HAWKER TEMPEST 61% SEMISPAN AIRFOIL (tempest2-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: HAWKER TEMPEST 61% SEMISPAN AIRFOIL (tempest2-il) Reynolds number: 200,000 Max Cl/Cd: 55.01 at α=4.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-tempest2-il-200000-n5.txt Download as CSV file: xf-tempest2-il-200000-n5.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 = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.250 -0.6682 0.08685 0.08296 -0.0443 1.0000 0.0134
-13.000 -0.6950 0.07644 0.07246 -0.0511 1.0000 0.0132
-12.750 -0.7234 0.06712 0.06296 -0.0579 1.0000 0.0131
-12.500 -0.7415 0.06129 0.05706 -0.0608 1.0000 0.0123
-12.250 -0.7651 0.05564 0.05119 -0.0634 1.0000 0.0125
-12.000 -0.7863 0.05122 0.04656 -0.0637 1.0000 0.0126
-11.750 -0.8033 0.04787 0.04301 -0.0625 1.0000 0.0126
-11.500 -0.8210 0.04496 0.03984 -0.0600 1.0000 0.0129
-11.250 -0.8370 0.04258 0.03718 -0.0563 1.0000 0.0133
-11.000 -0.8492 0.04047 0.03488 -0.0520 1.0000 0.0132
-10.750 -0.8628 0.03882 0.03299 -0.0467 1.0000 0.0134
-10.500 -0.8725 0.03729 0.03123 -0.0414 1.0000 0.0135
-10.250 -0.8780 0.03526 0.02900 -0.0370 1.0000 0.0138
-10.000 -0.8787 0.03360 0.02717 -0.0330 1.0000 0.0139
-9.750 -0.8773 0.03216 0.02561 -0.0292 1.0000 0.0142
-9.500 -0.8735 0.03084 0.02412 -0.0256 1.0000 0.0144
-9.250 -0.8683 0.02968 0.02284 -0.0222 1.0000 0.0148
-9.000 -0.8619 0.02856 0.02157 -0.0189 1.0000 0.0152
-8.750 -0.8542 0.02740 0.02026 -0.0157 1.0000 0.0155
-8.500 -0.8449 0.02635 0.01907 -0.0127 0.9999 0.0159
-8.250 -0.8179 0.02499 0.01751 -0.0134 0.9969 0.0168
-8.000 -0.7897 0.02391 0.01624 -0.0141 0.9939 0.0178
-7.750 -0.7651 0.02266 0.01488 -0.0143 0.9901 0.0192
-7.500 -0.7379 0.02172 0.01388 -0.0149 0.9865 0.0205
-7.250 -0.7088 0.02079 0.01284 -0.0158 0.9834 0.0219
-7.000 -0.6838 0.01995 0.01187 -0.0157 0.9788 0.0234
-6.750 -0.6575 0.01907 0.01091 -0.0159 0.9743 0.0253
-6.500 -0.6274 0.01836 0.01014 -0.0169 0.9710 0.0292
-6.250 -0.6013 0.01766 0.00936 -0.0169 0.9662 0.0335
-6.000 -0.5746 0.01702 0.00869 -0.0171 0.9611 0.0396
-5.500 -0.5150 0.01575 0.00755 -0.0188 0.9537 0.0749
-5.250 -0.4903 0.01528 0.00715 -0.0184 0.9474 0.0973
-5.000 -0.4591 0.01480 0.00674 -0.0195 0.9437 0.1220
-4.750 -0.4259 0.01431 0.00633 -0.0210 0.9412 0.1500
-4.500 -0.4044 0.01387 0.00600 -0.0200 0.9336 0.1805
-4.250 -0.3755 0.01328 0.00562 -0.0206 0.9294 0.2314
-4.000 -0.3468 0.01263 0.00525 -0.0212 0.9258 0.2987
-3.750 -0.3293 0.01208 0.00498 -0.0194 0.9173 0.3701
-3.500 -0.3033 0.01149 0.00470 -0.0192 0.9129 0.4544
-3.250 -0.2839 0.01110 0.00455 -0.0175 0.9051 0.5195
-3.000 -0.2575 0.01074 0.00437 -0.0171 0.8998 0.5783
-2.750 -0.2318 0.01047 0.00423 -0.0165 0.8938 0.6260
-2.500 -0.2058 0.01026 0.00414 -0.0159 0.8871 0.6680
-2.250 -0.1733 0.01007 0.00404 -0.0166 0.8829 0.7069
-2.000 -0.1475 0.00998 0.00402 -0.0159 0.8748 0.7396
-1.750 -0.1139 0.00989 0.00397 -0.0168 0.8696 0.7700
-1.500 -0.0828 0.00988 0.00402 -0.0172 0.8626 0.8014
-1.250 -0.0474 0.00992 0.00409 -0.0183 0.8564 0.8311
-1.000 -0.0141 0.00997 0.00413 -0.0191 0.8495 0.8509
-0.750 0.0206 0.01003 0.00416 -0.0203 0.8421 0.8648
-0.500 0.0570 0.01009 0.00419 -0.0219 0.8346 0.8747
-0.250 0.0897 0.01013 0.00418 -0.0228 0.8262 0.8842
0.000 0.1234 0.01019 0.00422 -0.0238 0.8168 0.8917
0.250 0.1565 0.01023 0.00421 -0.0248 0.8080 0.8989
0.500 0.1911 0.01030 0.00425 -0.0261 0.7974 0.9045
0.750 0.2192 0.01034 0.00427 -0.0260 0.7861 0.9123
1.000 0.2562 0.01041 0.00431 -0.0279 0.7746 0.9159
1.250 0.2887 0.01047 0.00434 -0.0288 0.7616 0.9213
1.500 0.3181 0.01053 0.00437 -0.0290 0.7473 0.9273
1.750 0.3538 0.01062 0.00443 -0.0306 0.7319 0.9305
2.000 0.3857 0.01070 0.00449 -0.0314 0.7163 0.9352
2.250 0.4127 0.01078 0.00455 -0.0312 0.7008 0.9414
2.500 0.4477 0.01088 0.00464 -0.0327 0.6840 0.9444
2.750 0.4795 0.01099 0.00471 -0.0335 0.6647 0.9486
3.000 0.5037 0.01112 0.00479 -0.0327 0.6421 0.9553
3.250 0.5374 0.01126 0.00488 -0.0340 0.6156 0.9582
3.500 0.5686 0.01142 0.00499 -0.0348 0.5908 0.9622
3.750 0.5948 0.01160 0.00513 -0.0345 0.5655 0.9680
4.000 0.6254 0.01180 0.00529 -0.0352 0.5354 0.9718
4.250 0.6556 0.01205 0.00545 -0.0359 0.4994 0.9759
4.500 0.6810 0.01238 0.00565 -0.0357 0.4538 0.9813
4.750 0.7071 0.01288 0.00587 -0.0358 0.3872 0.9855
5.000 0.7315 0.01357 0.00622 -0.0358 0.3121 0.9902
5.250 0.7556 0.01432 0.00663 -0.0358 0.2435 0.9946
5.500 0.7826 0.01500 0.00706 -0.0365 0.1872 0.9984
5.750 0.8015 0.01561 0.00748 -0.0353 0.1468 1.0000
6.000 0.8127 0.01616 0.00791 -0.0325 0.1168 1.0000
6.250 0.8239 0.01670 0.00834 -0.0297 0.0920 1.0000
6.500 0.8345 0.01727 0.00881 -0.0267 0.0710 1.0000
6.750 0.8451 0.01783 0.00931 -0.0237 0.0556 1.0000
7.000 0.8550 0.01842 0.00986 -0.0205 0.0444 1.0000
7.250 0.8643 0.01903 0.01044 -0.0173 0.0379 1.0000
7.500 0.8744 0.01958 0.01108 -0.0141 0.0336 1.0000
7.750 0.8819 0.02027 0.01178 -0.0106 0.0302 1.0000
8.000 0.8905 0.02089 0.01247 -0.0072 0.0279 1.0000
8.250 0.8992 0.02149 0.01314 -0.0039 0.0256 1.0000
8.500 0.9056 0.02213 0.01382 -0.0003 0.0238 1.0000
8.750 0.9067 0.02295 0.01467 0.0042 0.0225 1.0000
9.000 0.9117 0.02370 0.01550 0.0081 0.0216 1.0000
9.250 0.9176 0.02453 0.01645 0.0116 0.0206 1.0000
9.500 0.9253 0.02533 0.01734 0.0146 0.0195 1.0000
9.750 0.9326 0.02624 0.01832 0.0175 0.0186 1.0000
10.000 0.9403 0.02718 0.01931 0.0202 0.0178 1.0000
10.250 0.9454 0.02841 0.02058 0.0230 0.0170 1.0000
10.500 0.9531 0.02962 0.02190 0.0254 0.0162 1.0000
10.750 0.9616 0.03088 0.02329 0.0277 0.0158 1.0000
11.000 0.9697 0.03224 0.02480 0.0299 0.0151 1.0000
11.250 0.9774 0.03372 0.02642 0.0319 0.0147 1.0000
11.500 0.9840 0.03524 0.02811 0.0339 0.0142 1.0000
11.750 0.9896 0.03689 0.02990 0.0358 0.0138 1.0000
12.000 0.9942 0.03864 0.03180 0.0377 0.0136 1.0000
12.250 0.9971 0.04036 0.03363 0.0393 0.0132 1.0000
12.500 0.9989 0.04229 0.03567 0.0408 0.0129 1.0000
12.750 0.9984 0.04454 0.03800 0.0422 0.0125 1.0000
13.000 0.9964 0.04723 0.04090 0.0435 0.0124 1.0000
13.250 0.9900 0.05005 0.04397 0.0444 0.0121 1.0000
13.500 0.9824 0.05328 0.04745 0.0450 0.0118 1.0000
13.750 0.9729 0.05691 0.05131 0.0451 0.0117 1.0000
14.000 0.9610 0.06098 0.05562 0.0445 0.0115 1.0000
14.250 0.9478 0.06552 0.06038 0.0433 0.0113 1.0000
14.500 0.9318 0.07082 0.06589 0.0415 0.0114 1.0000
14.750 0.9141 0.07683 0.07210 0.0388 0.0114 1.0000
15.000 0.8936 0.08384 0.07932 0.0351 0.0113 1.0000
15.250 0.8737 0.09141 0.08706 0.0308 0.0114 1.0000
15.500 0.8496 0.10048 0.09630 0.0255 0.0116 1.0000
15.750 0.8183 0.11229 0.10828 0.0185 0.0117 1.0000
16.000 0.7910 0.12376 0.11985 0.0122 0.0120 1.0000
16.250 0.7458 0.14154 0.13770 0.0035 0.0125 1.0000
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