NACA 63-206 (naca63206-il) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 63-206 (naca63206-il) Reynolds number: 100,000 Max Cl/Cd: 41.48 at α=2.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca63206-il-100000-n5.txt Download as CSV file: xf-naca63206-il-100000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NACA 63-206
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.100 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-8.000 -0.5597 0.08871 0.08401 -0.0080 1.0000 0.0354
-7.750 -0.5586 0.08484 0.08019 -0.0103 1.0000 0.0358
-7.500 -0.5560 0.08036 0.07576 -0.0142 1.0000 0.0363
-7.250 -0.5507 0.07559 0.07099 -0.0188 1.0000 0.0365
-7.000 -0.5439 0.07080 0.06616 -0.0228 1.0000 0.0370
-6.750 -0.5350 0.06589 0.06117 -0.0266 1.0000 0.0369
-6.500 -0.5235 0.06033 0.05542 -0.0307 1.0000 0.0354
-6.000 -0.4851 0.04969 0.04412 -0.0340 1.0000 0.0193
-5.750 -0.4697 0.04500 0.03907 -0.0351 1.0000 0.0188
-5.500 -0.4512 0.04074 0.03447 -0.0359 1.0000 0.0185
-5.250 -0.4303 0.03676 0.03010 -0.0364 1.0000 0.0183
-5.000 -0.4077 0.03314 0.02602 -0.0365 1.0000 0.0183
-4.750 -0.3820 0.03093 0.02327 -0.0360 1.0000 0.0197
-4.500 -0.3602 0.02698 0.01892 -0.0364 1.0000 0.0222
-4.250 -0.3353 0.02454 0.01610 -0.0360 1.0000 0.0234
-4.000 -0.3097 0.02228 0.01345 -0.0353 1.0000 0.0244
-3.750 -0.2843 0.02033 0.01121 -0.0344 1.0000 0.0259
-3.500 -0.2594 0.01894 0.00959 -0.0335 1.0000 0.0299
-3.250 -0.2353 0.01757 0.00807 -0.0326 1.0000 0.0339
-3.000 -0.2121 0.01619 0.00660 -0.0318 1.0000 0.0366
-2.750 -0.1882 0.01526 0.00557 -0.0311 1.0000 0.0407
-2.500 -0.1638 0.01448 0.00463 -0.0305 1.0000 0.0476
-2.250 -0.1394 0.01371 0.00394 -0.0301 1.0000 0.0749
-2.000 -0.1190 0.01120 0.00345 -0.0299 1.0000 0.5408
-1.750 -0.1124 0.01053 0.00371 -0.0240 1.0000 0.7934
-1.500 -0.0876 0.01013 0.00356 -0.0210 1.0000 0.9782
-1.250 -0.0606 0.01007 0.00322 -0.0216 1.0000 1.0000
-1.000 -0.0375 0.01010 0.00305 -0.0214 1.0000 1.0000
-0.750 -0.0141 0.01016 0.00295 -0.0212 1.0000 1.0000
-0.500 0.0205 0.01026 0.00291 -0.0232 0.9934 1.0000
-0.250 0.0599 0.01037 0.00288 -0.0261 0.9839 1.0000
0.000 0.0990 0.01047 0.00290 -0.0288 0.9746 1.0000
0.250 0.1387 0.01057 0.00295 -0.0316 0.9657 1.0000
0.500 0.1772 0.01065 0.00302 -0.0341 0.9558 1.0000
0.750 0.2139 0.01073 0.00313 -0.0361 0.9447 1.0000
1.000 0.2501 0.01081 0.00324 -0.0380 0.9332 1.0000
1.250 0.2853 0.01088 0.00338 -0.0396 0.9211 1.0000
1.500 0.3192 0.01096 0.00355 -0.0408 0.9082 1.0000
1.750 0.3519 0.01105 0.00380 -0.0417 0.8944 1.0000
2.000 0.3835 0.01113 0.00402 -0.0423 0.8793 1.0000
2.250 0.4142 0.01121 0.00424 -0.0425 0.8621 1.0000
2.500 0.4421 0.01128 0.00447 -0.0420 0.8389 1.0000
2.750 0.4629 0.01116 0.00418 -0.0383 0.7544 1.0000
3.000 0.4792 0.01163 0.00398 -0.0341 0.5725 1.0000
3.250 0.4893 0.01427 0.00444 -0.0315 0.1434 1.0000
3.500 0.5114 0.01573 0.00543 -0.0308 0.0564 1.0000
3.750 0.5357 0.01672 0.00652 -0.0302 0.0460 1.0000
4.000 0.5597 0.01773 0.00771 -0.0294 0.0413 1.0000
4.250 0.5815 0.01929 0.00928 -0.0285 0.0366 1.0000
4.500 0.6067 0.02026 0.01046 -0.0279 0.0307 1.0000
4.750 0.6313 0.02196 0.01237 -0.0270 0.0280 1.0000
5.000 0.6565 0.02410 0.01465 -0.0263 0.0260 1.0000
5.250 0.6812 0.02718 0.01801 -0.0256 0.0237 1.0000
5.500 0.7071 0.02896 0.02032 -0.0247 0.0204 1.0000
5.750 0.7310 0.03211 0.02401 -0.0236 0.0195 1.0000
6.000 0.7527 0.03567 0.02814 -0.0224 0.0191 1.0000
6.250 0.7719 0.03963 0.03264 -0.0213 0.0189 1.0000
6.500 0.7886 0.04394 0.03747 -0.0203 0.0190 1.0000
6.750 0.8025 0.04847 0.04245 -0.0195 0.0190 1.0000
7.000 0.8139 0.05298 0.04736 -0.0190 0.0184 1.0000
7.250 0.8227 0.05743 0.05214 -0.0188 0.0175 1.0000
7.500 0.8284 0.06194 0.05692 -0.0190 0.0167 1.0000
7.750 0.8310 0.06646 0.06165 -0.0195 0.0161 1.0000
8.000 0.8293 0.07144 0.06682 -0.0206 0.0161 1.0000
8.250 0.8231 0.07688 0.07240 -0.0225 0.0165 1.0000
8.500 0.8120 0.08231 0.07789 -0.0250 0.0174 1.0000
8.750 0.8020 0.08865 0.08424 -0.0302 0.0183 1.0000
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Polar data table (+)
Polar graphs
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