GOE 738 AIRFOIL (goe738-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 738 AIRFOIL (goe738-il) Reynolds number: 1,000,000 Max Cl/Cd: 93.59 at α=7.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe738-il-1000000-n5.txt Download as CSV file: xf-goe738-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 738 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.500 -1.2043 0.09380 0.09057 -0.0190 1.0000 0.0238
-19.250 -1.2434 0.08376 0.08038 -0.0251 1.0000 0.0239
-19.000 -1.2812 0.07413 0.07058 -0.0309 1.0000 0.0240
-18.750 -1.3126 0.06573 0.06202 -0.0360 1.0000 0.0240
-18.500 -1.3366 0.05860 0.05473 -0.0402 1.0000 0.0240
-18.250 -1.3515 0.05309 0.04911 -0.0433 1.0000 0.0243
-18.000 -1.3637 0.04820 0.04410 -0.0459 1.0000 0.0244
-17.750 -1.3722 0.04409 0.03988 -0.0478 1.0000 0.0245
-17.500 -1.3753 0.04086 0.03656 -0.0490 1.0000 0.0247
-17.250 -1.3785 0.03785 0.03345 -0.0498 1.0000 0.0249
-17.000 -1.3782 0.03542 0.03093 -0.0500 1.0000 0.0251
-16.750 -1.3764 0.03329 0.02872 -0.0499 1.0000 0.0252
-16.500 -1.3724 0.03151 0.02687 -0.0494 1.0000 0.0255
-16.250 -1.3671 0.02994 0.02523 -0.0487 1.0000 0.0258
-16.000 -1.3625 0.02844 0.02365 -0.0477 1.0000 0.0259
-15.750 -1.3559 0.02717 0.02231 -0.0464 1.0000 0.0261
-15.500 -1.3487 0.02603 0.02110 -0.0450 1.0000 0.0263
-15.250 -1.3399 0.02505 0.02006 -0.0435 1.0000 0.0264
-14.750 -1.3262 0.02317 0.01806 -0.0392 0.9922 0.0269
-14.500 -1.3025 0.02241 0.01701 -0.0400 0.8591 0.0273
-14.250 -1.2946 0.02181 0.01628 -0.0373 0.8299 0.0275
-14.000 -1.2845 0.02124 0.01560 -0.0349 0.8112 0.0279
-13.750 -1.2730 0.02071 0.01499 -0.0325 0.7973 0.0281
-13.500 -1.2608 0.02020 0.01440 -0.0301 0.7850 0.0284
-13.250 -1.2473 0.01974 0.01387 -0.0278 0.7752 0.0287
-12.750 -1.2156 0.01890 0.01289 -0.0240 0.7573 0.0294
-12.500 -1.1971 0.01848 0.01239 -0.0225 0.7491 0.0297
-12.250 -1.1776 0.01807 0.01192 -0.0211 0.7420 0.0300
-12.000 -1.1573 0.01767 0.01146 -0.0199 0.7346 0.0303
-11.750 -1.1365 0.01731 0.01101 -0.0187 0.7279 0.0305
-11.500 -1.1158 0.01687 0.01053 -0.0175 0.7214 0.0309
-11.250 -1.0948 0.01645 0.01007 -0.0164 0.7145 0.0314
-11.000 -1.0728 0.01607 0.00965 -0.0153 0.7085 0.0320
-10.750 -1.0501 0.01571 0.00926 -0.0144 0.7026 0.0325
-10.500 -1.0270 0.01539 0.00889 -0.0135 0.6959 0.0330
-10.250 -1.0035 0.01507 0.00852 -0.0127 0.6903 0.0335
-10.000 -0.9795 0.01477 0.00818 -0.0119 0.6844 0.0340
-9.750 -0.9553 0.01448 0.00785 -0.0112 0.6780 0.0345
-9.500 -0.9308 0.01422 0.00753 -0.0105 0.6722 0.0349
-9.250 -0.9065 0.01389 0.00717 -0.0097 0.6666 0.0357
-9.000 -0.8819 0.01359 0.00685 -0.0091 0.6606 0.0365
-8.500 -0.8315 0.01308 0.00629 -0.0079 0.6493 0.0383
-8.250 -0.8058 0.01285 0.00603 -0.0073 0.6431 0.0392
-8.000 -0.7801 0.01263 0.00576 -0.0068 0.6374 0.0401
-7.750 -0.7544 0.01238 0.00550 -0.0062 0.6324 0.0413
-7.500 -0.7285 0.01215 0.00526 -0.0057 0.6262 0.0427
-7.250 -0.7023 0.01195 0.00503 -0.0053 0.6197 0.0440
-7.000 -0.6757 0.01177 0.00481 -0.0048 0.6142 0.0452
-6.750 -0.6495 0.01155 0.00459 -0.0044 0.6085 0.0469
-6.500 -0.6230 0.01136 0.00438 -0.0040 0.6024 0.0488
-6.250 -0.5962 0.01119 0.00419 -0.0036 0.5967 0.0505
-6.000 -0.5694 0.01102 0.00400 -0.0032 0.5904 0.0524
-5.750 -0.5427 0.01084 0.00382 -0.0028 0.5838 0.0550
-5.500 -0.5156 0.01069 0.00365 -0.0025 0.5786 0.0573
-5.250 -0.4885 0.01053 0.00349 -0.0021 0.5729 0.0596
-5.000 -0.4616 0.01038 0.00333 -0.0018 0.5667 0.0624
-4.750 -0.4342 0.01025 0.00318 -0.0015 0.5611 0.0650
-4.500 -0.4070 0.01010 0.00303 -0.0012 0.5548 0.0681
-4.250 -0.3798 0.00997 0.00289 -0.0009 0.5485 0.0719
-4.000 -0.3523 0.00984 0.00276 -0.0006 0.5433 0.0755
-3.750 -0.3251 0.00969 0.00263 -0.0003 0.5380 0.0811
-3.500 -0.2978 0.00955 0.00250 0.0000 0.5323 0.0875
-3.250 -0.2708 0.00939 0.00237 0.0003 0.5269 0.0983
-3.000 -0.2440 0.00920 0.00226 0.0006 0.5203 0.1170
-2.750 -0.2169 0.00909 0.00217 0.0009 0.5112 0.1327
-2.500 -0.1895 0.00897 0.00209 0.0012 0.5039 0.1450
-2.250 -0.1618 0.00887 0.00201 0.0014 0.4976 0.1549
-2.000 -0.1339 0.00882 0.00195 0.0016 0.4924 0.1628
-1.750 -0.1062 0.00871 0.00189 0.0018 0.4875 0.1734
-1.500 -0.0783 0.00864 0.00183 0.0020 0.4808 0.1835
-1.250 -0.0507 0.00858 0.00178 0.0022 0.4743 0.1954
-1.000 -0.0231 0.00847 0.00173 0.0024 0.4690 0.2131
-0.750 0.0043 0.00838 0.00169 0.0026 0.4625 0.2331
-0.500 0.0313 0.00827 0.00165 0.0029 0.4556 0.2600
-0.250 0.0583 0.00813 0.00162 0.0032 0.4488 0.2929
0.000 0.0850 0.00800 0.00159 0.0036 0.4415 0.3293
0.250 0.1117 0.00785 0.00156 0.0039 0.4357 0.3697
0.500 0.1379 0.00767 0.00154 0.0043 0.4304 0.4201
0.750 0.1635 0.00748 0.00153 0.0048 0.4251 0.4808
1.000 0.1898 0.00735 0.00154 0.0053 0.4205 0.5282
1.250 0.2167 0.00725 0.00155 0.0056 0.4156 0.5647
1.500 0.2436 0.00720 0.00157 0.0060 0.4101 0.5945
1.750 0.2706 0.00717 0.00160 0.0063 0.4047 0.6218
2.000 0.2976 0.00712 0.00164 0.0066 0.3998 0.6490
2.250 0.3246 0.00709 0.00168 0.0070 0.3938 0.6765
2.500 0.3507 0.00708 0.00173 0.0075 0.3875 0.7082
2.750 0.3774 0.00706 0.00179 0.0079 0.3802 0.7352
3.000 0.4030 0.00708 0.00186 0.0085 0.3703 0.7667
3.250 0.4285 0.00707 0.00194 0.0091 0.3597 0.8003
3.500 0.4538 0.00707 0.00203 0.0098 0.3500 0.8344
3.750 0.4796 0.00709 0.00214 0.0105 0.3387 0.8742
4.000 0.5103 0.00720 0.00229 0.0100 0.3205 0.9095
4.250 0.5472 0.00750 0.00250 0.0080 0.2921 0.9307
4.500 0.5855 0.00779 0.00271 0.0057 0.2728 0.9425
4.750 0.6214 0.00808 0.00291 0.0038 0.2551 0.9514
5.000 0.6576 0.00835 0.00311 0.0020 0.2417 0.9568
5.250 0.6916 0.00855 0.00328 0.0007 0.2339 0.9621
5.750 0.7532 0.00899 0.00364 -0.0007 0.2200 0.9720
6.000 0.7844 0.00919 0.00382 -0.0014 0.2143 0.9761
6.250 0.8117 0.00942 0.00402 -0.0014 0.2086 0.9812
6.500 0.8456 0.00961 0.00420 -0.0028 0.2035 0.9830
6.750 0.8788 0.00980 0.00437 -0.0040 0.1986 0.9852
7.000 0.9108 0.01004 0.00458 -0.0050 0.1931 0.9877
7.250 0.9422 0.01025 0.00478 -0.0059 0.1886 0.9904
7.500 0.9730 0.01047 0.00499 -0.0066 0.1828 0.9929
7.750 1.0070 0.01076 0.00523 -0.0082 0.1733 0.9947
8.000 1.0395 0.01114 0.00552 -0.0096 0.1571 0.9967
8.250 1.0696 0.01172 0.00595 -0.0108 0.1339 0.9985
8.500 1.0998 0.01225 0.00638 -0.0119 0.1191 0.9999
8.750 1.1192 0.01270 0.00678 -0.0107 0.1101 1.0000
9.000 1.1383 0.01306 0.00713 -0.0093 0.1042 1.0000
9.250 1.1556 0.01350 0.00753 -0.0078 0.0980 1.0000
9.500 1.1737 0.01387 0.00790 -0.0063 0.0920 1.0000
9.750 1.1889 0.01438 0.00836 -0.0045 0.0838 1.0000
10.000 1.2017 0.01496 0.00889 -0.0023 0.0743 1.0000
10.250 1.2138 0.01554 0.00943 -0.0001 0.0680 1.0000
10.500 1.2263 0.01606 0.00994 0.0021 0.0648 1.0000
10.750 1.2327 0.01661 0.01050 0.0052 0.0624 1.0000
11.000 1.2348 0.01727 0.01118 0.0087 0.0605 1.0000
11.250 1.2429 0.01801 0.01196 0.0108 0.0595 1.0000
11.500 1.2529 0.01886 0.01284 0.0122 0.0584 1.0000
11.750 1.2636 0.01979 0.01380 0.0134 0.0573 1.0000
12.000 1.2732 0.02090 0.01493 0.0145 0.0558 1.0000
12.250 1.2830 0.02206 0.01612 0.0154 0.0546 1.0000
12.500 1.2925 0.02330 0.01738 0.0162 0.0531 1.0000
12.750 1.3041 0.02442 0.01854 0.0168 0.0527 1.0000
13.000 1.3155 0.02559 0.01976 0.0174 0.0520 1.0000
13.250 1.3256 0.02689 0.02110 0.0179 0.0511 1.0000
13.500 1.3350 0.02827 0.02252 0.0184 0.0505 1.0000
13.750 1.3431 0.02979 0.02408 0.0188 0.0496 1.0000
14.000 1.3497 0.03147 0.02580 0.0192 0.0488 1.0000
14.250 1.3569 0.03312 0.02750 0.0196 0.0484 1.0000
14.500 1.3617 0.03503 0.02944 0.0198 0.0475 1.0000
14.750 1.3648 0.03712 0.03158 0.0201 0.0466 1.0000
15.000 1.3728 0.03878 0.03330 0.0202 0.0460 1.0000
15.250 1.3778 0.04077 0.03535 0.0203 0.0459 1.0000
15.500 1.3838 0.04271 0.03735 0.0203 0.0455 1.0000
15.750 1.3885 0.04486 0.03955 0.0202 0.0451 1.0000
16.000 1.3928 0.04709 0.04184 0.0200 0.0443 1.0000
16.250 1.3966 0.04939 0.04420 0.0198 0.0440 1.0000
16.500 1.3990 0.05189 0.04676 0.0194 0.0433 1.0000
16.750 1.4001 0.05459 0.04950 0.0190 0.0425 1.0000
17.000 1.4007 0.05736 0.05232 0.0186 0.0417 1.0000
17.250 1.3998 0.06036 0.05537 0.0180 0.0410 1.0000
17.500 1.3991 0.06339 0.05847 0.0173 0.0406 1.0000
17.750 1.4018 0.06602 0.06116 0.0168 0.0401 1.0000
18.000 1.4022 0.06895 0.06416 0.0161 0.0394 1.0000
18.250 1.4016 0.07206 0.06733 0.0153 0.0390 1.0000
18.500 1.4011 0.07516 0.07049 0.0145 0.0380 1.0000
18.750 1.3978 0.07869 0.07409 0.0135 0.0373 1.0000
19.000 1.3935 0.08236 0.07781 0.0124 0.0363 1.0000
19.250 1.3883 0.08620 0.08170 0.0112 0.0356 1.0000
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