GOE 304 (FRIEDRICHSHAFEN G02) AIRFOIL (goe304-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 304 (FRIEDRICHSHAFEN G02) AIRFOIL (goe304-il) Reynolds number: 500,000 Max Cl/Cd: 109.66 at α=4.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe304-il-500000-n5.txt Download as CSV file: xf-goe304-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 304 (FRIEDRICHSHAFEN G02) 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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-8.500 -0.1384 0.09049 0.08797 -0.0623 0.9349 0.0236
-8.250 -0.1318 0.08716 0.08459 -0.0652 0.9176 0.0245
-8.000 -0.1249 0.08421 0.08160 -0.0671 0.9005 0.0245
-7.750 -0.1179 0.08129 0.07861 -0.0692 0.8837 0.0246
-7.500 -0.1085 0.07823 0.07550 -0.0723 0.8685 0.0246
-7.250 -0.0949 0.07479 0.07199 -0.0766 0.8550 0.0246
-7.000 -0.0814 0.07209 0.06923 -0.0778 0.8432 0.0248
-6.750 -0.0668 0.07009 0.06719 -0.0784 0.8313 0.0250
-6.500 -0.0500 0.06795 0.06500 -0.0803 0.8200 0.0255
-6.250 -0.0316 0.06552 0.06251 -0.0833 0.8092 0.0262
-6.000 -0.0079 0.06209 0.05900 -0.0890 0.7980 0.0279
-5.750 0.0205 0.05781 0.05460 -0.0968 0.7878 0.0282
-5.250 0.0746 0.05048 0.04706 -0.1071 0.7680 0.0282
-5.000 0.1041 0.04658 0.04301 -0.1122 0.7586 0.0283
-4.750 0.1266 0.04443 0.04080 -0.1136 0.7485 0.0281
-4.500 0.1470 0.04295 0.03927 -0.1141 0.7393 0.0276
-4.250 0.1753 0.04007 0.03628 -0.1172 0.7299 0.0270
-4.000 0.2059 0.03693 0.03298 -0.1207 0.7217 0.0267
-3.750 0.2370 0.03385 0.02973 -0.1237 0.7133 0.0266
-3.500 0.2679 0.03089 0.02657 -0.1263 0.7057 0.0267
-3.250 0.2996 0.02780 0.02326 -0.1285 0.6980 0.0273
-2.750 0.3621 0.02063 0.01540 -0.1318 0.6839 0.0276
-2.500 0.3928 0.01514 0.00908 -0.1329 0.6774 0.0286
-2.250 0.4203 0.01478 0.00862 -0.1329 0.6703 0.0289
-2.000 0.4480 0.01434 0.00807 -0.1329 0.6629 0.0294
-1.500 0.5039 0.01273 0.00605 -0.1328 0.6492 0.0305
-1.250 0.5317 0.01205 0.00517 -0.1327 0.6423 0.0311
-1.000 0.5595 0.01152 0.00448 -0.1326 0.6360 0.0318
-0.750 0.5873 0.01115 0.00399 -0.1324 0.6288 0.0324
-0.250 0.6426 0.01084 0.00364 -0.1322 0.6157 0.0337
0.000 0.6701 0.01073 0.00350 -0.1320 0.6085 0.0347
0.250 0.6976 0.01058 0.00330 -0.1318 0.6018 0.0356
0.500 0.7253 0.01042 0.00310 -0.1316 0.5944 0.0365
0.750 0.7523 0.01032 0.00296 -0.1314 0.5851 0.0373
1.000 0.7788 0.01030 0.00290 -0.1310 0.5698 0.0383
1.250 0.8051 0.01031 0.00285 -0.1306 0.5503 0.0395
1.500 0.8314 0.01036 0.00282 -0.1302 0.5332 0.0413
1.750 0.8580 0.01036 0.00279 -0.1299 0.5205 0.0430
2.000 0.8851 0.01037 0.00280 -0.1297 0.5099 0.0448
2.250 0.9118 0.01042 0.00282 -0.1294 0.4988 0.0469
2.500 0.9380 0.01049 0.00285 -0.1290 0.4850 0.0492
2.750 0.9639 0.01061 0.00292 -0.1286 0.4693 0.0526
3.000 0.9896 0.01074 0.00299 -0.1282 0.4530 0.0561
3.250 1.0154 0.01088 0.00309 -0.1278 0.4382 0.0604
3.500 1.0413 0.01100 0.00320 -0.1274 0.4252 0.0678
3.750 1.0671 0.01112 0.00336 -0.1270 0.4125 0.1050
4.250 1.1141 0.01016 0.00391 -0.1258 0.3814 1.0000
4.500 1.1389 0.01044 0.00409 -0.1252 0.3656 1.0000
4.750 1.1632 0.01074 0.00429 -0.1246 0.3487 1.0000
5.000 1.1870 0.01108 0.00453 -0.1239 0.3289 1.0000
5.250 1.2101 0.01147 0.00480 -0.1231 0.3074 1.0000
5.500 1.2329 0.01187 0.00508 -0.1223 0.2876 1.0000
5.750 1.2556 0.01227 0.00538 -0.1214 0.2692 1.0000
6.000 1.2781 0.01268 0.00570 -0.1206 0.2527 1.0000
6.250 1.3004 0.01308 0.00602 -0.1197 0.2384 1.0000
6.500 1.3223 0.01351 0.00638 -0.1187 0.2245 1.0000
6.750 1.3439 0.01393 0.00674 -0.1177 0.2114 1.0000
7.000 1.3659 0.01430 0.00708 -0.1168 0.2019 1.0000
7.250 1.3871 0.01472 0.00745 -0.1158 0.1927 1.0000
7.500 1.4085 0.01510 0.00782 -0.1148 0.1842 1.0000
7.750 1.4290 0.01552 0.00822 -0.1136 0.1764 1.0000
8.000 1.4497 0.01591 0.00860 -0.1125 0.1691 1.0000
8.250 1.4687 0.01637 0.00905 -0.1111 0.1615 1.0000
8.500 1.4866 0.01682 0.00948 -0.1095 0.1527 1.0000
8.750 1.5030 0.01732 0.00996 -0.1077 0.1438 1.0000
9.000 1.5183 0.01791 0.01050 -0.1058 0.1334 1.0000
9.250 1.5333 0.01851 0.01109 -0.1039 0.1225 1.0000
9.500 1.5472 0.01920 0.01173 -0.1019 0.1119 1.0000
9.750 1.5605 0.01993 0.01244 -0.0999 0.1038 1.0000
10.000 1.5731 0.02072 0.01320 -0.0979 0.0975 1.0000
10.250 1.5868 0.02146 0.01397 -0.0961 0.0936 1.0000
10.500 1.5997 0.02227 0.01480 -0.0942 0.0903 1.0000
10.750 1.6113 0.02318 0.01573 -0.0923 0.0871 1.0000
11.000 1.6235 0.02409 0.01668 -0.0906 0.0844 1.0000
11.250 1.6369 0.02493 0.01759 -0.0891 0.0825 1.0000
11.500 1.6489 0.02590 0.01861 -0.0875 0.0803 1.0000
11.750 1.6596 0.02700 0.01975 -0.0859 0.0780 1.0000
12.000 1.6687 0.02825 0.02104 -0.0842 0.0755 1.0000
12.250 1.6775 0.02956 0.02240 -0.0826 0.0733 1.0000
12.500 1.6904 0.03058 0.02352 -0.0814 0.0717 1.0000
12.750 1.7014 0.03177 0.02478 -0.0802 0.0692 1.0000
13.000 1.7102 0.03318 0.02624 -0.0789 0.0662 1.0000
13.250 1.7170 0.03479 0.02790 -0.0775 0.0632 1.0000
13.500 1.7266 0.03620 0.02938 -0.0764 0.0591 1.0000
13.750 1.7319 0.03802 0.03121 -0.0752 0.0523 1.0000
14.000 1.7320 0.04038 0.03351 -0.0738 0.0427 1.0000
14.250 1.7308 0.04295 0.03608 -0.0725 0.0372 1.0000
14.500 1.7302 0.04554 0.03872 -0.0714 0.0338 1.0000
14.750 1.7297 0.04819 0.04143 -0.0704 0.0315 1.0000
15.000 1.7285 0.05100 0.04432 -0.0696 0.0296 1.0000
15.250 1.7286 0.05376 0.04716 -0.0690 0.0280 1.0000
15.500 1.7267 0.05679 0.05027 -0.0684 0.0266 1.0000
16.000 1.7220 0.06318 0.05685 -0.0677 0.0243 1.0000
16.250 1.7194 0.06651 0.06028 -0.0675 0.0232 1.0000
16.500 1.7151 0.07012 0.06399 -0.0675 0.0223 1.0000
16.750 1.7087 0.07406 0.06802 -0.0676 0.0215 1.0000
17.000 1.7038 0.07791 0.07198 -0.0679 0.0208 1.0000
17.250 1.6989 0.08182 0.07600 -0.0683 0.0202 1.0000
17.500 1.6927 0.08597 0.08026 -0.0688 0.0195 1.0000
17.750 1.6850 0.09038 0.08478 -0.0695 0.0189 1.0000
18.000 1.6759 0.09509 0.08959 -0.0704 0.0184 1.0000
18.250 1.6656 0.10008 0.09468 -0.0715 0.0179 1.0000
18.500 1.6554 0.10510 0.09982 -0.0728 0.0175 1.0000
18.750 1.6466 0.10995 0.10479 -0.0742 0.0171 1.0000
19.000 1.6371 0.11499 0.10995 -0.0757 0.0167 1.0000
19.250 1.6270 0.12020 0.11528 -0.0775 0.0163 1.0000
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