HAWKER TEMPEST 37.5% SEMISPAN AIRFOIL (tempest1-il) Xfoil prediction polar at RE=500,000 Ncrit=9
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Airfoil: HAWKER TEMPEST 37.5% SEMISPAN AIRFOIL (tempest1-il) Reynolds number: 500,000 Max Cl/Cd: 71.53 at α=5.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-tempest1-il-500000.txt Download as CSV file: xf-tempest1-il-500000.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 = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-17.000 -0.7378 0.11356 0.11077 -0.0445 1.0000 0.0152
-16.750 -0.7865 0.09899 0.09599 -0.0528 1.0000 0.0147
-16.500 -0.8212 0.08810 0.08492 -0.0593 1.0000 0.0145
-16.250 -0.8487 0.07937 0.07601 -0.0645 1.0000 0.0145
-16.000 -0.8779 0.07105 0.06745 -0.0690 1.0000 0.0142
-15.750 -0.8952 0.06526 0.06150 -0.0718 1.0000 0.0143
-15.500 -0.9101 0.06022 0.05630 -0.0739 1.0000 0.0143
-15.250 -0.9227 0.05587 0.05179 -0.0753 1.0000 0.0144
-15.000 -0.9342 0.05197 0.04774 -0.0760 1.0000 0.0146
-14.750 -0.9442 0.04849 0.04410 -0.0761 1.0000 0.0146
-14.500 -0.9527 0.04540 0.04085 -0.0757 1.0000 0.0146
-14.250 -0.9591 0.04277 0.03806 -0.0748 1.0000 0.0149
-14.000 -0.9640 0.04037 0.03552 -0.0735 1.0000 0.0149
-13.750 -0.9683 0.03828 0.03329 -0.0717 1.0000 0.0152
-13.500 -0.9710 0.03639 0.03125 -0.0697 1.0000 0.0154
-13.250 -0.9726 0.03476 0.02949 -0.0673 1.0000 0.0156
-13.000 -0.9728 0.03337 0.02797 -0.0648 1.0000 0.0157
-12.750 -0.9726 0.03214 0.02662 -0.0620 1.0000 0.0158
-12.500 -0.9749 0.03043 0.02479 -0.0587 1.0000 0.0160
-12.250 -0.9776 0.02883 0.02311 -0.0551 1.0000 0.0163
-12.000 -0.9796 0.02768 0.02190 -0.0513 1.0000 0.0166
-11.750 -0.9820 0.02677 0.02096 -0.0471 1.0000 0.0170
-11.500 -0.9844 0.02606 0.02020 -0.0427 1.0000 0.0173
-11.250 -0.9883 0.02534 0.01941 -0.0378 1.0000 0.0174
-11.000 -0.9929 0.02490 0.01892 -0.0327 1.0000 0.0180
-10.750 -0.9999 0.02437 0.01833 -0.0270 1.0000 0.0181
-10.500 -0.9733 0.02361 0.01747 -0.0278 0.9978 0.0189
-10.250 -0.9464 0.02280 0.01656 -0.0287 0.9952 0.0196
-10.000 -0.9251 0.02157 0.01524 -0.0286 0.9922 0.0204
-9.750 -0.9034 0.02056 0.01419 -0.0285 0.9883 0.0214
-9.500 -0.8761 0.01982 0.01340 -0.0293 0.9855 0.0224
-9.250 -0.8455 0.01917 0.01269 -0.0306 0.9835 0.0239
-9.000 -0.8228 0.01845 0.01189 -0.0302 0.9792 0.0250
-8.750 -0.7983 0.01762 0.01106 -0.0303 0.9751 0.0275
-8.500 -0.7670 0.01702 0.01040 -0.0316 0.9726 0.0297
-8.250 -0.7364 0.01615 0.00953 -0.0329 0.9707 0.0342
-8.000 -0.7121 0.01554 0.00890 -0.0325 0.9661 0.0394
-7.750 -0.6862 0.01489 0.00829 -0.0326 0.9616 0.0483
-7.500 -0.6548 0.01425 0.00774 -0.0339 0.9591 0.0635
-7.250 -0.6207 0.01370 0.00727 -0.0357 0.9575 0.0807
-7.000 -0.5849 0.01323 0.00686 -0.0378 0.9562 0.0955
-6.750 -0.5579 0.01289 0.00653 -0.0379 0.9518 0.1072
-6.500 -0.5287 0.01255 0.00620 -0.0384 0.9477 0.1190
-6.250 -0.4953 0.01215 0.00584 -0.0399 0.9450 0.1327
-6.000 -0.4612 0.01172 0.00546 -0.0416 0.9428 0.1484
-5.750 -0.4270 0.01125 0.00507 -0.0433 0.9406 0.1682
-5.500 -0.4093 0.01094 0.00484 -0.0413 0.9327 0.1884
-5.250 -0.3813 0.01043 0.00448 -0.0417 0.9284 0.2248
-5.000 -0.3554 0.00987 0.00414 -0.0417 0.9240 0.2772
-4.750 -0.3401 0.00943 0.00391 -0.0392 0.9156 0.3290
-4.500 -0.3170 0.00888 0.00360 -0.0385 0.9105 0.3950
-4.250 -0.3031 0.00853 0.00344 -0.0357 0.9018 0.4483
-4.000 -0.2811 0.00819 0.00325 -0.0345 0.8959 0.5004
-3.750 -0.2635 0.00796 0.00314 -0.0323 0.8880 0.5399
-3.500 -0.2407 0.00775 0.00299 -0.0312 0.8814 0.5730
-3.250 -0.2196 0.00758 0.00290 -0.0297 0.8742 0.6029
-3.000 -0.1972 0.00743 0.00279 -0.0284 0.8669 0.6305
-2.750 -0.1739 0.00730 0.00271 -0.0273 0.8600 0.6548
-2.500 -0.1515 0.00719 0.00264 -0.0261 0.8522 0.6783
-2.250 -0.1271 0.00709 0.00258 -0.0252 0.8454 0.7020
-2.000 -0.1044 0.00702 0.00254 -0.0240 0.8372 0.7226
-1.750 -0.0788 0.00696 0.00250 -0.0234 0.8301 0.7420
-1.500 -0.0554 0.00692 0.00248 -0.0223 0.8216 0.7606
-1.250 -0.0297 0.00689 0.00246 -0.0217 0.8139 0.7777
-1.000 -0.0056 0.00688 0.00246 -0.0207 0.8053 0.7956
-0.750 0.0181 0.00689 0.00248 -0.0196 0.7968 0.8153
-0.500 0.0441 0.00691 0.00252 -0.0190 0.7882 0.8322
-0.250 0.0688 0.00695 0.00256 -0.0181 0.7789 0.8459
0.000 0.0990 0.00701 0.00260 -0.0184 0.7705 0.8568
0.250 0.1247 0.00706 0.00267 -0.0178 0.7600 0.8675
0.500 0.1484 0.00713 0.00270 -0.0167 0.7501 0.8785
0.750 0.1808 0.00723 0.00277 -0.0176 0.7399 0.8850
1.000 0.2030 0.00729 0.00282 -0.0162 0.7282 0.8943
1.250 0.2357 0.00741 0.00292 -0.0172 0.7169 0.8993
1.500 0.2603 0.00751 0.00298 -0.0164 0.7063 0.9072
1.750 0.2914 0.00763 0.00309 -0.0170 0.6952 0.9119
2.000 0.3245 0.00778 0.00322 -0.0181 0.6837 0.9159
2.250 0.3435 0.00787 0.00328 -0.0160 0.6732 0.9245
2.500 0.3801 0.00804 0.00341 -0.0179 0.6617 0.9265
2.750 0.4151 0.00822 0.00356 -0.0195 0.6481 0.9290
3.000 0.4480 0.00839 0.00371 -0.0206 0.6332 0.9320
3.250 0.4658 0.00851 0.00380 -0.0184 0.6197 0.9400
3.500 0.5036 0.00869 0.00396 -0.0206 0.6048 0.9413
3.750 0.5410 0.00889 0.00413 -0.0227 0.5902 0.9425
4.000 0.5762 0.00908 0.00430 -0.0244 0.5746 0.9442
4.250 0.6096 0.00929 0.00447 -0.0257 0.5582 0.9467
4.500 0.6352 0.00948 0.00464 -0.0253 0.5411 0.9517
4.750 0.6608 0.00967 0.00479 -0.0249 0.5230 0.9561
5.000 0.6953 0.00990 0.00498 -0.0266 0.4991 0.9578
5.250 0.7270 0.01018 0.00519 -0.0276 0.4709 0.9603
5.500 0.7532 0.01053 0.00542 -0.0276 0.4344 0.9645
5.750 0.7723 0.01095 0.00567 -0.0261 0.3926 0.9703
6.000 0.8014 0.01153 0.00600 -0.0269 0.3393 0.9728
6.250 0.8294 0.01207 0.00634 -0.0276 0.2959 0.9761
6.500 0.8509 0.01261 0.00671 -0.0268 0.2586 0.9815
6.750 0.8797 0.01312 0.00705 -0.0277 0.2206 0.9842
7.000 0.9092 0.01367 0.00742 -0.0288 0.1846 0.9868
7.250 0.9367 0.01419 0.00780 -0.0294 0.1559 0.9902
7.500 0.9618 0.01472 0.00822 -0.0296 0.1321 0.9938
7.750 0.9918 0.01518 0.00859 -0.0308 0.1113 0.9962
8.000 1.0198 0.01572 0.00902 -0.0317 0.0905 0.9989
8.250 1.0309 0.01615 0.00938 -0.0290 0.0755 1.0000
8.500 1.0251 0.01645 0.00965 -0.0227 0.0664 1.0000
8.750 1.0209 0.01679 0.00997 -0.0169 0.0582 1.0000
9.000 1.0179 0.01720 0.01036 -0.0113 0.0509 1.0000
9.250 1.0149 0.01772 0.01086 -0.0059 0.0447 1.0000
9.500 1.0166 0.01818 0.01134 -0.0015 0.0406 1.0000
9.750 1.0150 0.01886 0.01200 0.0034 0.0364 1.0000
10.000 1.0200 0.01937 0.01256 0.0071 0.0337 1.0000
10.250 1.0217 0.02012 0.01330 0.0111 0.0308 1.0000
10.500 1.0249 0.02089 0.01412 0.0148 0.0292 1.0000
10.750 1.0325 0.02153 0.01482 0.0176 0.0274 1.0000
11.000 1.0374 0.02238 0.01570 0.0207 0.0258 1.0000
11.250 1.0367 0.02362 0.01697 0.0242 0.0245 1.0000
11.500 1.0416 0.02463 0.01806 0.0269 0.0237 1.0000
11.750 1.0487 0.02559 0.01908 0.0292 0.0228 1.0000
12.000 1.0568 0.02654 0.02008 0.0312 0.0218 1.0000
12.250 1.0623 0.02772 0.02131 0.0333 0.0209 1.0000
12.500 1.0659 0.02909 0.02272 0.0354 0.0202 1.0000
12.750 1.0607 0.03119 0.02488 0.0380 0.0194 1.0000
13.000 1.0674 0.03251 0.02630 0.0395 0.0191 1.0000
13.250 1.0735 0.03394 0.02782 0.0409 0.0187 1.0000
13.500 1.0796 0.03541 0.02937 0.0422 0.0181 1.0000
13.750 1.0839 0.03709 0.03113 0.0434 0.0176 1.0000
14.000 1.0873 0.03891 0.03302 0.0445 0.0172 1.0000
14.250 1.0917 0.04070 0.03486 0.0453 0.0166 1.0000
14.500 1.0935 0.04279 0.03703 0.0462 0.0165 1.0000
14.750 1.0936 0.04509 0.03938 0.0470 0.0159 1.0000
15.000 1.0919 0.04765 0.04202 0.0479 0.0156 1.0000
15.250 1.0922 0.05011 0.04460 0.0484 0.0153 1.0000
15.500 1.0952 0.05241 0.04701 0.0484 0.0150 1.0000
15.750 1.0951 0.05506 0.04978 0.0487 0.0149 1.0000
16.000 1.0944 0.05791 0.05275 0.0487 0.0146 1.0000
16.250 1.0952 0.06066 0.05560 0.0482 0.0142 1.0000
16.500 1.0931 0.06381 0.05886 0.0478 0.0140 1.0000
16.750 1.0909 0.06707 0.06223 0.0471 0.0138 1.0000
17.000 1.0876 0.07056 0.06584 0.0464 0.0137 1.0000
17.250 1.0821 0.07439 0.06979 0.0455 0.0135 1.0000
17.500 1.0781 0.07820 0.07370 0.0442 0.0133 1.0000
17.750 1.0715 0.08244 0.07806 0.0428 0.0132 1.0000
18.000 1.0659 0.08667 0.08239 0.0412 0.0130 1.0000
18.250 1.0588 0.09118 0.08698 0.0394 0.0129 1.0000
18.500 1.0531 0.09553 0.09140 0.0375 0.0127 1.0000
18.750 1.0410 0.10109 0.09712 0.0352 0.0127 1.0000
19.000 1.0279 0.10704 0.10323 0.0324 0.0127 1.0000
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