WORTMANN FX 05-188 AIRFOIL (fx05188-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: WORTMANN FX 05-188 AIRFOIL (fx05188-il) Reynolds number: 500,000 Max Cl/Cd: 99.52 at α=6.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx05188-il-500000.txt Download as CSV file: xf-fx05188-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 05-188 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
------ -------- --------- --------- -------- -------- --------
-13.750 -0.2514 0.07289 0.06983 -0.1244 0.8579 0.0415
-13.500 -0.2907 0.06340 0.06022 -0.1291 0.8548 0.0412
-13.250 -0.3247 0.05592 0.05260 -0.1322 0.8507 0.0409
-13.000 -0.3637 0.04951 0.04597 -0.1344 0.8460 0.0412
-12.750 -0.3917 0.04492 0.04122 -0.1351 0.8408 0.0413
-12.500 -0.4185 0.04123 0.03736 -0.1347 0.8352 0.0415
-12.250 -0.6037 0.03618 0.03051 -0.1311 0.8389 0.0259
-12.000 -0.6006 0.03466 0.02879 -0.1293 0.8325 0.0258
-11.750 -0.5936 0.03390 0.02786 -0.1278 0.8270 0.0256
-11.500 -0.5586 0.03116 0.02503 -0.1291 0.8243 0.0251
-11.250 -0.5403 0.02948 0.02321 -0.1286 0.8203 0.0250
-11.000 -0.5256 0.02825 0.02181 -0.1276 0.8163 0.0251
-10.750 -0.5009 0.02692 0.02033 -0.1277 0.8131 0.0251
-10.500 -0.4785 0.02593 0.01921 -0.1274 0.8097 0.0252
-10.250 -0.4547 0.02497 0.01817 -0.1271 0.8066 0.0252
-10.000 -0.4347 0.02425 0.01737 -0.1265 0.8033 0.0254
-9.750 -0.4121 0.02355 0.01657 -0.1261 0.8000 0.0255
-9.500 -0.3752 0.02254 0.01556 -0.1267 0.7979 0.0260
-9.250 -0.3517 0.02189 0.01490 -0.1263 0.7951 0.0264
-9.000 -0.3327 0.02130 0.01431 -0.1255 0.7922 0.0268
-8.750 -0.3154 0.02071 0.01373 -0.1245 0.7892 0.0273
-8.500 -0.2988 0.02012 0.01312 -0.1234 0.7861 0.0279
-8.250 -0.2827 0.01953 0.01251 -0.1223 0.7833 0.0282
-8.000 -0.2671 0.01895 0.01188 -0.1211 0.7807 0.0285
-7.750 -0.2516 0.01838 0.01126 -0.1199 0.7781 0.0292
-7.500 -0.2377 0.01781 0.01068 -0.1184 0.7756 0.0296
-7.250 -0.2243 0.01724 0.01009 -0.1168 0.7728 0.0301
-7.000 -0.2107 0.01669 0.00952 -0.1152 0.7700 0.0304
-6.750 -0.2019 0.01599 0.00879 -0.1130 0.7672 0.0310
-6.500 -0.1950 0.01541 0.00819 -0.1103 0.7648 0.0320
-6.250 -0.1825 0.01501 0.00774 -0.1085 0.7624 0.0329
-6.000 -0.1666 0.01459 0.00732 -0.1073 0.7599 0.0343
-5.750 -0.1479 0.01423 0.00694 -0.1064 0.7572 0.0358
-5.500 -0.1288 0.01381 0.00652 -0.1056 0.7547 0.0384
-5.250 -0.1070 0.01349 0.00618 -0.1052 0.7524 0.0421
-5.000 -0.0873 0.01292 0.00574 -0.1046 0.7500 0.0682
-4.500 -0.0560 0.00978 0.00418 -0.1050 0.7451 0.4364
-4.250 -0.0281 0.00935 0.00404 -0.1058 0.7426 0.5174
-4.000 0.0009 0.00920 0.00399 -0.1064 0.7402 0.5554
-3.750 0.0301 0.00916 0.00404 -0.1068 0.7378 0.5856
-3.500 0.0599 0.00921 0.00409 -0.1073 0.7354 0.6068
-3.250 0.0899 0.00934 0.00420 -0.1078 0.7331 0.6227
-3.000 0.1201 0.00957 0.00439 -0.1083 0.7307 0.6350
-2.750 0.1486 0.00975 0.00457 -0.1084 0.7282 0.6423
-2.500 0.1775 0.00992 0.00471 -0.1087 0.7255 0.6505
-2.250 0.2061 0.01005 0.00484 -0.1088 0.7228 0.6560
-2.000 0.2348 0.01018 0.00496 -0.1090 0.7201 0.6604
-1.750 0.2650 0.01024 0.00496 -0.1097 0.7175 0.6650
-1.500 0.2959 0.01030 0.00492 -0.1105 0.7149 0.6692
-1.250 0.3240 0.01040 0.00504 -0.1106 0.7121 0.6718
-1.000 0.3514 0.01046 0.00513 -0.1106 0.7092 0.6749
-0.750 0.3801 0.01052 0.00518 -0.1110 0.7061 0.6784
-0.500 0.4101 0.01055 0.00517 -0.1116 0.7032 0.6825
-0.250 0.4399 0.01057 0.00516 -0.1122 0.7003 0.6859
0.000 0.4688 0.01069 0.00526 -0.1124 0.6973 0.6888
0.250 0.4957 0.01079 0.00540 -0.1123 0.6938 0.6921
0.500 0.5233 0.01081 0.00544 -0.1124 0.6896 0.6960
0.750 0.5531 0.01082 0.00541 -0.1130 0.6855 0.7001
1.000 0.5823 0.01080 0.00538 -0.1134 0.6823 0.7028
1.250 0.6116 0.01091 0.00547 -0.1138 0.6792 0.7050
1.500 0.6376 0.01092 0.00555 -0.1136 0.6758 0.7074
1.750 0.6652 0.01094 0.00560 -0.1137 0.6719 0.7100
2.000 0.6941 0.01094 0.00561 -0.1141 0.6683 0.7130
2.250 0.7244 0.01096 0.00559 -0.1149 0.6651 0.7163
2.500 0.7541 0.01100 0.00562 -0.1155 0.6620 0.7189
2.750 0.7795 0.01100 0.00571 -0.1151 0.6580 0.7210
3.000 0.8065 0.01101 0.00577 -0.1151 0.6539 0.7230
3.250 0.8347 0.01100 0.00577 -0.1153 0.6499 0.7251
3.500 0.8626 0.01099 0.00576 -0.1154 0.6450 0.7275
3.750 0.8888 0.01096 0.00579 -0.1153 0.6388 0.7301
4.000 0.9173 0.01094 0.00578 -0.1157 0.6341 0.7329
4.250 0.9463 0.01096 0.00578 -0.1161 0.6297 0.7353
4.500 0.9711 0.01095 0.00586 -0.1157 0.6237 0.7371
4.750 0.9970 0.01093 0.00584 -0.1154 0.6166 0.7388
5.000 1.0203 0.01093 0.00589 -0.1146 0.6061 0.7406
5.250 1.0438 0.01096 0.00592 -0.1139 0.5942 0.7426
5.500 1.0672 0.01106 0.00598 -0.1132 0.5825 0.7447
5.750 1.0904 0.01117 0.00609 -0.1125 0.5704 0.7472
6.000 1.1143 0.01130 0.00623 -0.1120 0.5595 0.7495
6.250 1.1377 0.01147 0.00637 -0.1115 0.5482 0.7514
6.500 1.1574 0.01163 0.00652 -0.1101 0.5341 0.7530
6.750 1.1749 0.01185 0.00673 -0.1084 0.5180 0.7546
7.000 1.1908 0.01210 0.00698 -0.1063 0.5004 0.7564
7.250 1.2029 0.01237 0.00724 -0.1035 0.4818 0.7583
7.500 1.2118 0.01275 0.00757 -0.1003 0.4594 0.7604
7.750 1.2162 0.01336 0.00807 -0.0964 0.4317 0.7627
8.000 1.2169 0.01419 0.00876 -0.0922 0.4026 0.7650
8.250 1.2161 0.01520 0.00963 -0.0882 0.3731 0.7672
8.500 1.2128 0.01642 0.01070 -0.0841 0.3393 0.7690
8.750 1.2049 0.01798 0.01209 -0.0796 0.2973 0.7708
9.000 1.1950 0.01987 0.01376 -0.0754 0.2553 0.7725
9.250 1.1858 0.02191 0.01558 -0.0716 0.2132 0.7744
9.500 1.1795 0.02393 0.01739 -0.0683 0.1751 0.7762
9.750 1.1775 0.02580 0.01910 -0.0658 0.1442 0.7780
10.000 1.1768 0.02769 0.02083 -0.0636 0.1148 0.7796
10.250 1.1780 0.02952 0.02254 -0.0617 0.0934 0.7812
10.500 1.1836 0.03114 0.02410 -0.0603 0.0806 0.7828
10.750 1.1898 0.03277 0.02569 -0.0590 0.0697 0.7841
11.000 1.1956 0.03443 0.02732 -0.0577 0.0567 0.7853
11.250 1.2013 0.03614 0.02898 -0.0565 0.0465 0.7865
11.500 1.2084 0.03781 0.03064 -0.0555 0.0412 0.7878
11.750 1.2154 0.03952 0.03235 -0.0545 0.0379 0.7891
12.000 1.2239 0.04117 0.03406 -0.0537 0.0360 0.7907
12.250 1.2327 0.04284 0.03578 -0.0530 0.0346 0.7924
12.500 1.2402 0.04468 0.03766 -0.0523 0.0334 0.7939
12.750 1.2452 0.04681 0.03983 -0.0516 0.0322 0.7954
13.000 1.2502 0.04901 0.04209 -0.0510 0.0314 0.7969
13.250 1.2586 0.05093 0.04409 -0.0506 0.0308 0.7983
13.500 1.2663 0.05298 0.04621 -0.0503 0.0301 0.7997
13.750 1.2737 0.05503 0.04833 -0.0500 0.0294 0.8011
14.000 1.2796 0.05728 0.05065 -0.0497 0.0287 0.8026
14.250 1.2853 0.05960 0.05304 -0.0495 0.0281 0.8041
14.500 1.2891 0.06219 0.05568 -0.0493 0.0276 0.8056
14.750 1.2913 0.06500 0.05855 -0.0491 0.0270 0.8073
15.000 1.2920 0.06799 0.06161 -0.0490 0.0265 0.8091
15.250 1.3003 0.07020 0.06391 -0.0491 0.0262 0.8112
15.500 1.3077 0.07258 0.06637 -0.0492 0.0259 0.8133
15.750 1.3153 0.07496 0.06882 -0.0495 0.0255 0.8151
16.000 1.3224 0.07737 0.07132 -0.0497 0.0251 0.8170
16.250 1.3292 0.07982 0.07386 -0.0500 0.0247 0.8189
16.500 1.3362 0.08227 0.07639 -0.0503 0.0242 0.8210
16.750 1.3425 0.08484 0.07904 -0.0507 0.0238 0.8233
17.000 1.3492 0.08737 0.08162 -0.0511 0.0234 0.8257
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