HAWKER TEMPEST 37.5% SEMISPAN AIRFOIL (tempest1-il) Xfoil prediction polar at RE=100,000 Ncrit=9
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Airfoil: HAWKER TEMPEST 37.5% SEMISPAN AIRFOIL (tempest1-il) Reynolds number: 100,000 Max Cl/Cd: 49.75 at α=6.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-tempest1-il-100000.txt Download as CSV file: xf-tempest1-il-100000.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 = 0.100 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.750 -0.5436 0.10755 0.10224 -0.0506 1.0000 0.0781
-12.500 -0.6536 0.08160 0.07618 -0.0676 1.0000 0.0651
-12.250 -0.6728 0.07624 0.07079 -0.0687 1.0000 0.0645
-12.000 -0.6984 0.07125 0.06573 -0.0690 1.0000 0.0639
-11.750 -0.7254 0.06705 0.06142 -0.0679 1.0000 0.0635
-11.500 -0.7524 0.06345 0.05771 -0.0654 1.0000 0.0630
-11.250 -0.7773 0.06055 0.05469 -0.0616 1.0000 0.0624
-11.000 -0.8059 0.05809 0.05210 -0.0561 1.0000 0.0623
-10.750 -0.8316 0.05607 0.04995 -0.0497 1.0000 0.0618
-10.500 -0.8548 0.05374 0.04745 -0.0435 1.0000 0.0615
-10.250 -0.8748 0.05129 0.04478 -0.0374 1.0000 0.0615
-10.000 -0.8908 0.04884 0.04207 -0.0316 1.0000 0.0614
-9.750 -0.9031 0.04643 0.03937 -0.0261 1.0000 0.0617
-9.500 -0.9110 0.04411 0.03672 -0.0210 1.0000 0.0621
-9.250 -0.9163 0.04196 0.03422 -0.0160 1.0000 0.0632
-9.000 -0.9192 0.04015 0.03200 -0.0112 1.0000 0.0646
-8.750 -0.9149 0.03782 0.02946 -0.0078 1.0000 0.0667
-8.500 -0.9048 0.03635 0.02795 -0.0053 1.0000 0.0691
-8.250 -0.8949 0.03487 0.02629 -0.0025 1.0000 0.0722
-8.000 -0.8850 0.03338 0.02446 0.0007 1.0000 0.0757
-7.750 -0.8715 0.03183 0.02290 0.0028 1.0000 0.0807
-7.500 -0.8593 0.03083 0.02178 0.0053 1.0000 0.0863
-7.250 -0.8444 0.02941 0.02028 0.0074 1.0000 0.0932
-7.000 -0.8339 0.02869 0.01937 0.0104 1.0000 0.1028
-6.750 -0.8200 0.02756 0.01838 0.0124 1.0000 0.1136
-6.500 -0.8078 0.02661 0.01743 0.0149 1.0000 0.1273
-6.250 -0.7960 0.02576 0.01658 0.0174 1.0000 0.1434
-6.000 -0.7840 0.02500 0.01580 0.0199 1.0000 0.1607
-5.750 -0.7716 0.02423 0.01514 0.0222 1.0000 0.1784
-5.500 -0.7591 0.02356 0.01457 0.0245 1.0000 0.1964
-5.250 -0.7466 0.02295 0.01404 0.0268 1.0000 0.2167
-5.000 -0.7339 0.02234 0.01353 0.0290 1.0000 0.2391
-4.750 -0.7219 0.02171 0.01308 0.0314 1.0000 0.2650
-4.500 -0.7110 0.02104 0.01265 0.0340 1.0000 0.2997
-4.250 -0.6863 0.02024 0.01251 0.0338 0.9944 0.3795
-4.000 -0.6667 0.01949 0.01268 0.0353 0.9869 0.5295
-3.750 -0.6389 0.01952 0.01321 0.0358 0.9799 0.6462
-3.500 -0.6054 0.01990 0.01376 0.0355 0.9726 0.7204
-3.250 -0.5669 0.02051 0.01441 0.0342 0.9660 0.7723
-3.000 -0.5250 0.02125 0.01508 0.0323 0.9591 0.8123
-2.750 -0.4712 0.02233 0.01602 0.0282 0.9545 0.8429
-2.500 -0.4248 0.02319 0.01674 0.0252 0.9475 0.8650
-2.250 -0.3579 0.02440 0.01776 0.0185 0.9434 0.8815
-2.000 -0.2792 0.02571 0.01887 0.0095 0.9410 0.8955
-1.750 -0.2069 0.02685 0.01987 0.0017 0.9369 0.9101
-1.500 -0.1384 0.02758 0.02047 -0.0059 0.9321 0.9232
-1.250 -0.0630 0.02794 0.02071 -0.0153 0.9285 0.9317
-1.000 0.0018 0.02808 0.02075 -0.0230 0.9253 0.9420
-0.750 0.0488 0.02809 0.02072 -0.0275 0.9165 0.9532
-0.500 0.1157 0.02786 0.02043 -0.0358 0.9123 0.9601
-0.250 0.1673 0.02769 0.02024 -0.0413 0.9056 0.9699
0.000 0.2287 0.02725 0.01978 -0.0487 0.8992 0.9770
0.250 0.2946 0.02671 0.01924 -0.0568 0.8957 0.9838
0.500 0.3480 0.02620 0.01876 -0.0627 0.8873 0.9918
0.750 0.4166 0.02534 0.01794 -0.0713 0.8830 0.9976
1.000 0.4830 0.02437 0.01702 -0.0792 0.8797 1.0000
1.250 0.5079 0.02405 0.01673 -0.0793 0.8674 1.0000
1.500 0.5398 0.02358 0.01630 -0.0805 0.8570 1.0000
1.750 0.5862 0.02271 0.01548 -0.0840 0.8495 1.0000
2.000 0.6092 0.02241 0.01522 -0.0833 0.8365 1.0000
2.250 0.6343 0.02206 0.01492 -0.0828 0.8243 1.0000
2.500 0.6652 0.02155 0.01445 -0.0833 0.8134 1.0000
2.750 0.6968 0.02102 0.01397 -0.0837 0.8024 1.0000
3.000 0.7165 0.02080 0.01380 -0.0821 0.7883 1.0000
3.250 0.7375 0.02054 0.01358 -0.0805 0.7739 1.0000
3.500 0.7597 0.02021 0.01329 -0.0790 0.7587 1.0000
3.750 0.7822 0.01985 0.01296 -0.0775 0.7426 1.0000
4.000 0.8042 0.01954 0.01266 -0.0759 0.7262 1.0000
4.250 0.8263 0.01925 0.01239 -0.0743 0.7092 1.0000
4.500 0.8429 0.01914 0.01233 -0.0718 0.6905 1.0000
4.750 0.8594 0.01904 0.01227 -0.0693 0.6710 1.0000
5.000 0.8779 0.01890 0.01215 -0.0671 0.6508 1.0000
5.250 0.8963 0.01879 0.01204 -0.0649 0.6293 1.0000
5.500 0.9101 0.01879 0.01205 -0.0618 0.6050 1.0000
5.750 0.9239 0.01881 0.01206 -0.0588 0.5790 1.0000
6.000 0.9365 0.01887 0.01208 -0.0555 0.5508 1.0000
6.250 0.9458 0.01901 0.01218 -0.0517 0.5195 1.0000
6.500 0.9520 0.01923 0.01235 -0.0473 0.4844 1.0000
6.750 0.9563 0.01955 0.01251 -0.0427 0.4468 1.0000
7.000 0.9574 0.01999 0.01280 -0.0376 0.4071 1.0000
7.250 0.9568 0.02060 0.01314 -0.0323 0.3688 1.0000
7.500 0.9547 0.02128 0.01364 -0.0269 0.3322 1.0000
7.750 0.9518 0.02204 0.01419 -0.0214 0.2994 1.0000
8.000 0.9484 0.02284 0.01481 -0.0160 0.2703 1.0000
8.250 0.9444 0.02367 0.01544 -0.0105 0.2449 1.0000
8.500 0.9389 0.02440 0.01607 -0.0047 0.2223 1.0000
8.750 0.9335 0.02524 0.01672 0.0009 0.2025 1.0000
9.000 0.9302 0.02613 0.01753 0.0060 0.1816 1.0000
9.250 0.9280 0.02715 0.01842 0.0106 0.1624 1.0000
9.500 0.9281 0.02837 0.01945 0.0147 0.1447 1.0000
9.750 0.9301 0.02967 0.02064 0.0184 0.1276 1.0000
10.000 0.9351 0.03102 0.02192 0.0215 0.1133 1.0000
10.250 0.9444 0.03245 0.02324 0.0239 0.1014 1.0000
10.500 0.9534 0.03372 0.02459 0.0264 0.0924 1.0000
10.750 0.9693 0.03539 0.02630 0.0279 0.0842 1.0000
11.000 0.9920 0.03727 0.02799 0.0281 0.0765 1.0000
11.250 1.0040 0.03892 0.02995 0.0303 0.0724 1.0000
11.500 1.0163 0.04051 0.03166 0.0321 0.0685 1.0000
11.750 1.0408 0.04313 0.03427 0.0319 0.0643 1.0000
12.000 1.0409 0.04500 0.03646 0.0352 0.0624 1.0000
12.250 1.0433 0.04729 0.03904 0.0380 0.0608 1.0000
12.500 1.0435 0.04973 0.04175 0.0407 0.0596 1.0000
12.750 1.0414 0.05223 0.04447 0.0433 0.0586 1.0000
13.000 1.0396 0.05464 0.04705 0.0456 0.0575 1.0000
13.250 1.0339 0.05731 0.04989 0.0480 0.0566 1.0000
13.500 1.0362 0.06031 0.05293 0.0492 0.0551 1.0000
13.750 1.0226 0.06432 0.05713 0.0511 0.0544 1.0000
14.000 1.0047 0.06810 0.06114 0.0530 0.0545 1.0000
14.250 0.9806 0.07182 0.06511 0.0545 0.0544 1.0000
14.750 0.9334 0.08084 0.07453 0.0548 0.0545 1.0000
15.000 0.8018 0.09936 0.09381 0.0446 0.0619 1.0000
15.250 0.7626 0.11050 0.10501 0.0386 0.0636 1.0000
15.500 0.7407 0.11957 0.11409 0.0344 0.0647 1.0000
15.750 0.6755 0.14528 0.13973 0.0218 0.0765 1.0000
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