NASA/LANGLEY RC-10(B)3 AIRFOIL (rc10b3-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: NASA/LANGLEY RC-10(B)3 AIRFOIL (rc10b3-il) Reynolds number: 500,000 Max Cl/Cd: 74.67 at α=3.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-rc10b3-il-500000.txt Download as CSV file: xf-rc10b3-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: NASA/LANGLEY RC-10(B)3 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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-9.500 -0.5641 0.08352 0.08127 -0.0273 1.0000 0.0241
-9.250 -0.5704 0.07817 0.07592 -0.0318 1.0000 0.0243
-9.000 -0.5775 0.07387 0.07159 -0.0337 1.0000 0.0244
-8.750 -0.5836 0.07027 0.06796 -0.0340 1.0000 0.0246
-8.500 -0.5842 0.06687 0.06452 -0.0343 1.0000 0.0248
-8.250 -0.5834 0.06350 0.06109 -0.0344 1.0000 0.0250
-8.000 -0.5822 0.06027 0.05780 -0.0339 1.0000 0.0254
-7.750 -0.5868 0.05751 0.05498 -0.0315 1.0000 0.0258
-7.250 -0.5752 0.04987 0.04701 -0.0304 0.9950 0.0280
-7.000 -0.5688 0.04066 0.03711 -0.0307 0.9884 0.0304
-6.750 -0.5434 0.03825 0.03464 -0.0322 0.9859 0.0309
-6.500 -0.5170 0.03598 0.03225 -0.0336 0.9835 0.0317
-6.250 -0.4946 0.03370 0.02979 -0.0337 0.9779 0.0329
-6.000 -0.4864 0.02225 0.01686 -0.0288 0.9715 0.0230
-5.750 -0.4640 0.01990 0.01419 -0.0277 0.9652 0.0226
-5.500 -0.4381 0.01810 0.01212 -0.0272 0.9600 0.0225
-5.250 -0.4124 0.01694 0.01075 -0.0266 0.9548 0.0228
-5.000 -0.3879 0.01611 0.00978 -0.0257 0.9482 0.0233
-4.750 -0.3630 0.01527 0.00879 -0.0249 0.9430 0.0236
-4.500 -0.3387 0.01456 0.00799 -0.0240 0.9364 0.0238
-4.250 -0.3164 0.01325 0.00661 -0.0227 0.9304 0.0245
-4.000 -0.2935 0.01261 0.00595 -0.0216 0.9245 0.0254
-3.750 -0.2698 0.01215 0.00547 -0.0206 0.9179 0.0264
-3.500 -0.2462 0.01175 0.00503 -0.0195 0.9126 0.0276
-3.250 -0.2216 0.01139 0.00464 -0.0187 0.9059 0.0290
-3.000 -0.1983 0.01090 0.00413 -0.0176 0.8998 0.0316
-2.750 -0.1736 0.01061 0.00382 -0.0169 0.8940 0.0348
-2.500 -0.1491 0.01023 0.00344 -0.0160 0.8871 0.0407
-2.250 -0.1251 0.00983 0.00310 -0.0150 0.8815 0.0614
-2.000 -0.1008 0.00944 0.00291 -0.0143 0.8741 0.1064
-1.750 -0.0774 0.00901 0.00272 -0.0134 0.8677 0.1762
-1.500 -0.0574 0.00825 0.00254 -0.0120 0.8603 0.3394
-1.250 -0.0501 0.00684 0.00229 -0.0079 0.8524 0.6531
-1.000 -0.0026 0.00651 0.00286 -0.0109 0.8474 0.9217
-0.750 0.0287 0.00689 0.00318 -0.0109 0.8398 0.9461
-0.500 0.0678 0.00720 0.00340 -0.0128 0.8338 0.9570
-0.250 0.1198 0.00755 0.00370 -0.0176 0.8268 0.9663
0.000 0.1753 0.00788 0.00394 -0.0231 0.8201 0.9785
0.250 0.2452 0.00801 0.00402 -0.0318 0.8114 0.9928
0.500 0.2904 0.00789 0.00384 -0.0356 0.8026 0.9972
0.750 0.3260 0.00779 0.00371 -0.0374 0.7922 0.9995
1.000 0.3545 0.00773 0.00360 -0.0376 0.7812 1.0000
1.250 0.3803 0.00768 0.00349 -0.0373 0.7679 1.0000
1.500 0.4061 0.00764 0.00340 -0.0369 0.7535 1.0000
1.750 0.4322 0.00761 0.00333 -0.0366 0.7400 1.0000
2.000 0.4582 0.00760 0.00327 -0.0363 0.7250 1.0000
2.250 0.4843 0.00759 0.00322 -0.0360 0.7082 1.0000
2.500 0.5103 0.00762 0.00318 -0.0357 0.6854 1.0000
2.750 0.5362 0.00767 0.00315 -0.0354 0.6597 1.0000
3.000 0.5620 0.00776 0.00314 -0.0350 0.6282 1.0000
3.250 0.5875 0.00795 0.00314 -0.0347 0.5821 1.0000
3.500 0.6127 0.00823 0.00319 -0.0343 0.5292 1.0000
3.750 0.6377 0.00854 0.00328 -0.0340 0.4758 1.0000
4.000 0.6624 0.00889 0.00341 -0.0337 0.4256 1.0000
4.250 0.6868 0.00925 0.00358 -0.0333 0.3776 1.0000
4.500 0.7108 0.00963 0.00376 -0.0329 0.3319 1.0000
4.750 0.7346 0.01000 0.00395 -0.0324 0.2905 1.0000
5.000 0.7580 0.01039 0.00418 -0.0319 0.2502 1.0000
5.250 0.7809 0.01084 0.00442 -0.0313 0.2096 1.0000
5.500 0.8034 0.01130 0.00470 -0.0306 0.1687 1.0000
5.750 0.8253 0.01180 0.00501 -0.0298 0.1322 1.0000
6.000 0.8462 0.01238 0.00540 -0.0289 0.0966 1.0000
6.250 0.8672 0.01291 0.00580 -0.0278 0.0749 1.0000
6.500 0.8882 0.01338 0.00622 -0.0267 0.0635 1.0000
6.750 0.9088 0.01386 0.00669 -0.0256 0.0568 1.0000
7.000 0.9293 0.01428 0.00713 -0.0244 0.0522 1.0000
7.250 0.9479 0.01490 0.00775 -0.0228 0.0480 1.0000
7.500 0.9682 0.01527 0.00818 -0.0215 0.0456 1.0000
7.750 0.9873 0.01572 0.00867 -0.0201 0.0433 1.0000
8.000 1.0040 0.01639 0.00934 -0.0183 0.0409 1.0000
8.250 1.0190 0.01717 0.01019 -0.0161 0.0390 1.0000
8.500 1.0375 0.01758 0.01066 -0.0146 0.0376 1.0000
8.750 1.0546 0.01808 0.01121 -0.0128 0.0361 1.0000
9.000 1.0707 0.01864 0.01181 -0.0109 0.0347 1.0000
9.250 1.0848 0.01933 0.01253 -0.0087 0.0335 1.0000
9.500 1.0916 0.02077 0.01402 -0.0053 0.0319 1.0000
9.750 1.1075 0.02121 0.01454 -0.0034 0.0312 1.0000
10.000 1.1220 0.02174 0.01516 -0.0012 0.0303 1.0000
10.250 1.1349 0.02240 0.01589 0.0012 0.0293 1.0000
10.500 1.1467 0.02308 0.01663 0.0037 0.0285 1.0000
10.750 1.1576 0.02377 0.01736 0.0063 0.0277 1.0000
11.000 1.1658 0.02451 0.01814 0.0093 0.0269 1.0000
11.250 1.1688 0.02584 0.01951 0.0130 0.0260 1.0000
11.500 1.1738 0.02707 0.02087 0.0163 0.0253 1.0000
11.750 1.1803 0.02776 0.02167 0.0193 0.0248 1.0000
12.000 1.1873 0.02867 0.02270 0.0221 0.0243 1.0000
12.250 1.1945 0.02970 0.02383 0.0245 0.0236 1.0000
12.500 1.2015 0.03078 0.02502 0.0268 0.0230 1.0000
12.750 1.2085 0.03185 0.02617 0.0288 0.0224 1.0000
13.000 1.2154 0.03296 0.02734 0.0306 0.0219 1.0000
13.250 1.2217 0.03426 0.02870 0.0322 0.0213 1.0000
13.500 1.2229 0.03658 0.03110 0.0340 0.0207 1.0000
13.750 1.2216 0.03898 0.03370 0.0357 0.0203 1.0000
14.000 1.2231 0.04084 0.03573 0.0370 0.0200 1.0000
14.250 1.2228 0.04305 0.03811 0.0380 0.0196 1.0000
14.500 1.2207 0.04556 0.04079 0.0388 0.0193 1.0000
14.750 1.2172 0.04836 0.04376 0.0392 0.0189 1.0000
15.000 1.2122 0.05145 0.04701 0.0393 0.0186 1.0000
15.250 1.2066 0.05476 0.05046 0.0390 0.0183 1.0000
15.500 1.1992 0.05848 0.05434 0.0382 0.0181 1.0000
15.750 1.1905 0.06255 0.05855 0.0369 0.0178 1.0000
16.000 1.1814 0.06699 0.06312 0.0352 0.0176 1.0000
16.250 1.1716 0.07181 0.06807 0.0330 0.0174 1.0000
16.500 1.1593 0.07728 0.07368 0.0303 0.0173 1.0000
16.750 1.1440 0.08363 0.08017 0.0269 0.0172 1.0000
17.000 1.1247 0.09103 0.08774 0.0228 0.0171 1.0000
17.250 1.0845 0.10312 0.10010 0.0158 0.0173 1.0000
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