0242 0.0292 1.0000
10.250 0.9211 0.03661 0.02766 0.0261 0.0278 1.0000
10.500 0.9333 0.03847 0.02975 0.0279 0.0267 1.0000
10.750 0.9434 0.04041 0.03191 0.0298 0.0259 1.0000
11.000 0.9492 0.04234 0.03404 0.0321 0.0249 1.0000
11.250 0.9530 0.04429 0.03618 0.0343 0.0242 1.0000
11.500 0.9544 0.04600 0.03796 0.0364 0.0232 1.0000
11.750 0.9552 0.04847 0.04052 0.0382 0.0225 1.0000
12.000 0.9509 0.05115 0.04349 0.0403 0.0222 1.0000
12.250 0.9403 0.05394 0.04662 0.0424 0.0217 1.0000
12.500 0.9293 0.05719 0.05015 0.0438 0.0214 1.0000
12.750 0.9159 0.06086 0.05408 0.0447 0.0213 1.0000
13.000 0.9005 0.06492 0.05839 0.0448 0.0213 1.0000
13.250 0.8821 0.06963 0.06333 0.0441 0.0212 1.0000
13.500 0.8624 0.07493 0.06885 0.0424 0.0212 1.0000
13.750 0.8418 0.08090 0.07500 0.0398 0.0214 1.0000
14.000 0.8192 0.08783 0.08208 0.0361 0.0215 1.0000
14.250 0.7971 0.09552 0.08990 0.0316 0.0217 1.0000
14.500 0.7732 0.10457 0.09905 0.0260 0.0219 1.0000
14.750 0.7499 0.11453 0.10908 0.0202 0.0222 1.0000
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