GOE 767 AIRFOIL (goe767-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 767 AIRFOIL (goe767-il) Reynolds number: 1,000,000 Max Cl/Cd: 93.08 at α=6.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe767-il-1000000.txt Download as CSV file: xf-goe767-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 767 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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.000 -1.0735 0.12774 0.12517 0.0099 1.0000 0.0243
-18.750 -1.1106 0.11618 0.11344 0.0025 1.0000 0.0244
-18.500 -1.1407 0.10638 0.10350 -0.0036 1.0000 0.0244
-18.250 -1.1680 0.09748 0.09447 -0.0091 1.0000 0.0245
-18.000 -1.1943 0.08893 0.08579 -0.0144 1.0000 0.0245
-17.750 -1.2189 0.08115 0.07788 -0.0192 1.0000 0.0245
-17.500 -1.2415 0.07377 0.07037 -0.0238 1.0000 0.0246
-17.250 -1.2613 0.06677 0.06325 -0.0283 1.0000 0.0246
-17.000 -1.2778 0.06032 0.05666 -0.0326 1.0000 0.0247
-16.750 -1.2899 0.05463 0.05084 -0.0365 1.0000 0.0247
-16.500 -1.2968 0.04982 0.04589 -0.0400 1.0000 0.0248
-16.250 -1.3117 0.04445 0.04037 -0.0431 1.0000 0.0249
-16.000 -1.3245 0.03987 0.03566 -0.0453 1.0000 0.0251
-15.750 -1.3319 0.03639 0.03209 -0.0464 1.0000 0.0253
-15.500 -1.3350 0.03377 0.02938 -0.0465 1.0000 0.0255
-15.250 -1.3353 0.03172 0.02725 -0.0458 1.0000 0.0256
-15.000 -1.3341 0.03004 0.02550 -0.0445 1.0000 0.0258
-14.750 -1.3310 0.02867 0.02407 -0.0428 1.0000 0.0260
-14.500 -1.3263 0.02754 0.02287 -0.0406 1.0000 0.0262
-14.250 -1.3213 0.02652 0.02178 -0.0381 1.0000 0.0264
-14.000 -1.3148 0.02566 0.02086 -0.0353 1.0000 0.0266
-13.750 -1.3051 0.02483 0.01997 -0.0329 1.0000 0.0268
-13.500 -1.2916 0.02402 0.01910 -0.0311 1.0000 0.0270
-13.250 -1.2765 0.02326 0.01827 -0.0294 1.0000 0.0273
-13.000 -1.2595 0.02258 0.01752 -0.0279 1.0000 0.0276
-12.750 -1.2416 0.02194 0.01682 -0.0265 1.0000 0.0279
-12.500 -1.2227 0.02133 0.01615 -0.0251 1.0000 0.0281
-12.250 -1.2032 0.02074 0.01550 -0.0238 1.0000 0.0283
-12.000 -1.1854 0.01995 0.01464 -0.0224 1.0000 0.0286
-11.750 -1.1699 0.01889 0.01353 -0.0206 1.0000 0.0290
-11.500 -1.1510 0.01814 0.01275 -0.0192 1.0000 0.0294
-11.250 -1.1304 0.01753 0.01211 -0.0180 1.0000 0.0298
-11.000 -1.1089 0.01699 0.01153 -0.0168 1.0000 0.0301
-10.750 -1.0868 0.01649 0.01100 -0.0158 1.0000 0.0305
-10.500 -1.0643 0.01603 0.01051 -0.0147 1.0000 0.0310
-10.250 -1.0414 0.01559 0.01003 -0.0137 1.0000 0.0314
-10.000 -1.0184 0.01516 0.00956 -0.0126 1.0000 0.0318
-9.750 -0.9951 0.01476 0.00912 -0.0116 1.0000 0.0321
-9.500 -0.9715 0.01438 0.00871 -0.0106 1.0000 0.0324
-9.250 -0.9504 0.01372 0.00802 -0.0093 1.0000 0.0331
-9.000 -0.9277 0.01324 0.00753 -0.0081 1.0000 0.0337
-8.750 -0.9043 0.01285 0.00712 -0.0071 1.0000 0.0344
-8.500 -0.8806 0.01249 0.00675 -0.0060 1.0000 0.0350
-8.250 -0.8567 0.01217 0.00641 -0.0050 1.0000 0.0357
-8.000 -0.8325 0.01187 0.00609 -0.0040 1.0000 0.0364
-7.750 -0.8089 0.01151 0.00572 -0.0029 1.0000 0.0373
-7.500 -0.7854 0.01114 0.00535 -0.0018 1.0000 0.0385
-7.250 -0.7616 0.01082 0.00504 -0.0007 1.0000 0.0399
-7.000 -0.7374 0.01055 0.00476 0.0004 1.0000 0.0412
-6.750 -0.7140 0.01021 0.00445 0.0015 1.0000 0.0438
-6.500 -0.6905 0.00990 0.00417 0.0027 1.0000 0.0475
-6.250 -0.6664 0.00953 0.00389 0.0036 0.9998 0.0567
-6.000 -0.6246 0.00921 0.00369 0.0009 0.9932 0.0723
-5.750 -0.5845 0.00901 0.00355 -0.0014 0.9800 0.0807
-5.500 -0.5296 0.00880 0.00339 -0.0068 0.9457 0.0872
-5.250 -0.4933 0.00890 0.00323 -0.0080 0.8519 0.0907
-5.000 -0.4734 0.00918 0.00305 -0.0058 0.7080 0.0935
-4.750 -0.4490 0.00931 0.00294 -0.0048 0.6288 0.0967
-4.500 -0.4226 0.00934 0.00283 -0.0042 0.5884 0.0995
-4.250 -0.3955 0.00936 0.00274 -0.0037 0.5581 0.1015
-4.000 -0.3687 0.00929 0.00259 -0.0032 0.5327 0.1048
-3.750 -0.3416 0.00922 0.00248 -0.0027 0.5112 0.1085
-3.500 -0.3141 0.00918 0.00239 -0.0023 0.4923 0.1117
-3.250 -0.2864 0.00916 0.00230 -0.0019 0.4753 0.1139
-3.000 -0.2593 0.00905 0.00217 -0.0014 0.4600 0.1187
-2.750 -0.2319 0.00899 0.00208 -0.0010 0.4455 0.1227
-2.500 -0.2042 0.00896 0.00200 -0.0006 0.4316 0.1264
-2.250 -0.1767 0.00887 0.00190 -0.0002 0.4195 0.1326
-2.000 -0.1492 0.00881 0.00184 0.0002 0.4077 0.1397
-1.750 -0.1217 0.00873 0.00177 0.0006 0.3959 0.1501
-1.500 -0.0941 0.00865 0.00171 0.0010 0.3847 0.1628
-1.250 -0.0668 0.00858 0.00165 0.0015 0.3729 0.1794
-1.000 -0.0393 0.00848 0.00159 0.0019 0.3627 0.1985
-0.750 -0.0122 0.00838 0.00154 0.0023 0.3525 0.2240
-0.500 0.0139 0.00813 0.00149 0.0028 0.3423 0.2870
-0.250 0.0403 0.00793 0.00147 0.0033 0.3327 0.3477
0.000 0.0666 0.00776 0.00144 0.0039 0.3220 0.4063
0.250 0.0927 0.00754 0.00143 0.0045 0.3118 0.4742
0.500 0.1181 0.00735 0.00143 0.0052 0.3000 0.5501
0.750 0.1432 0.00715 0.00145 0.0060 0.2885 0.6302
1.000 0.1687 0.00703 0.00149 0.0068 0.2778 0.6923
1.250 0.1942 0.00697 0.00153 0.0077 0.2680 0.7402
1.500 0.2200 0.00689 0.00158 0.0085 0.2609 0.7856
1.750 0.2450 0.00685 0.00165 0.0096 0.2525 0.8330
2.000 0.2707 0.00680 0.00173 0.0106 0.2471 0.8828
2.250 0.2989 0.00682 0.00183 0.0110 0.2419 0.9216
2.500 0.3319 0.00694 0.00194 0.0104 0.2360 0.9462
2.750 0.3680 0.00705 0.00205 0.0090 0.2320 0.9606
3.000 0.4067 0.00717 0.00215 0.0071 0.2275 0.9725
3.250 0.4432 0.00734 0.00227 0.0057 0.2228 0.9815
3.500 0.4841 0.00751 0.00239 0.0032 0.2175 0.9849
3.750 0.5216 0.00759 0.00247 0.0015 0.2148 0.9883
4.000 0.5576 0.00771 0.00256 0.0001 0.2108 0.9921
4.250 0.5986 0.00785 0.00266 -0.0025 0.2054 0.9953
4.500 0.6435 0.00797 0.00275 -0.0058 0.2007 0.9989
4.750 0.6763 0.00803 0.00282 -0.0066 0.1970 1.0000
5.000 0.7002 0.00814 0.00290 -0.0056 0.1927 1.0000
5.250 0.7238 0.00830 0.00302 -0.0046 0.1869 1.0000
5.500 0.7483 0.00837 0.00311 -0.0037 0.1829 1.0000
5.750 0.7724 0.00850 0.00321 -0.0027 0.1764 1.0000
6.000 0.7965 0.00866 0.00333 -0.0017 0.1695 1.0000
6.250 0.8204 0.00885 0.00346 -0.0008 0.1593 1.0000
6.500 0.8442 0.00907 0.00363 0.0002 0.1480 1.0000
6.750 0.8677 0.00933 0.00383 0.0012 0.1376 1.0000
7.000 0.8913 0.00960 0.00405 0.0021 0.1301 1.0000
7.250 0.9149 0.00988 0.00429 0.0031 0.1236 1.0000
7.500 0.9388 0.01014 0.00454 0.0040 0.1187 1.0000
7.750 0.9629 0.01038 0.00477 0.0049 0.1152 1.0000
8.000 0.9866 0.01068 0.00504 0.0058 0.1114 1.0000
8.250 1.0106 0.01095 0.00532 0.0067 0.1084 1.0000
8.500 1.0352 0.01116 0.00555 0.0074 0.1063 1.0000
8.750 1.0594 0.01141 0.00581 0.0082 0.1038 1.0000
9.000 1.0831 0.01173 0.00611 0.0091 0.1008 1.0000
9.250 1.1067 0.01205 0.00644 0.0099 0.0979 1.0000
9.500 1.1314 0.01225 0.00668 0.0106 0.0961 1.0000
9.750 1.1556 0.01251 0.00695 0.0114 0.0938 1.0000
10.000 1.1792 0.01283 0.00726 0.0122 0.0911 1.0000
10.250 1.2022 0.01321 0.00765 0.0130 0.0882 1.0000
10.500 1.2269 0.01342 0.00790 0.0137 0.0864 1.0000
10.750 1.2508 0.01371 0.00820 0.0144 0.0838 1.0000
11.000 1.2736 0.01410 0.00857 0.0152 0.0805 1.0000
11.250 1.2973 0.01440 0.00891 0.0159 0.0778 1.0000
11.500 1.3205 0.01474 0.00925 0.0166 0.0744 1.0000
11.750 1.3426 0.01517 0.00968 0.0175 0.0706 1.0000
12.000 1.3651 0.01556 0.01007 0.0183 0.0667 1.0000
12.250 1.3861 0.01606 0.01056 0.0192 0.0622 1.0000
12.500 1.4058 0.01666 0.01114 0.0203 0.0572 1.0000
12.750 1.4255 0.01724 0.01173 0.0213 0.0530 1.0000
13.000 1.4435 0.01791 0.01240 0.0226 0.0495 1.0000
13.250 1.4608 0.01861 0.01311 0.0238 0.0467 1.0000
13.500 1.4768 0.01935 0.01388 0.0252 0.0445 1.0000
13.750 1.4931 0.02002 0.01460 0.0266 0.0430 1.0000
14.000 1.5065 0.02083 0.01544 0.0283 0.0416 1.0000
14.250 1.5157 0.02182 0.01646 0.0303 0.0402 1.0000
14.500 1.5235 0.02258 0.01729 0.0328 0.0395 1.0000
14.750 1.5292 0.02344 0.01822 0.0354 0.0388 1.0000
15.000 1.5327 0.02453 0.01938 0.0376 0.0382 1.0000
15.250 1.5337 0.02598 0.02091 0.0394 0.0376 1.0000
15.500 1.5315 0.02803 0.02304 0.0402 0.0371 1.0000
15.750 1.5250 0.03120 0.02633 0.0392 0.0365 1.0000
16.000 1.5164 0.03586 0.03113 0.0360 0.0362 1.0000
16.250 1.4984 0.04220 0.03762 0.0316 0.0358 1.0000
16.500 1.4729 0.04920 0.04477 0.0276 0.0355 1.0000
16.750 1.4441 0.05634 0.05206 0.0239 0.0355 1.0000
17.000 1.4129 0.06367 0.05953 0.0203 0.0354 1.0000
17.250 1.3828 0.07087 0.06684 0.0169 0.0353 1.0000
17.500 1.3584 0.07740 0.07348 0.0138 0.0352 1.0000
17.750 1.3392 0.08344 0.07963 0.0110 0.0350 1.0000
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