PROPFAN CRUISE MISSILE WING AIRFOIL (pfcm-il) Xfoil prediction polar at RE=50,000 Ncrit=9
| Details | Polar file |
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Airfoil: PROPFAN CRUISE MISSILE WING AIRFOIL (pfcm-il) Reynolds number: 50,000 Max Cl/Cd: 30.65 at α=4.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-pfcm-il-50000.txt Download as CSV file: xf-pfcm-il-50000.csv |
XFOIL Version 6.96
Calculated polar for: PROPFAN CRUISE MISSILE WING AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.050 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-8.750 -0.5492 0.10760 0.10077 0.0051 1.0000 0.2671
-8.500 -0.5488 0.10455 0.09778 0.0050 1.0000 0.2832
-8.250 -0.5556 0.10210 0.09542 0.0045 1.0000 0.2992
-8.000 -0.5343 0.09744 0.09074 0.0067 1.0000 0.3212
-7.750 -0.5484 0.09579 0.08921 0.0065 1.0000 0.3414
-7.500 -0.5189 0.09120 0.08457 0.0102 1.0000 0.3783
-7.250 -0.5192 0.08890 0.08234 0.0122 1.0000 0.4098
-6.750 -0.4858 0.08154 0.07499 0.0163 1.0000 0.4728
-6.500 -0.4751 0.07843 0.07191 0.0182 1.0000 0.5037
-5.500 -0.4898 0.04579 0.03768 -0.0377 1.0000 0.1585
-5.250 -0.4667 0.04122 0.03252 -0.0379 1.0000 0.1386
-5.000 -0.4428 0.03758 0.02824 -0.0375 1.0000 0.1263
-4.750 -0.4175 0.03469 0.02450 -0.0366 1.0000 0.1183
-4.500 -0.3934 0.03185 0.02133 -0.0357 1.0000 0.1159
-4.250 -0.3684 0.02954 0.01861 -0.0346 1.0000 0.1164
-4.000 -0.3440 0.02749 0.01627 -0.0337 1.0000 0.1226
-3.750 -0.3188 0.02566 0.01425 -0.0325 1.0000 0.1285
-3.500 -0.2930 0.02399 0.01242 -0.0310 1.0000 0.1351
-3.250 -0.2687 0.02243 0.01093 -0.0297 1.0000 0.1517
-3.000 -0.1261 0.01792 0.00920 -0.0361 1.0000 1.0000
-2.750 -0.1185 0.01745 0.00853 -0.0342 1.0000 1.0000
-2.500 -0.1155 0.01704 0.00798 -0.0316 1.0000 1.0000
-2.250 -0.1162 0.01668 0.00751 -0.0281 1.0000 1.0000
-2.000 -0.1174 0.01640 0.00710 -0.0245 1.0000 1.0000
-1.750 -0.1120 0.01624 0.00674 -0.0218 1.0000 1.0000
-1.500 -0.0985 0.01619 0.00645 -0.0203 1.0000 1.0000
-1.250 -0.0809 0.01622 0.00620 -0.0194 1.0000 1.0000
-1.000 -0.0614 0.01632 0.00607 -0.0189 1.0000 1.0000
-0.750 -0.0409 0.01646 0.00601 -0.0184 1.0000 1.0000
-0.500 -0.0199 0.01664 0.00603 -0.0181 1.0000 1.0000
-0.250 0.0015 0.01686 0.00610 -0.0178 1.0000 1.0000
0.000 0.0229 0.01712 0.00622 -0.0176 1.0000 1.0000
0.250 0.0445 0.01742 0.00642 -0.0175 1.0000 1.0000
0.500 0.0660 0.01776 0.00668 -0.0174 1.0000 1.0000
0.750 0.0874 0.01814 0.00700 -0.0173 1.0000 1.0000
1.000 0.1087 0.01856 0.00738 -0.0173 1.0000 1.0000
1.250 0.1299 0.01903 0.00783 -0.0173 1.0000 1.0000
1.500 0.1509 0.01954 0.00833 -0.0174 1.0000 1.0000
1.750 0.1717 0.02009 0.00890 -0.0175 1.0000 1.0000
2.000 0.1923 0.02069 0.00953 -0.0177 1.0000 1.0000
2.250 0.2127 0.02134 0.01023 -0.0179 1.0000 1.0000
2.500 0.2329 0.02204 0.01103 -0.0181 1.0000 1.0000
2.750 0.2528 0.02279 0.01187 -0.0184 1.0000 1.0000
3.000 0.2724 0.02360 0.01278 -0.0187 1.0000 1.0000
3.250 0.2918 0.02447 0.01377 -0.0190 1.0000 1.0000
3.500 0.3107 0.02540 0.01485 -0.0194 1.0000 1.0000
3.750 0.3590 0.02672 0.01652 -0.0255 0.9859 1.0000
4.000 0.4160 0.02808 0.01829 -0.0327 0.9647 1.0000
4.250 0.4792 0.02917 0.01992 -0.0402 0.9356 1.0000
4.500 0.6225 0.02031 0.01013 -0.0291 0.2975 1.0000
4.750 0.6314 0.02401 0.01242 -0.0264 0.1759 1.0000
5.000 0.6551 0.02615 0.01444 -0.0250 0.1450 1.0000
5.250 0.6853 0.02843 0.01647 -0.0244 0.1259 1.0000
5.500 0.7190 0.03069 0.01898 -0.0239 0.1182 1.0000
5.750 0.7502 0.03379 0.02205 -0.0237 0.1126 1.0000
6.000 0.7762 0.03609 0.02499 -0.0225 0.1072 1.0000
6.250 0.8019 0.03920 0.02859 -0.0215 0.1060 1.0000
6.500 0.8254 0.04285 0.03283 -0.0203 0.1084 1.0000
6.750 0.8470 0.04707 0.03741 -0.0194 0.1116 1.0000
7.000 0.8626 0.05123 0.04257 -0.0175 0.1211 1.0000
7.250 0.8758 0.05619 0.04822 -0.0164 0.1326 1.0000
7.500 0.8844 0.06204 0.05468 -0.0161 0.1491 1.0000
7.750 0.8807 0.07086 0.06435 -0.0193 0.1979 1.0000
8.000 0.8195 0.08781 0.08167 -0.0398 0.3059 1.0000
8.250 0.7559 0.07289 0.06695 -0.0138 0.2104 1.0000
8.500 0.7138 0.07989 0.07389 -0.0174 0.2129 1.0000
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Polar data table (+)
Polar graphs
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