OAF128 AIRFOIL (oaf128-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: OAF128 AIRFOIL (oaf128-il) Reynolds number: 1,000,000 Max Cl/Cd: 85.24 at α=9° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-oaf128-il-1000000-n5.txt Download as CSV file: xf-oaf128-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: OAF128 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
------ -------- --------- --------- -------- -------- --------
-17.000 -1.3534 0.08695 0.08338 0.0175 1.0000 0.0137
-16.750 -1.3881 0.07786 0.07414 0.0127 1.0000 0.0136
-16.500 -1.4221 0.06900 0.06513 0.0080 1.0000 0.0136
-16.250 -1.4538 0.06053 0.05650 0.0033 1.0000 0.0136
-16.000 -1.4800 0.05278 0.04860 -0.0013 1.0000 0.0136
-15.750 -1.4992 0.04576 0.04142 -0.0059 1.0000 0.0137
-15.500 -1.5100 0.03971 0.03522 -0.0107 1.0000 0.0137
-15.250 -1.5160 0.03464 0.03000 -0.0151 1.0000 0.0138
-15.000 -1.5195 0.03118 0.02640 -0.0173 1.0000 0.0139
-14.750 -1.5087 0.02944 0.02457 -0.0175 1.0000 0.0141
-14.500 -1.4933 0.02806 0.02312 -0.0176 1.0000 0.0142
-14.250 -1.4754 0.02686 0.02186 -0.0176 1.0000 0.0144
-14.000 -1.4559 0.02580 0.02072 -0.0175 1.0000 0.0146
-13.750 -1.4350 0.02482 0.01968 -0.0175 1.0000 0.0148
-13.500 -1.4130 0.02391 0.01871 -0.0175 1.0000 0.0150
-13.250 -1.3901 0.02308 0.01781 -0.0176 1.0000 0.0152
-13.000 -1.3664 0.02230 0.01697 -0.0176 1.0000 0.0154
-12.750 -1.3419 0.02158 0.01619 -0.0177 1.0000 0.0156
-12.500 -1.3169 0.02090 0.01546 -0.0177 1.0000 0.0158
-12.250 -1.2916 0.02021 0.01471 -0.0179 1.0000 0.0160
-12.000 -1.2661 0.01946 0.01392 -0.0180 1.0000 0.0163
-11.750 -1.2399 0.01882 0.01325 -0.0182 1.0000 0.0167
-11.500 -1.2132 0.01824 0.01264 -0.0184 1.0000 0.0170
-11.250 -1.1861 0.01770 0.01207 -0.0185 1.0000 0.0173
-11.000 -1.1587 0.01720 0.01154 -0.0187 1.0000 0.0177
-10.750 -1.1310 0.01673 0.01103 -0.0189 1.0000 0.0181
-10.500 -1.1031 0.01628 0.01055 -0.0191 1.0000 0.0185
-10.250 -1.0749 0.01587 0.01010 -0.0193 1.0000 0.0188
-10.000 -1.0467 0.01537 0.00958 -0.0196 1.0000 0.0193
-9.750 -1.0182 0.01493 0.00913 -0.0199 1.0000 0.0199
-9.500 -0.9895 0.01453 0.00872 -0.0201 1.0000 0.0206
-9.250 -0.9606 0.01417 0.00834 -0.0204 1.0000 0.0213
-9.000 -0.9315 0.01383 0.00798 -0.0207 1.0000 0.0219
-8.750 -0.9024 0.01345 0.00759 -0.0210 1.0000 0.0226
-8.500 -0.8731 0.01308 0.00723 -0.0213 1.0000 0.0235
-8.250 -0.8436 0.01276 0.00690 -0.0216 1.0000 0.0245
-8.000 -0.8140 0.01247 0.00659 -0.0219 1.0000 0.0254
-7.750 -0.7876 0.01234 0.00639 -0.0214 0.9261 0.0266
-7.500 -0.7611 0.01216 0.00613 -0.0209 0.8960 0.0281
-7.250 -0.7333 0.01198 0.00587 -0.0207 0.8710 0.0297
-7.000 -0.7047 0.01175 0.00559 -0.0207 0.8477 0.0322
-6.750 -0.6758 0.01155 0.00532 -0.0208 0.8239 0.0349
-6.500 -0.6465 0.01135 0.00506 -0.0209 0.8006 0.0385
-6.250 -0.6170 0.01113 0.00479 -0.0212 0.7777 0.0439
-6.000 -0.5873 0.01087 0.00451 -0.0215 0.7537 0.0529
-5.750 -0.5574 0.01061 0.00425 -0.0218 0.7301 0.0653
-5.500 -0.5274 0.01041 0.00403 -0.0221 0.7069 0.0776
-5.250 -0.4974 0.01025 0.00384 -0.0225 0.6827 0.0875
-5.000 -0.4673 0.01011 0.00366 -0.0228 0.6603 0.0967
-4.750 -0.4372 0.00997 0.00350 -0.0231 0.6407 0.1055
-4.500 -0.4070 0.00986 0.00336 -0.0234 0.6225 0.1134
-4.250 -0.3768 0.00975 0.00321 -0.0237 0.6046 0.1219
-4.000 -0.3465 0.00962 0.00307 -0.0240 0.5880 0.1322
-3.750 -0.3162 0.00947 0.00295 -0.0244 0.5739 0.1475
-3.500 -0.2858 0.00927 0.00283 -0.0248 0.5612 0.1732
-3.250 -0.2555 0.00915 0.00274 -0.0252 0.5485 0.1920
-3.000 -0.2252 0.00909 0.00265 -0.0254 0.5335 0.2012
-2.750 -0.1949 0.00904 0.00257 -0.0257 0.5165 0.2092
-2.500 -0.1646 0.00900 0.00249 -0.0260 0.5018 0.2175
-2.250 -0.1343 0.00893 0.00243 -0.0263 0.4908 0.2286
-2.000 -0.1039 0.00887 0.00237 -0.0266 0.4775 0.2440
-1.750 -0.0736 0.00881 0.00232 -0.0269 0.4640 0.2611
-1.500 -0.0432 0.00876 0.00228 -0.0272 0.4536 0.2769
-1.250 -0.0129 0.00871 0.00226 -0.0275 0.4441 0.2897
-1.000 0.0174 0.00869 0.00223 -0.0277 0.4357 0.3019
-0.750 0.0477 0.00867 0.00222 -0.0280 0.4255 0.3154
-0.500 0.0780 0.00865 0.00221 -0.0283 0.4160 0.3281
-0.250 0.1083 0.00864 0.00221 -0.0285 0.4064 0.3414
0.000 0.1386 0.00862 0.00222 -0.0288 0.3986 0.3557
0.250 0.1688 0.00862 0.00223 -0.0290 0.3896 0.3704
0.500 0.1991 0.00863 0.00225 -0.0293 0.3807 0.3826
0.750 0.2293 0.00866 0.00227 -0.0295 0.3701 0.3924
1.000 0.2595 0.00867 0.00229 -0.0298 0.3620 0.4033
1.250 0.2897 0.00871 0.00233 -0.0300 0.3524 0.4138
1.500 0.3199 0.00877 0.00236 -0.0302 0.3391 0.4234
1.750 0.3501 0.00888 0.00242 -0.0305 0.3174 0.4336
2.250 0.4103 0.00909 0.00255 -0.0311 0.2807 0.4575
2.500 0.4404 0.00919 0.00262 -0.0314 0.2654 0.4693
2.750 0.4705 0.00931 0.00271 -0.0317 0.2494 0.4813
3.000 0.5005 0.00942 0.00281 -0.0320 0.2352 0.4954
3.250 0.5306 0.00951 0.00291 -0.0322 0.2242 0.5135
3.500 0.5606 0.00962 0.00303 -0.0325 0.2131 0.5342
3.750 0.5906 0.00972 0.00315 -0.0328 0.2034 0.5525
4.000 0.6205 0.00981 0.00327 -0.0331 0.1942 0.5714
4.250 0.6504 0.00995 0.00342 -0.0334 0.1816 0.5949
4.500 0.6803 0.01007 0.00357 -0.0337 0.1678 0.6252
4.750 0.7101 0.01022 0.00376 -0.0340 0.1506 0.6644
5.000 0.7397 0.01043 0.00398 -0.0343 0.1314 0.7057
5.250 0.7691 0.01063 0.00422 -0.0346 0.1169 0.7448
5.500 0.7982 0.01081 0.00446 -0.0348 0.1057 0.7844
5.750 0.8270 0.01097 0.00468 -0.0348 0.0972 0.8219
6.000 0.8552 0.01113 0.00490 -0.0347 0.0908 0.8570
6.250 0.8823 0.01125 0.00510 -0.0344 0.0857 0.8947
6.500 0.9056 0.01123 0.00519 -0.0331 0.0812 0.9884
6.750 0.9348 0.01146 0.00541 -0.0333 0.0773 1.0000
7.000 0.9640 0.01175 0.00566 -0.0335 0.0733 1.0000
7.250 0.9931 0.01198 0.00589 -0.0337 0.0705 1.0000
7.500 1.0221 0.01226 0.00614 -0.0339 0.0674 1.0000
7.750 1.0509 0.01255 0.00642 -0.0340 0.0647 1.0000
8.000 1.0797 0.01280 0.00667 -0.0342 0.0626 1.0000
8.250 1.1083 0.01310 0.00696 -0.0343 0.0600 1.0000
8.500 1.1367 0.01343 0.00727 -0.0344 0.0577 1.0000
8.750 1.1651 0.01370 0.00755 -0.0345 0.0561 1.0000
9.000 1.1934 0.01400 0.00786 -0.0346 0.0540 1.0000
9.250 1.2213 0.01435 0.00820 -0.0347 0.0521 1.0000
9.500 1.2491 0.01469 0.00855 -0.0347 0.0505 1.0000
9.750 1.2769 0.01501 0.00888 -0.0348 0.0489 1.0000
10.000 1.3043 0.01536 0.00924 -0.0348 0.0473 1.0000
10.250 1.3314 0.01577 0.00965 -0.0348 0.0457 1.0000
10.500 1.3585 0.01614 0.01004 -0.0348 0.0444 1.0000
10.750 1.3854 0.01651 0.01043 -0.0347 0.0430 1.0000
11.000 1.4119 0.01693 0.01086 -0.0347 0.0416 1.0000
11.250 1.4379 0.01740 0.01134 -0.0345 0.0402 1.0000
11.500 1.4639 0.01783 0.01179 -0.0344 0.0391 1.0000
11.750 1.4896 0.01827 0.01226 -0.0343 0.0379 1.0000
12.000 1.5148 0.01875 0.01276 -0.0341 0.0367 1.0000
12.250 1.5393 0.01931 0.01333 -0.0338 0.0354 1.0000
12.500 1.5636 0.01983 0.01388 -0.0335 0.0345 1.0000
12.750 1.5877 0.02035 0.01445 -0.0332 0.0335 1.0000
13.000 1.6110 0.02093 0.01505 -0.0328 0.0324 1.0000
13.250 1.6332 0.02158 0.01572 -0.0324 0.0313 1.0000
13.500 1.6549 0.02226 0.01644 -0.0319 0.0304 1.0000
13.750 1.6762 0.02290 0.01713 -0.0313 0.0296 1.0000
14.000 1.6964 0.02362 0.01788 -0.0306 0.0286 1.0000
14.250 1.7149 0.02443 0.01873 -0.0298 0.0277 1.0000
14.500 1.7311 0.02535 0.01969 -0.0288 0.0269 1.0000
14.750 1.7463 0.02625 0.02065 -0.0277 0.0263 1.0000
15.000 1.7590 0.02725 0.02172 -0.0264 0.0257 1.0000
15.250 1.7653 0.02850 0.02304 -0.0245 0.0251 1.0000
15.500 1.7671 0.03029 0.02492 -0.0232 0.0246 1.0000
15.750 1.7696 0.03250 0.02720 -0.0228 0.0240 1.0000
16.000 1.7711 0.03518 0.02997 -0.0231 0.0235 1.0000
16.250 1.7719 0.03817 0.03305 -0.0238 0.0231 1.0000
16.500 1.7723 0.04140 0.03640 -0.0249 0.0227 1.0000
16.750 1.7697 0.04511 0.04022 -0.0262 0.0224 1.0000
17.000 1.7638 0.04933 0.04454 -0.0278 0.0220 1.0000
17.250 1.7543 0.05404 0.04937 -0.0295 0.0217 1.0000
17.500 1.7413 0.05925 0.05470 -0.0315 0.0214 1.0000
17.750 1.7248 0.06494 0.06050 -0.0336 0.0212 1.0000
18.000 1.7050 0.07115 0.06684 -0.0360 0.0210 1.0000
18.250 1.6826 0.07777 0.07359 -0.0385 0.0209 1.0000
18.500 1.6600 0.08468 0.08062 -0.0414 0.0207 1.0000
18.750 1.6360 0.09200 0.08807 -0.0445 0.0205 1.0000
19.000 1.6120 0.09951 0.09570 -0.0479 0.0204 1.0000
19.250 1.5882 0.10713 0.10344 -0.0514 0.0202 1.0000
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