GOE 342 AIRFOIL (goe342-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 342 AIRFOIL (goe342-il) Reynolds number: 200,000 Max Cl/Cd: 85.95 at α=4° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe342-il-200000-n5.txt Download as CSV file: xf-goe342-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 342 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
------ -------- --------- --------- -------- -------- --------
-9.000 -0.2780 0.11078 0.10724 -0.0317 1.0000 0.0193
-8.750 -0.2778 0.10891 0.10542 -0.0313 1.0000 0.0195
-8.500 -0.2798 0.10729 0.10387 -0.0305 0.9997 0.0196
-8.250 -0.2628 0.10387 0.10044 -0.0355 0.9942 0.0197
-8.000 -0.2455 0.10062 0.09719 -0.0413 0.9871 0.0198
-7.750 -0.2257 0.09733 0.09391 -0.0487 0.9779 0.0199
-7.500 -0.2127 0.09213 0.08870 -0.0466 0.9766 0.0204
-7.250 -0.1956 0.08869 0.08526 -0.0499 0.9690 0.0208
-7.000 -0.1766 0.08532 0.08188 -0.0539 0.9611 0.0214
-6.750 -0.1559 0.08191 0.07846 -0.0585 0.9535 0.0221
-6.500 -0.1324 0.07846 0.07499 -0.0640 0.9459 0.0234
-6.250 -0.0995 0.07543 0.07190 -0.0739 0.9353 0.0246
-6.000 -0.0606 0.07203 0.06841 -0.0856 0.9253 0.0249
-5.750 -0.0291 0.06806 0.06436 -0.0925 0.9185 0.0250
-5.500 -0.0085 0.06374 0.06001 -0.0956 0.9100 0.0252
-5.250 0.0025 0.06029 0.05657 -0.0942 0.9041 0.0257
-5.000 0.0212 0.05756 0.05381 -0.0955 0.8962 0.0266
-4.750 0.0489 0.05480 0.05098 -0.0994 0.8906 0.0289
-4.500 0.1040 0.05179 0.04776 -0.1112 0.8834 0.0322
-4.250 0.1476 0.04852 0.04429 -0.1184 0.8776 0.0325
-3.750 0.1986 0.04119 0.03682 -0.1238 0.8640 0.0339
-3.500 0.2254 0.03879 0.03434 -0.1258 0.8573 0.0350
-3.250 0.2563 0.03647 0.03190 -0.1285 0.8497 0.0365
-2.750 0.3444 0.03251 0.02725 -0.1370 0.8379 0.0433
-2.500 0.3721 0.02891 0.02359 -0.1394 0.8322 0.0443
-2.250 0.3998 0.02712 0.02172 -0.1407 0.8262 0.0456
-2.000 0.4300 0.02555 0.02003 -0.1421 0.8196 0.0476
-1.750 0.4492 0.00791 0.00224 -0.1355 0.8007 0.0552
-1.250 0.5263 0.02139 0.01524 -0.1459 0.8021 0.0630
-0.750 0.5941 0.01789 0.01099 -0.1473 0.7887 0.0416
-0.500 0.6239 0.01675 0.00963 -0.1476 0.7796 0.0401
-0.250 0.6534 0.01584 0.00846 -0.1477 0.7698 0.0392
0.000 0.6825 0.01510 0.00753 -0.1478 0.7616 0.0388
0.250 0.7114 0.01451 0.00676 -0.1478 0.7549 0.0388
0.500 0.7396 0.01416 0.00629 -0.1477 0.7477 0.0409
0.750 0.7678 0.01377 0.00579 -0.1475 0.7402 0.0414
1.000 0.7958 0.01338 0.00534 -0.1474 0.7328 0.0411
1.250 0.8235 0.01307 0.00499 -0.1473 0.7248 0.0409
1.500 0.8511 0.01280 0.00472 -0.1471 0.7162 0.0410
1.750 0.8786 0.01259 0.00449 -0.1469 0.7067 0.0412
2.000 0.9058 0.01242 0.00435 -0.1467 0.6947 0.0416
2.250 0.9327 0.01229 0.00425 -0.1463 0.6793 0.0423
2.500 0.9591 0.01222 0.00415 -0.1459 0.6592 0.0430
2.750 0.9853 0.01212 0.00402 -0.1455 0.6309 0.0459
3.000 1.0101 0.01220 0.00394 -0.1447 0.5830 0.0500
3.250 1.0321 0.01257 0.00395 -0.1434 0.5231 0.0517
3.500 1.0539 0.01309 0.00415 -0.1422 0.4749 0.0537
3.750 1.0762 0.01359 0.00444 -0.1412 0.4361 0.0591
4.000 1.0950 0.01274 0.00488 -0.1397 0.4098 1.0000
4.250 1.1188 0.01318 0.00518 -0.1390 0.3908 1.0000
4.500 1.1430 0.01358 0.00548 -0.1383 0.3774 1.0000
4.750 1.1670 0.01398 0.00581 -0.1377 0.3643 1.0000
5.000 1.1907 0.01440 0.00618 -0.1370 0.3517 1.0000
5.250 1.2141 0.01484 0.00655 -0.1363 0.3376 1.0000
5.500 1.2378 0.01524 0.00692 -0.1356 0.3246 1.0000
5.750 1.2619 0.01559 0.00731 -0.1350 0.3141 1.0000
6.000 1.2854 0.01599 0.00772 -0.1343 0.3035 1.0000
6.250 1.3085 0.01639 0.00813 -0.1336 0.2901 1.0000
6.500 1.3315 0.01679 0.00854 -0.1328 0.2759 1.0000
6.750 1.3546 0.01717 0.00899 -0.1320 0.2592 1.0000
7.000 1.3768 0.01761 0.00944 -0.1312 0.2354 1.0000
7.250 1.3948 0.01841 0.01001 -0.1298 0.1830 1.0000
7.500 1.4077 0.01978 0.01098 -0.1277 0.1328 1.0000
7.750 1.4240 0.02080 0.01190 -0.1261 0.1141 1.0000
8.000 1.4411 0.02168 0.01279 -0.1246 0.1014 1.0000
8.250 1.4597 0.02237 0.01354 -0.1232 0.0902 1.0000
8.500 1.4774 0.02311 0.01431 -0.1218 0.0791 1.0000
8.750 1.4940 0.02389 0.01511 -0.1202 0.0698 1.0000
9.000 1.5091 0.02477 0.01597 -0.1184 0.0602 1.0000
9.250 1.5228 0.02568 0.01692 -0.1164 0.0506 1.0000
9.500 1.5342 0.02662 0.01791 -0.1140 0.0408 1.0000
9.750 1.5430 0.02781 0.01907 -0.1113 0.0303 1.0000
10.000 1.5501 0.02916 0.02041 -0.1085 0.0234 1.0000
10.250 1.5573 0.03053 0.02186 -0.1059 0.0201 1.0000
10.500 1.5625 0.03211 0.02351 -0.1032 0.0179 1.0000
10.750 1.5665 0.03385 0.02539 -0.1005 0.0166 1.0000
11.000 1.5716 0.03551 0.02724 -0.0981 0.0158 1.0000
11.250 1.5753 0.03735 0.02925 -0.0957 0.0150 1.0000
11.500 1.5778 0.03936 0.03142 -0.0935 0.0143 1.0000
11.750 1.5793 0.04154 0.03375 -0.0914 0.0136 1.0000
12.000 1.5789 0.04397 0.03632 -0.0894 0.0130 1.0000
12.250 1.5749 0.04685 0.03935 -0.0875 0.0124 1.0000
12.500 1.5672 0.05027 0.04290 -0.0856 0.0119 1.0000
12.750 1.5670 0.05296 0.04577 -0.0843 0.0115 1.0000
13.000 1.5644 0.05601 0.04900 -0.0831 0.0113 1.0000
13.250 1.5606 0.05930 0.05250 -0.0821 0.0110 1.0000
13.500 1.5557 0.06280 0.05617 -0.0812 0.0108 1.0000
13.750 1.5500 0.06650 0.06005 -0.0806 0.0106 1.0000
14.000 1.5436 0.07044 0.06417 -0.0802 0.0104 1.0000
14.250 1.5367 0.07460 0.06851 -0.0801 0.0102 1.0000
14.500 1.5292 0.07901 0.07310 -0.0804 0.0100 1.0000
14.750 1.5213 0.08368 0.07794 -0.0810 0.0098 1.0000
15.000 1.5129 0.08861 0.08305 -0.0819 0.0097 1.0000
15.250 1.5040 0.09378 0.08840 -0.0832 0.0096 1.0000
15.500 1.4948 0.09921 0.09400 -0.0849 0.0095 1.0000
15.750 1.4854 0.10486 0.09982 -0.0869 0.0093 1.0000
16.000 1.4757 0.11073 0.10586 -0.0892 0.0092 1.0000
16.250 1.4659 0.11677 0.11207 -0.0919 0.0091 1.0000
16.500 1.4557 0.12300 0.11845 -0.0948 0.0090 1.0000
16.750 1.4455 0.12941 0.12502 -0.0981 0.0089 1.0000
17.000 1.4354 0.13598 0.13173 -0.1016 0.0088 1.0000
17.250 1.4249 0.14278 0.13868 -0.1054 0.0088 1.0000
17.500 1.4144 0.14980 0.14584 -0.1095 0.0087 1.0000
17.750 1.4033 0.15719 0.15338 -0.1141 0.0086 1.0000
18.000 1.3920 0.16500 0.16135 -0.1191 0.0086 1.0000
18.250 1.3792 0.17378 0.17031 -0.1249 0.0087 1.0000
18.500 1.3618 0.18483 0.18157 -0.1325 0.0088 1.0000
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