HAWKER TEMPEST 37.5% SEMISPAN AIRFOIL (tempest1-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: HAWKER TEMPEST 37.5% SEMISPAN AIRFOIL (tempest1-il) Reynolds number: 200,000 Max Cl/Cd: 66.97 at α=5.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-tempest1-il-200000.txt Download as CSV file: xf-tempest1-il-200000.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 = 0.200 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.500 -0.8132 0.06078 0.05595 -0.0756 1.0000 0.0308
-13.250 -0.8373 0.05700 0.05195 -0.0746 1.0000 0.0307
-13.000 -0.8567 0.05378 0.04854 -0.0727 1.0000 0.0308
-12.750 -0.8746 0.05095 0.04554 -0.0700 1.0000 0.0308
-12.500 -0.8906 0.04839 0.04279 -0.0666 1.0000 0.0309
-12.250 -0.9039 0.04611 0.04036 -0.0628 1.0000 0.0311
-12.000 -0.9177 0.04399 0.03806 -0.0583 1.0000 0.0312
-11.750 -0.9267 0.04225 0.03621 -0.0539 1.0000 0.0315
-11.500 -0.9376 0.04072 0.03454 -0.0487 1.0000 0.0318
-11.250 -0.9502 0.03926 0.03289 -0.0427 1.0000 0.0317
-11.000 -0.9581 0.03819 0.03174 -0.0374 1.0000 0.0323
-10.750 -0.9621 0.03678 0.03018 -0.0327 1.0000 0.0326
-10.500 -0.9636 0.03540 0.02864 -0.0283 1.0000 0.0329
-10.250 -0.9626 0.03414 0.02724 -0.0242 1.0000 0.0336
-10.000 -0.9603 0.03296 0.02591 -0.0203 1.0000 0.0343
-9.750 -0.9562 0.03178 0.02456 -0.0165 1.0000 0.0352
-9.500 -0.9510 0.03075 0.02333 -0.0129 1.0000 0.0361
-9.250 -0.9474 0.03011 0.02249 -0.0089 1.0000 0.0372
-9.000 -0.9343 0.02815 0.02052 -0.0070 1.0000 0.0387
-8.750 -0.9259 0.02726 0.01962 -0.0040 1.0000 0.0403
-8.500 -0.9168 0.02642 0.01872 -0.0010 1.0000 0.0416
-8.250 -0.9076 0.02563 0.01782 0.0021 1.0000 0.0437
-8.000 -0.8926 0.02456 0.01666 0.0039 0.9991 0.0463
-7.750 -0.8611 0.02367 0.01580 0.0023 0.9952 0.0514
-7.500 -0.8322 0.02267 0.01477 0.0014 0.9909 0.0572
-7.250 -0.8019 0.02193 0.01400 0.0003 0.9862 0.0664
-7.000 -0.7697 0.02117 0.01334 -0.0014 0.9825 0.0814
-6.750 -0.7453 0.02056 0.01276 -0.0013 0.9762 0.0981
-6.500 -0.7120 0.02010 0.01230 -0.0029 0.9718 0.1183
-6.250 -0.6828 0.01961 0.01188 -0.0038 0.9670 0.1362
-6.000 -0.6561 0.01914 0.01144 -0.0041 0.9608 0.1527
-5.750 -0.6215 0.01870 0.01103 -0.0060 0.9570 0.1734
-5.500 -0.5967 0.01823 0.01064 -0.0059 0.9509 0.1935
-5.250 -0.5703 0.01769 0.01022 -0.0061 0.9450 0.2212
-5.000 -0.5388 0.01697 0.00977 -0.0074 0.9414 0.2681
-4.750 -0.5262 0.01629 0.00943 -0.0048 0.9328 0.3274
-4.500 -0.5045 0.01542 0.00908 -0.0039 0.9276 0.4298
-4.250 -0.4886 0.01493 0.00892 -0.0016 0.9205 0.5123
-4.000 -0.4657 0.01455 0.00878 -0.0004 0.9142 0.5776
-3.750 -0.4314 0.01422 0.00861 -0.0015 0.9112 0.6317
-3.500 -0.4130 0.01410 0.00860 0.0007 0.9030 0.6696
-3.250 -0.3798 0.01392 0.00848 -0.0001 0.8987 0.7065
-3.000 -0.3401 0.01377 0.00838 -0.0021 0.8963 0.7386
-2.750 -0.2959 0.01365 0.00827 -0.0050 0.8948 0.7661
-2.500 -0.2769 0.01373 0.00837 -0.0028 0.8853 0.7877
-2.250 -0.2319 0.01369 0.00832 -0.0059 0.8829 0.8078
-2.000 -0.1839 0.01367 0.00827 -0.0095 0.8812 0.8253
-1.750 -0.1339 0.01371 0.00827 -0.0135 0.8797 0.8405
-1.500 -0.1037 0.01400 0.00856 -0.0133 0.8718 0.8559
-1.250 -0.0512 0.01425 0.00878 -0.0176 0.8691 0.8677
-1.000 -0.0059 0.01429 0.00877 -0.0206 0.8660 0.8785
-0.750 0.0585 0.01444 0.00887 -0.0276 0.8645 0.8811
-0.500 0.1075 0.01466 0.00906 -0.0316 0.8581 0.8853
-0.250 0.1432 0.01461 0.00897 -0.0329 0.8516 0.8942
0.000 0.2032 0.01457 0.00889 -0.0392 0.8483 0.8955
0.250 0.2460 0.01471 0.00903 -0.0420 0.8390 0.8990
0.500 0.2943 0.01463 0.00889 -0.0460 0.8331 0.9029
0.750 0.3218 0.01466 0.00892 -0.0458 0.8220 0.9110
1.000 0.3681 0.01464 0.00888 -0.0494 0.8132 0.9142
1.250 0.4061 0.01458 0.00879 -0.0513 0.8032 0.9198
1.500 0.4364 0.01456 0.00876 -0.0517 0.7909 0.9266
1.750 0.4775 0.01452 0.00871 -0.0543 0.7794 0.9305
2.000 0.5084 0.01450 0.00866 -0.0549 0.7687 0.9378
2.250 0.5456 0.01443 0.00859 -0.0568 0.7565 0.9424
2.500 0.5831 0.01438 0.00856 -0.0589 0.7434 0.9471
2.750 0.6083 0.01441 0.00858 -0.0583 0.7301 0.9552
3.000 0.6489 0.01425 0.00843 -0.0610 0.7143 0.9588
3.250 0.6828 0.01417 0.00832 -0.0623 0.6977 0.9643
3.500 0.7125 0.01413 0.00827 -0.0627 0.6813 0.9706
3.750 0.7499 0.01400 0.00814 -0.0648 0.6641 0.9750
4.000 0.7808 0.01399 0.00811 -0.0656 0.6466 0.9812
4.250 0.8155 0.01386 0.00800 -0.0672 0.6263 0.9859
4.500 0.8487 0.01378 0.00792 -0.0685 0.6042 0.9912
4.750 0.8823 0.01370 0.00783 -0.0700 0.5805 0.9962
5.000 0.9123 0.01367 0.00775 -0.0708 0.5537 1.0000
5.250 0.9248 0.01381 0.00787 -0.0679 0.5277 1.0000
5.500 0.9360 0.01400 0.00800 -0.0649 0.4983 1.0000
5.750 0.9452 0.01426 0.00815 -0.0614 0.4636 1.0000
6.000 0.9525 0.01460 0.00834 -0.0576 0.4253 1.0000
6.250 0.9571 0.01504 0.00860 -0.0534 0.3849 1.0000
6.500 0.9609 0.01554 0.00892 -0.0491 0.3455 1.0000
6.750 0.9629 0.01610 0.00929 -0.0445 0.3094 1.0000
7.000 0.9646 0.01666 0.00969 -0.0398 0.2776 1.0000
7.250 0.9657 0.01720 0.01011 -0.0351 0.2486 1.0000
7.500 0.9661 0.01774 0.01053 -0.0303 0.2226 1.0000
7.750 0.9646 0.01828 0.01096 -0.0250 0.2008 1.0000
8.000 0.9607 0.01874 0.01136 -0.0193 0.1818 1.0000
8.250 0.9552 0.01920 0.01175 -0.0133 0.1650 1.0000
8.500 0.9511 0.01973 0.01221 -0.0077 0.1494 1.0000
8.750 0.9483 0.02034 0.01275 -0.0025 0.1340 1.0000
9.000 0.9461 0.02105 0.01338 0.0024 0.1186 1.0000
9.250 0.9447 0.02185 0.01410 0.0070 0.1040 1.0000
9.500 0.9436 0.02276 0.01494 0.0114 0.0908 1.0000
9.750 0.9437 0.02373 0.01586 0.0154 0.0787 1.0000
10.000 0.9454 0.02474 0.01688 0.0191 0.0698 1.0000
10.250 0.9447 0.02600 0.01808 0.0228 0.0636 1.0000
10.500 0.9498 0.02701 0.01915 0.0257 0.0583 1.0000
10.750 0.9500 0.02847 0.02054 0.0288 0.0540 1.0000
11.000 0.9573 0.02952 0.02169 0.0312 0.0499 1.0000
11.250 0.9623 0.03078 0.02296 0.0335 0.0469 1.0000
11.500 0.9681 0.03240 0.02454 0.0358 0.0446 1.0000
11.750 0.9776 0.03361 0.02590 0.0377 0.0425 1.0000
12.000 0.9866 0.03488 0.02724 0.0395 0.0404 1.0000
12.250 0.9958 0.03624 0.02860 0.0411 0.0386 1.0000
12.500 1.0099 0.03803 0.03036 0.0423 0.0366 1.0000
12.750 1.0182 0.03947 0.03198 0.0439 0.0355 1.0000
13.000 1.0276 0.04106 0.03373 0.0454 0.0344 1.0000
13.250 1.0369 0.04278 0.03559 0.0468 0.0334 1.0000
13.500 1.0435 0.04454 0.03749 0.0482 0.0325 1.0000
13.750 1.0496 0.04638 0.03941 0.0494 0.0316 1.0000
14.000 1.0593 0.04841 0.04146 0.0504 0.0306 1.0000
14.250 1.0575 0.05137 0.04461 0.0517 0.0296 1.0000
14.500 1.0544 0.05413 0.04760 0.0530 0.0294 1.0000
14.750 1.0440 0.05706 0.05078 0.0541 0.0290 1.0000
15.000 1.0344 0.06042 0.05437 0.0549 0.0288 1.0000
15.250 1.0218 0.06423 0.05842 0.0552 0.0287 1.0000
15.500 1.0073 0.06841 0.06283 0.0551 0.0286 1.0000
15.750 0.9910 0.07301 0.06764 0.0545 0.0287 1.0000
16.000 0.9694 0.07845 0.07332 0.0530 0.0285 1.0000
16.250 0.9487 0.08431 0.07939 0.0510 0.0286 1.0000
16.500 0.9246 0.09109 0.08636 0.0481 0.0288 1.0000
16.750 0.9000 0.09846 0.09392 0.0444 0.0290 1.0000
17.000 0.8747 0.10658 0.10219 0.0402 0.0293 1.0000
17.250 0.8457 0.11604 0.11180 0.0349 0.0296 1.0000
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