HAWKER TEMPEST 61% SEMISPAN AIRFOIL (tempest2-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: HAWKER TEMPEST 61% SEMISPAN AIRFOIL (tempest2-il) Reynolds number: 1,000,000 Max Cl/Cd: 79.53 at α=4° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-tempest2-il-1000000.txt Download as CSV file: xf-tempest2-il-1000000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-15.000 -0.7864 0.09008 0.08804 -0.0387 1.0000 0.0071
-14.750 -0.8331 0.07552 0.07330 -0.0476 1.0000 0.0070
-14.500 -0.8894 0.06076 0.05827 -0.0574 1.0000 0.0067
-14.250 -0.8979 0.05568 0.05308 -0.0607 1.0000 0.0068
-14.000 -0.9214 0.04916 0.04635 -0.0642 1.0000 0.0068
-13.750 -0.9373 0.04453 0.04156 -0.0656 1.0000 0.0068
-13.500 -0.9462 0.04127 0.03816 -0.0658 1.0000 0.0068
-13.250 -0.9566 0.03827 0.03499 -0.0649 1.0000 0.0069
-13.000 -0.9676 0.03552 0.03208 -0.0631 1.0000 0.0069
-12.750 -0.9709 0.03374 0.03015 -0.0610 1.0000 0.0070
-12.500 -0.9823 0.03141 0.02767 -0.0576 1.0000 0.0069
-12.250 -0.9789 0.03058 0.02673 -0.0549 1.0000 0.0071
-12.000 -0.9730 0.03017 0.02625 -0.0521 1.0000 0.0072
-11.750 -0.9940 0.02775 0.02360 -0.0456 1.0000 0.0072
-11.500 -1.0212 0.02563 0.02127 -0.0370 1.0000 0.0074
-11.250 -1.0334 0.02463 0.02018 -0.0304 1.0000 0.0077
-11.000 -1.0330 0.02393 0.01941 -0.0259 1.0000 0.0077
-10.750 -1.0284 0.02324 0.01864 -0.0222 0.9998 0.0079
-10.500 -1.0015 0.02233 0.01766 -0.0230 0.9984 0.0082
-10.250 -0.9756 0.02121 0.01642 -0.0237 0.9966 0.0084
-10.000 -0.9476 0.02034 0.01545 -0.0246 0.9950 0.0087
-9.750 -0.9210 0.01936 0.01436 -0.0252 0.9933 0.0090
-9.500 -0.8959 0.01849 0.01340 -0.0253 0.9908 0.0092
-9.250 -0.8690 0.01765 0.01245 -0.0258 0.9885 0.0096
-9.000 -0.8388 0.01711 0.01184 -0.0268 0.9867 0.0099
-8.750 -0.8090 0.01638 0.01103 -0.0278 0.9852 0.0100
-8.500 -0.7840 0.01481 0.00932 -0.0282 0.9836 0.0107
-8.250 -0.7565 0.01421 0.00869 -0.0285 0.9811 0.0114
-8.000 -0.7295 0.01379 0.00824 -0.0287 0.9776 0.0120
-7.750 -0.6991 0.01330 0.00770 -0.0296 0.9753 0.0128
-7.500 -0.6669 0.01285 0.00721 -0.0308 0.9736 0.0134
-7.250 -0.6363 0.01204 0.00632 -0.0319 0.9720 0.0146
-7.000 -0.6027 0.01150 0.00576 -0.0335 0.9708 0.0159
-6.750 -0.5682 0.01109 0.00531 -0.0352 0.9696 0.0173
-6.500 -0.5449 0.01071 0.00489 -0.0343 0.9639 0.0193
-6.250 -0.5151 0.01027 0.00446 -0.0350 0.9604 0.0232
-6.000 -0.4841 0.00983 0.00404 -0.0359 0.9575 0.0297
-5.750 -0.4558 0.00940 0.00367 -0.0363 0.9533 0.0449
-5.500 -0.4324 0.00901 0.00339 -0.0355 0.9465 0.0672
-5.250 -0.4031 0.00868 0.00313 -0.0361 0.9421 0.0880
-5.000 -0.3791 0.00844 0.00294 -0.0354 0.9350 0.1052
-4.750 -0.3525 0.00819 0.00273 -0.0352 0.9288 0.1223
-4.500 -0.3274 0.00796 0.00256 -0.0348 0.9220 0.1407
-4.250 -0.3031 0.00768 0.00237 -0.0341 0.9144 0.1697
-4.000 -0.2800 0.00739 0.00219 -0.0333 0.9067 0.2061
-3.750 -0.2573 0.00703 0.00201 -0.0324 0.8988 0.2590
-3.500 -0.2380 0.00658 0.00183 -0.0308 0.8900 0.3360
-3.250 -0.2181 0.00613 0.00166 -0.0293 0.8820 0.4211
-3.000 -0.1976 0.00583 0.00155 -0.0278 0.8729 0.4825
-2.750 -0.1758 0.00559 0.00146 -0.0266 0.8649 0.5349
-2.500 -0.1531 0.00542 0.00138 -0.0255 0.8562 0.5744
-2.250 -0.1300 0.00528 0.00131 -0.0245 0.8476 0.6072
-2.000 -0.1068 0.00516 0.00124 -0.0234 0.8391 0.6412
-1.750 -0.0841 0.00503 0.00120 -0.0223 0.8296 0.6732
-1.500 -0.0606 0.00495 0.00116 -0.0213 0.8209 0.7009
-1.250 -0.0374 0.00486 0.00113 -0.0202 0.8113 0.7304
-1.000 -0.0135 0.00480 0.00112 -0.0193 0.8015 0.7534
-0.750 0.0107 0.00477 0.00110 -0.0184 0.7916 0.7765
-0.500 0.0349 0.00474 0.00110 -0.0175 0.7810 0.7971
-0.250 0.0594 0.00472 0.00111 -0.0167 0.7695 0.8163
0.000 0.0833 0.00471 0.00113 -0.0157 0.7572 0.8395
0.250 0.1081 0.00472 0.00116 -0.0149 0.7446 0.8587
0.500 0.1334 0.00476 0.00119 -0.0143 0.7319 0.8724
0.750 0.1588 0.00481 0.00122 -0.0137 0.7190 0.8850
1.000 0.1835 0.00487 0.00126 -0.0129 0.7062 0.8968
1.250 0.2111 0.00494 0.00132 -0.0128 0.6929 0.9053
1.500 0.2369 0.00501 0.00137 -0.0123 0.6792 0.9137
1.750 0.2634 0.00510 0.00143 -0.0119 0.6637 0.9210
2.000 0.2889 0.00521 0.00149 -0.0114 0.6453 0.9280
2.250 0.3166 0.00534 0.00158 -0.0113 0.6262 0.9339
2.500 0.3401 0.00545 0.00165 -0.0104 0.6098 0.9410
2.750 0.3712 0.00560 0.00175 -0.0111 0.5924 0.9445
3.000 0.4001 0.00575 0.00187 -0.0114 0.5754 0.9490
3.250 0.4232 0.00589 0.00196 -0.0104 0.5581 0.9553
3.500 0.4562 0.00607 0.00209 -0.0116 0.5362 0.9574
3.750 0.4887 0.00628 0.00224 -0.0128 0.5108 0.9596
4.000 0.5201 0.00654 0.00240 -0.0137 0.4772 0.9620
4.250 0.5471 0.00694 0.00258 -0.0138 0.4224 0.9655
4.500 0.5695 0.00737 0.00280 -0.0129 0.3680 0.9700
4.750 0.6008 0.00792 0.00307 -0.0142 0.3045 0.9712
5.000 0.6314 0.00847 0.00337 -0.0153 0.2461 0.9727
5.250 0.6614 0.00900 0.00367 -0.0162 0.1953 0.9745
5.500 0.6904 0.00950 0.00398 -0.0169 0.1525 0.9770
5.750 0.7158 0.00997 0.00430 -0.0168 0.1193 0.9810
6.000 0.7442 0.01040 0.00460 -0.0173 0.0928 0.9835
6.250 0.7762 0.01092 0.00497 -0.0187 0.0631 0.9848
6.500 0.8069 0.01146 0.00537 -0.0199 0.0399 0.9865
6.750 0.8372 0.01192 0.00577 -0.0209 0.0285 0.9885
7.000 0.8660 0.01242 0.00624 -0.0215 0.0219 0.9908
7.250 0.8942 0.01280 0.00663 -0.0220 0.0191 0.9931
7.500 0.9224 0.01338 0.00724 -0.0225 0.0165 0.9948
7.750 0.9538 0.01372 0.00762 -0.0237 0.0153 0.9962
8.000 0.9839 0.01415 0.00808 -0.0247 0.0141 0.9978
8.250 1.0107 0.01497 0.00896 -0.0251 0.0125 0.9996
8.500 1.0280 0.01539 0.00943 -0.0234 0.0121 1.0000
8.750 1.0405 0.01564 0.00971 -0.0206 0.0116 1.0000
9.000 1.0493 0.01605 0.01017 -0.0171 0.0111 1.0000
9.250 1.0582 0.01643 0.01058 -0.0137 0.0106 1.0000
9.500 1.0672 0.01678 0.01095 -0.0103 0.0101 1.0000
9.750 1.0689 0.01721 0.01143 -0.0054 0.0099 1.0000
10.000 1.0690 0.01768 0.01195 -0.0002 0.0097 1.0000
10.250 1.0678 0.01841 0.01274 0.0049 0.0094 1.0000
10.500 1.0618 0.01964 0.01410 0.0105 0.0090 1.0000
10.750 1.0705 0.02026 0.01478 0.0134 0.0089 1.0000
11.000 1.0827 0.02075 0.01533 0.0158 0.0086 1.0000
11.250 1.0913 0.02153 0.01618 0.0184 0.0085 1.0000
11.500 1.1002 0.02234 0.01707 0.0209 0.0082 1.0000
11.750 1.1110 0.02307 0.01786 0.0230 0.0079 1.0000
12.000 1.1205 0.02393 0.01879 0.0251 0.0077 1.0000
12.250 1.1313 0.02472 0.01963 0.0269 0.0074 1.0000
12.500 1.1395 0.02575 0.02073 0.0288 0.0072 1.0000
12.750 1.1449 0.02704 0.02210 0.0309 0.0070 1.0000
13.000 1.1509 0.02834 0.02348 0.0327 0.0070 1.0000
13.250 1.1529 0.03001 0.02524 0.0346 0.0067 1.0000
13.500 1.1488 0.03234 0.02771 0.0367 0.0066 1.0000
13.750 1.1432 0.03497 0.03048 0.0385 0.0065 1.0000
14.000 1.1380 0.03768 0.03336 0.0399 0.0063 1.0000
14.250 1.1415 0.03960 0.03540 0.0406 0.0062 1.0000
14.500 1.1354 0.04264 0.03859 0.0413 0.0063 1.0000
14.750 1.1369 0.04495 0.04100 0.0414 0.0062 1.0000
15.000 1.1292 0.04848 0.04469 0.0414 0.0061 1.0000
15.250 1.1294 0.05123 0.04754 0.0410 0.0061 1.0000
15.500 1.1201 0.05531 0.05177 0.0401 0.0060 1.0000
15.750 1.1121 0.05951 0.05611 0.0389 0.0059 1.0000
16.000 1.1017 0.06423 0.06097 0.0371 0.0059 1.0000
16.250 1.0807 0.07079 0.06772 0.0345 0.0059 1.0000
16.500 1.0779 0.07492 0.07193 0.0324 0.0059 1.0000
16.750 1.0595 0.08179 0.07895 0.0290 0.0058 1.0000
17.000 1.0353 0.09001 0.08734 0.0249 0.0059 1.0000
17.250 1.0112 0.09867 0.09615 0.0203 0.0060 1.0000
17.500 0.9863 0.10795 0.10559 0.0153 0.0059 1.0000
17.750 0.9597 0.11787 0.11564 0.0101 0.0060 1.0000
18.000 0.9328 0.12823 0.12614 0.0046 0.0061 1.0000
18.250 0.8897 0.14299 0.14105 -0.0029 0.0062 1.0000
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