HAWKER TEMPEST 37.5% SEMISPAN AIRFOIL (tempest1-il) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
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Airfoil: HAWKER TEMPEST 37.5% SEMISPAN AIRFOIL (tempest1-il) Reynolds number: 100,000 Max Cl/Cd: 47.7 at α=5.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-tempest1-il-100000-n5.txt Download as CSV file: xf-tempest1-il-100000-n5.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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-14.500 -0.6329 0.10089 0.09527 -0.0533 1.0000 0.0297
-14.250 -0.6788 0.08738 0.08163 -0.0614 1.0000 0.0291
-14.000 -0.7116 0.07833 0.07242 -0.0667 1.0000 0.0286
-13.750 -0.7432 0.07079 0.06466 -0.0706 1.0000 0.0286
-13.500 -0.7679 0.06509 0.05876 -0.0725 1.0000 0.0285
-13.250 -0.7893 0.06047 0.05392 -0.0731 1.0000 0.0286
-13.000 -0.8068 0.05665 0.04989 -0.0727 1.0000 0.0287
-12.750 -0.8218 0.05335 0.04636 -0.0714 1.0000 0.0289
-12.500 -0.8346 0.05043 0.04322 -0.0694 1.0000 0.0291
-12.250 -0.8451 0.04788 0.04042 -0.0669 1.0000 0.0294
-12.000 -0.8537 0.04552 0.03781 -0.0640 1.0000 0.0299
-11.750 -0.8595 0.04346 0.03551 -0.0609 1.0000 0.0303
-11.500 -0.8603 0.04171 0.03370 -0.0580 1.0000 0.0309
-11.250 -0.8612 0.04027 0.03220 -0.0548 1.0000 0.0315
-11.000 -0.8636 0.03911 0.03100 -0.0511 1.0000 0.0324
-10.750 -0.8654 0.03797 0.02975 -0.0473 1.0000 0.0333
-10.500 -0.8672 0.03685 0.02851 -0.0432 1.0000 0.0343
-10.250 -0.8695 0.03583 0.02732 -0.0387 1.0000 0.0357
-10.000 -0.8695 0.03478 0.02607 -0.0345 1.0000 0.0369
-9.750 -0.8713 0.03374 0.02502 -0.0300 1.0000 0.0381
-9.500 -0.8709 0.03284 0.02409 -0.0259 1.0000 0.0392
-9.250 -0.8692 0.03195 0.02314 -0.0219 1.0000 0.0407
-9.000 -0.8659 0.03108 0.02217 -0.0181 1.0000 0.0426
-8.750 -0.8607 0.03027 0.02119 -0.0144 1.0000 0.0453
-8.500 -0.8585 0.02941 0.02036 -0.0105 1.0000 0.0473
-8.250 -0.8538 0.02870 0.01960 -0.0069 1.0000 0.0506
-8.000 -0.8288 0.02764 0.01845 -0.0073 0.9959 0.0562
-7.750 -0.8025 0.02679 0.01752 -0.0079 0.9912 0.0646
-7.500 -0.7770 0.02593 0.01668 -0.0084 0.9862 0.0740
-7.250 -0.7488 0.02521 0.01593 -0.0093 0.9818 0.0870
-7.000 -0.7243 0.02456 0.01523 -0.0093 0.9759 0.1011
-6.750 -0.6951 0.02397 0.01460 -0.0103 0.9713 0.1167
-6.500 -0.6701 0.02340 0.01404 -0.0104 0.9655 0.1324
-6.250 -0.6443 0.02282 0.01347 -0.0106 0.9597 0.1489
-6.000 -0.6138 0.02223 0.01293 -0.0118 0.9556 0.1687
-5.750 -0.5937 0.02171 0.01244 -0.0108 0.9481 0.1873
-5.500 -0.5660 0.02112 0.01192 -0.0113 0.9430 0.2115
-5.250 -0.5418 0.02054 0.01144 -0.0111 0.9371 0.2412
-5.000 -0.5205 0.01994 0.01101 -0.0102 0.9301 0.2796
-4.750 -0.4928 0.01924 0.01058 -0.0107 0.9258 0.3369
-4.500 -0.4786 0.01870 0.01031 -0.0083 0.9172 0.3973
-4.250 -0.4530 0.01817 0.01006 -0.0079 0.9122 0.4704
-4.000 -0.4306 0.01783 0.00993 -0.0068 0.9058 0.5304
-3.750 -0.4057 0.01758 0.00980 -0.0060 0.8994 0.5814
-3.500 -0.3713 0.01737 0.00969 -0.0070 0.8959 0.6282
-3.250 -0.3450 0.01731 0.00970 -0.0064 0.8892 0.6644
-3.000 -0.3116 0.01727 0.00969 -0.0071 0.8841 0.6983
-2.750 -0.2711 0.01726 0.00968 -0.0092 0.8810 0.7287
-2.500 -0.2374 0.01733 0.00974 -0.0100 0.8757 0.7558
-2.250 -0.2044 0.01748 0.00986 -0.0105 0.8696 0.7824
-2.000 -0.1584 0.01769 0.01005 -0.0135 0.8666 0.8053
-1.750 -0.1117 0.01784 0.01012 -0.0167 0.8640 0.8221
-1.500 -0.0828 0.01804 0.01028 -0.0167 0.8558 0.8361
-1.250 -0.0435 0.01808 0.01025 -0.0187 0.8511 0.8483
-1.000 0.0077 0.01814 0.01024 -0.0230 0.8484 0.8551
-0.750 0.0348 0.01826 0.01033 -0.0228 0.8392 0.8655
-0.500 0.0823 0.01825 0.01026 -0.0266 0.8349 0.8712
-0.250 0.1137 0.01828 0.01026 -0.0273 0.8272 0.8801
0.000 0.1586 0.01829 0.01024 -0.0306 0.8211 0.8848
0.250 0.1889 0.01824 0.01016 -0.0311 0.8137 0.8940
0.500 0.2321 0.01826 0.01017 -0.0341 0.8061 0.8978
0.750 0.2717 0.01821 0.01010 -0.0364 0.7989 0.9035
1.000 0.3025 0.01818 0.01008 -0.0370 0.7896 0.9109
1.250 0.3422 0.01817 0.01007 -0.0394 0.7807 0.9156
1.500 0.3747 0.01807 0.00997 -0.0403 0.7718 0.9229
1.750 0.4097 0.01807 0.00999 -0.0418 0.7604 0.9279
2.000 0.4460 0.01801 0.00995 -0.0435 0.7495 0.9331
2.250 0.4758 0.01794 0.00987 -0.0439 0.7384 0.9403
2.500 0.5139 0.01787 0.00984 -0.0460 0.7255 0.9443
2.750 0.5458 0.01785 0.00985 -0.0469 0.7119 0.9502
3.000 0.5755 0.01785 0.00988 -0.0473 0.6984 0.9564
3.250 0.6115 0.01779 0.00987 -0.0491 0.6842 0.9608
3.500 0.6422 0.01779 0.00990 -0.0497 0.6694 0.9668
3.750 0.6747 0.01776 0.00989 -0.0507 0.6526 0.9718
4.000 0.7083 0.01770 0.00985 -0.0519 0.6332 0.9765
4.250 0.7367 0.01775 0.00990 -0.0522 0.6125 0.9824
4.500 0.7699 0.01773 0.00990 -0.0534 0.5897 0.9868
4.750 0.8006 0.01778 0.00996 -0.0542 0.5663 0.9919
5.000 0.8312 0.01785 0.01004 -0.0550 0.5407 0.9967
5.250 0.8564 0.01798 0.01018 -0.0548 0.5133 1.0000
5.500 0.8682 0.01820 0.01038 -0.0518 0.4874 1.0000
5.750 0.8786 0.01846 0.01059 -0.0486 0.4588 1.0000
6.000 0.8874 0.01878 0.01082 -0.0451 0.4277 1.0000
6.250 0.8945 0.01917 0.01110 -0.0413 0.3952 1.0000
6.500 0.8997 0.01963 0.01143 -0.0373 0.3626 1.0000
6.750 0.9035 0.02015 0.01182 -0.0330 0.3309 1.0000
7.000 0.9059 0.02072 0.01225 -0.0286 0.3013 1.0000
7.250 0.9072 0.02131 0.01271 -0.0239 0.2736 1.0000
7.500 0.9076 0.02192 0.01320 -0.0192 0.2483 1.0000
7.750 0.9078 0.02251 0.01371 -0.0145 0.2247 1.0000
8.000 0.9050 0.02309 0.01419 -0.0092 0.2047 1.0000
8.250 0.9024 0.02369 0.01471 -0.0040 0.1867 1.0000
8.500 0.9020 0.02433 0.01530 0.0006 0.1690 1.0000
8.750 0.9026 0.02503 0.01594 0.0049 0.1526 1.0000
9.000 0.9041 0.02580 0.01666 0.0089 0.1374 1.0000
9.250 0.9063 0.02663 0.01746 0.0126 0.1238 1.0000
9.500 0.9090 0.02753 0.01832 0.0161 0.1109 1.0000
9.750 0.9116 0.02852 0.01928 0.0194 0.0990 1.0000
10.000 0.9137 0.02961 0.02032 0.0226 0.0887 1.0000
10.250 0.9177 0.03069 0.02144 0.0254 0.0789 1.0000
10.500 0.9210 0.03187 0.02265 0.0282 0.0711 1.0000
10.750 0.9220 0.03326 0.02400 0.0309 0.0652 1.0000
11.000 0.9263 0.03455 0.02537 0.0333 0.0591 1.0000
11.250 0.9273 0.03608 0.02690 0.0357 0.0551 1.0000
11.500 0.9308 0.03758 0.02849 0.0378 0.0518 1.0000
11.750 0.9342 0.03912 0.03010 0.0397 0.0482 1.0000
12.000 0.9353 0.04087 0.03187 0.0415 0.0457 1.0000
12.250 0.9384 0.04263 0.03374 0.0432 0.0432 1.0000
12.500 0.9426 0.04437 0.03561 0.0447 0.0412 1.0000
12.750 0.9456 0.04623 0.03754 0.0460 0.0393 1.0000
13.000 0.9477 0.04820 0.03956 0.0472 0.0379 1.0000
13.250 0.9496 0.05031 0.04172 0.0482 0.0363 1.0000
13.500 0.9542 0.05236 0.04395 0.0493 0.0351 1.0000
13.750 0.9561 0.05461 0.04637 0.0501 0.0337 1.0000
14.000 0.9570 0.05701 0.04889 0.0507 0.0324 1.0000
14.250 0.9579 0.05948 0.05146 0.0513 0.0315 1.0000
14.500 0.9587 0.06202 0.05410 0.0517 0.0308 1.0000
14.750 0.9599 0.06462 0.05675 0.0520 0.0302 1.0000
15.000 0.9574 0.06782 0.06011 0.0521 0.0296 1.0000
15.250 0.9500 0.07163 0.06418 0.0517 0.0290 1.0000
15.500 0.9411 0.07576 0.06855 0.0509 0.0285 1.0000
15.750 0.9304 0.08033 0.07334 0.0497 0.0282 1.0000
16.000 0.9161 0.08560 0.07883 0.0479 0.0277 1.0000
16.250 0.9009 0.09133 0.08477 0.0456 0.0276 1.0000
16.500 0.8815 0.09808 0.09173 0.0424 0.0274 1.0000
16.750 0.8584 0.10604 0.09991 0.0383 0.0275 1.0000
17.000 0.8275 0.11623 0.11032 0.0327 0.0279 1.0000
17.250 0.7835 0.13067 0.12495 0.0244 0.0284 1.0000
17.500 0.7331 0.14879 0.14314 0.0151 0.0294 1.0000
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