Joukovsky f=0% t=15% (joukowsk0015-jf) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: Joukovsky f=0% t=15% (joukowsk0015-jf) Reynolds number: 500,000 Max Cl/Cd: 68.36 at α=8.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-joukowsk0015-jf-500000-n5.txt Download as CSV file: xf-joukowsk0015-jf-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: Joukovsky f=0% t=15%
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.000 -1.2214 0.11186 0.10762 0.0127 1.0000 0.0295
-18.750 -1.2318 0.10597 0.10165 0.0093 1.0000 0.0299
-18.500 -1.2419 0.10021 0.09581 0.0061 1.0000 0.0303
-18.250 -1.2518 0.09462 0.09012 0.0030 1.0000 0.0308
-18.000 -1.2611 0.08922 0.08462 0.0001 1.0000 0.0311
-17.750 -1.2700 0.08399 0.07929 -0.0027 1.0000 0.0316
-17.500 -1.2780 0.07903 0.07423 -0.0052 1.0000 0.0321
-17.250 -1.2858 0.07418 0.06927 -0.0077 1.0000 0.0325
-17.000 -1.2938 0.06944 0.06443 -0.0100 1.0000 0.0329
-16.750 -1.3045 0.06441 0.05932 -0.0125 1.0000 0.0333
-16.500 -1.3130 0.05989 0.05471 -0.0146 1.0000 0.0338
-16.250 -1.3202 0.05570 0.05043 -0.0164 1.0000 0.0343
-16.000 -1.3261 0.05180 0.04645 -0.0180 1.0000 0.0348
-15.750 -1.3300 0.04827 0.04282 -0.0193 1.0000 0.0354
-15.500 -1.3321 0.04502 0.03949 -0.0204 1.0000 0.0360
-15.250 -1.3322 0.04212 0.03649 -0.0212 1.0000 0.0367
-14.750 -1.3320 0.03660 0.03082 -0.0225 1.0000 0.0380
-14.500 -1.3307 0.03413 0.02829 -0.0229 1.0000 0.0387
-14.250 -1.3272 0.03200 0.02609 -0.0230 1.0000 0.0397
-14.000 -1.3221 0.03011 0.02413 -0.0228 1.0000 0.0406
-13.750 -1.3152 0.02848 0.02242 -0.0225 1.0000 0.0416
-13.500 -1.3092 0.02689 0.02077 -0.0219 1.0000 0.0424
-13.250 -1.3032 0.02542 0.01926 -0.0211 1.0000 0.0434
-13.000 -1.2958 0.02419 0.01798 -0.0200 1.0000 0.0446
-12.750 -1.2871 0.02315 0.01689 -0.0187 1.0000 0.0459
-12.500 -1.2771 0.02231 0.01599 -0.0171 1.0000 0.0472
-12.250 -1.2688 0.02146 0.01511 -0.0151 1.0000 0.0485
-12.000 -1.2559 0.02074 0.01437 -0.0135 1.0000 0.0502
-11.750 -1.2388 0.02011 0.01370 -0.0124 1.0000 0.0519
-11.500 -1.2203 0.01950 0.01305 -0.0114 1.0000 0.0537
-11.250 -1.2014 0.01887 0.01242 -0.0105 1.0000 0.0559
-11.000 -1.1806 0.01833 0.01186 -0.0098 1.0000 0.0583
-10.750 -1.1594 0.01779 0.01130 -0.0091 1.0000 0.0606
-10.500 -1.1376 0.01726 0.01076 -0.0085 1.0000 0.0634
-10.250 -1.1145 0.01681 0.01029 -0.0079 1.0000 0.0662
-10.000 -1.0918 0.01629 0.00979 -0.0074 1.0000 0.0695
-9.750 -1.0680 0.01586 0.00935 -0.0069 1.0000 0.0730
-9.500 -1.0440 0.01540 0.00890 -0.0065 1.0000 0.0765
-9.250 -1.0195 0.01499 0.00849 -0.0061 1.0000 0.0808
-9.000 -0.9946 0.01457 0.00809 -0.0058 1.0000 0.0849
-8.750 -0.9694 0.01418 0.00772 -0.0055 1.0000 0.0897
-8.500 -0.9434 0.01380 0.00735 -0.0054 0.9912 0.0945
-8.250 -0.9087 0.01345 0.00700 -0.0069 0.9449 0.1009
-8.000 -0.8838 0.01316 0.00668 -0.0063 0.9123 0.1067
-7.500 -0.8370 0.01266 0.00609 -0.0044 0.8652 0.1193
-7.250 -0.8120 0.01244 0.00582 -0.0037 0.8461 0.1260
-7.000 -0.7868 0.01217 0.00553 -0.0032 0.8282 0.1338
-6.750 -0.7609 0.01194 0.00526 -0.0027 0.8113 0.1414
-6.500 -0.7346 0.01171 0.00500 -0.0023 0.7951 0.1499
-6.250 -0.7080 0.01147 0.00475 -0.0020 0.7797 0.1588
-6.000 -0.6810 0.01127 0.00452 -0.0017 0.7649 0.1678
-5.750 -0.6540 0.01106 0.00429 -0.0015 0.7505 0.1780
-5.500 -0.6268 0.01085 0.00408 -0.0013 0.7362 0.1881
-5.250 -0.5991 0.01067 0.00388 -0.0011 0.7221 0.1982
-5.000 -0.5715 0.01049 0.00369 -0.0009 0.7088 0.2094
-4.500 -0.5158 0.01015 0.00335 -0.0007 0.6816 0.2317
-4.250 -0.4877 0.01001 0.00319 -0.0006 0.6687 0.2436
-3.750 -0.4313 0.00972 0.00291 -0.0004 0.6424 0.2674
-3.500 -0.4028 0.00962 0.00279 -0.0003 0.6301 0.2794
-3.250 -0.3745 0.00950 0.00267 -0.0003 0.6169 0.2922
-3.000 -0.3460 0.00938 0.00256 -0.0002 0.6045 0.3043
-2.750 -0.3173 0.00930 0.00247 -0.0002 0.5920 0.3164
-2.500 -0.2887 0.00921 0.00238 -0.0001 0.5790 0.3295
-2.250 -0.2600 0.00912 0.00230 -0.0001 0.5667 0.3418
-2.000 -0.2312 0.00906 0.00223 -0.0001 0.5544 0.3542
-1.750 -0.2024 0.00901 0.00217 -0.0001 0.5416 0.3670
-1.500 -0.1736 0.00894 0.00212 0.0000 0.5294 0.3797
-1.250 -0.1447 0.00891 0.00207 0.0000 0.5170 0.3919
-1.000 -0.1157 0.00887 0.00204 0.0000 0.5042 0.4047
-0.750 -0.0868 0.00883 0.00201 0.0000 0.4921 0.4174
-0.500 -0.0580 0.00882 0.00199 0.0000 0.4795 0.4296
-0.250 -0.0289 0.00881 0.00198 0.0000 0.4669 0.4422
0.000 0.0000 0.00880 0.00197 0.0000 0.4547 0.4548
0.250 0.0289 0.00881 0.00198 0.0000 0.4422 0.4669
0.500 0.0580 0.00882 0.00199 0.0000 0.4295 0.4796
0.750 0.0869 0.00883 0.00201 0.0000 0.4173 0.4921
1.000 0.1157 0.00887 0.00204 0.0000 0.4046 0.5042
1.250 0.1447 0.00891 0.00207 0.0000 0.3919 0.5170
1.500 0.1736 0.00894 0.00212 0.0000 0.3797 0.5294
1.750 0.2024 0.00901 0.00217 0.0001 0.3671 0.5416
2.000 0.2312 0.00906 0.00223 0.0001 0.3542 0.5545
2.250 0.2600 0.00912 0.00230 0.0001 0.3418 0.5668
2.500 0.2887 0.00921 0.00238 0.0001 0.3295 0.5791
2.750 0.3173 0.00930 0.00247 0.0002 0.3165 0.5919
3.000 0.3460 0.00938 0.00256 0.0002 0.3043 0.6043
3.250 0.3745 0.00950 0.00267 0.0003 0.2922 0.6169
3.500 0.4028 0.00962 0.00279 0.0003 0.2795 0.6300
3.750 0.4313 0.00972 0.00291 0.0004 0.2673 0.6425
4.250 0.4877 0.01001 0.00319 0.0006 0.2437 0.6687
4.500 0.5158 0.01015 0.00335 0.0007 0.2317 0.6817
5.000 0.5715 0.01049 0.00369 0.0009 0.2095 0.7088
5.250 0.5991 0.01067 0.00388 0.0011 0.1982 0.7221
5.500 0.6268 0.01085 0.00408 0.0013 0.1882 0.7362
5.750 0.6540 0.01106 0.00429 0.0015 0.1781 0.7505
6.000 0.6810 0.01127 0.00452 0.0017 0.1677 0.7650
6.250 0.7080 0.01147 0.00475 0.0020 0.1588 0.7795
6.500 0.7345 0.01171 0.00500 0.0023 0.1499 0.7951
6.750 0.7609 0.01194 0.00526 0.0027 0.1414 0.8114
7.000 0.7868 0.01217 0.00553 0.0032 0.1338 0.8282
7.250 0.8120 0.01244 0.00582 0.0037 0.1259 0.8460
7.500 0.8370 0.01266 0.00609 0.0044 0.1193 0.8653
8.000 0.8837 0.01316 0.00668 0.0063 0.1066 0.9123
8.250 0.9087 0.01345 0.00700 0.0069 0.1009 0.9449
8.500 0.9434 0.01380 0.00735 0.0054 0.0946 0.9912
8.750 0.9694 0.01418 0.00772 0.0055 0.0897 1.0000
9.000 0.9946 0.01458 0.00809 0.0058 0.0848 1.0000
9.250 1.0194 0.01498 0.00849 0.0062 0.0808 1.0000
9.500 1.0440 0.01540 0.00890 0.0065 0.0766 1.0000
9.750 1.0680 0.01586 0.00934 0.0069 0.0730 1.0000
10.000 1.0918 0.01629 0.00979 0.0074 0.0695 1.0000
10.250 1.1146 0.01681 0.01029 0.0079 0.0662 1.0000
10.500 1.1377 0.01726 0.01076 0.0084 0.0634 1.0000
10.750 1.1595 0.01779 0.01130 0.0091 0.0607 1.0000
11.000 1.1807 0.01833 0.01185 0.0098 0.0582 1.0000
11.250 1.2014 0.01887 0.01242 0.0105 0.0558 1.0000
11.500 1.2203 0.01950 0.01305 0.0114 0.0537 1.0000
11.750 1.2388 0.02011 0.01370 0.0124 0.0519 1.0000
12.000 1.2559 0.02074 0.01436 0.0135 0.0501 1.0000
12.250 1.2689 0.02145 0.01510 0.0151 0.0486 1.0000
12.500 1.2772 0.02230 0.01598 0.0171 0.0472 1.0000
12.750 1.2873 0.02315 0.01689 0.0187 0.0459 1.0000
13.000 1.2962 0.02418 0.01797 0.0200 0.0446 1.0000
13.250 1.3038 0.02541 0.01924 0.0211 0.0434 1.0000
13.500 1.3097 0.02688 0.02075 0.0219 0.0424 1.0000
13.750 1.3161 0.02844 0.02238 0.0224 0.0415 1.0000
14.000 1.3229 0.03009 0.02410 0.0228 0.0406 1.0000
14.250 1.3282 0.03196 0.02604 0.0229 0.0396 1.0000
14.500 1.3318 0.03410 0.02825 0.0228 0.0388 1.0000
14.750 1.3333 0.03654 0.03075 0.0224 0.0379 1.0000
15.000 1.3323 0.03937 0.03365 0.0218 0.0373 1.0000
15.250 1.3338 0.04202 0.03639 0.0212 0.0366 1.0000
15.500 1.3334 0.04497 0.03943 0.0203 0.0360 1.0000
15.750 1.3315 0.04819 0.04274 0.0192 0.0353 1.0000
16.000 1.3276 0.05173 0.04637 0.0179 0.0348 1.0000
16.250 1.3219 0.05558 0.05031 0.0163 0.0343 1.0000
16.500 1.3145 0.05979 0.05460 0.0145 0.0338 1.0000
16.750 1.3058 0.06434 0.05924 0.0124 0.0333 1.0000
17.000 1.2951 0.06935 0.06433 0.0099 0.0329 1.0000
17.250 1.2867 0.07414 0.06922 0.0076 0.0326 1.0000
17.500 1.2801 0.07881 0.07401 0.0052 0.0320 1.0000
17.750 1.2715 0.08387 0.07917 0.0026 0.0316 1.0000
18.000 1.2629 0.08906 0.08445 -0.0002 0.0312 1.0000
18.250 1.2537 0.09445 0.08995 -0.0031 0.0308 1.0000
18.500 1.2440 0.10001 0.09560 -0.0061 0.0303 1.0000
18.750 1.2337 0.10581 0.10148 -0.0094 0.0299 1.0000
19.000 1.2234 0.11170 0.10746 -0.0128 0.0295 1.0000
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