WORTMANN FX 72-MS-150A AIRFOIL (fx72150a-il) Xfoil prediction polar at RE=500,000 Ncrit=5
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Airfoil: WORTMANN FX 72-MS-150A AIRFOIL (fx72150a-il) Reynolds number: 500,000 Max Cl/Cd: 121.05 at α=6.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx72150a-il-500000-n5.txt Download as CSV file: xf-fx72150a-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 72-MS-150A 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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-9.500 0.2057 0.08884 0.08455 -0.1391 0.6595 0.0147
-9.250 0.2136 0.08646 0.08217 -0.1401 0.6555 0.0150
-9.000 0.2213 0.08410 0.07981 -0.1411 0.6516 0.0153
-8.750 0.2276 0.08159 0.07727 -0.1421 0.6476 0.0158
-8.500 0.2305 0.07866 0.07434 -0.1438 0.6444 0.0161
-8.250 0.2317 0.07535 0.07106 -0.1458 0.6411 0.0162
-8.000 0.2398 0.07305 0.06877 -0.1463 0.6369 0.0163
-7.750 0.2457 0.07057 0.06629 -0.1473 0.6332 0.0163
-7.250 0.2654 0.06712 0.06282 -0.1477 0.6264 0.0167
-7.000 0.2739 0.06534 0.06105 -0.1481 0.6230 0.0172
-6.750 0.2790 0.06313 0.05886 -0.1487 0.6197 0.0174
-6.500 0.2822 0.06099 0.05672 -0.1489 0.6164 0.0177
-6.250 0.2837 0.05899 0.05472 -0.1491 0.6133 0.0180
-5.750 0.2984 0.04927 0.04504 -0.1615 0.6080 0.0192
-5.500 0.3130 0.04593 0.04170 -0.1658 0.6050 0.0194
-5.000 0.3710 0.02934 0.02453 -0.1913 0.5996 0.0133
-4.750 0.4017 0.02643 0.02136 -0.1958 0.5968 0.0130
-4.500 0.4367 0.02282 0.01737 -0.2006 0.5944 0.0126
-4.250 0.4745 0.01890 0.01291 -0.2050 0.5920 0.0120
-4.000 0.5097 0.01628 0.00978 -0.2077 0.5894 0.0118
-3.750 0.5413 0.01504 0.00825 -0.2090 0.5867 0.0118
-3.500 0.5715 0.01425 0.00726 -0.2099 0.5841 0.0119
-3.250 0.6013 0.01367 0.00652 -0.2106 0.5816 0.0122
-2.750 0.6609 0.01280 0.00545 -0.2120 0.5773 0.0129
-2.500 0.6908 0.01248 0.00506 -0.2126 0.5751 0.0132
-2.250 0.7206 0.01222 0.00475 -0.2133 0.5729 0.0135
-2.000 0.7505 0.01198 0.00447 -0.2140 0.5707 0.0140
-1.750 0.7797 0.01184 0.00430 -0.2145 0.5686 0.0146
-1.500 0.8086 0.01176 0.00418 -0.2150 0.5664 0.0156
-1.250 0.8377 0.01167 0.00403 -0.2155 0.5643 0.0165
-1.000 0.8667 0.01160 0.00393 -0.2159 0.5621 0.0173
-0.750 0.8959 0.01154 0.00385 -0.2164 0.5601 0.0185
-0.500 0.9249 0.01149 0.00379 -0.2168 0.5580 0.0211
-0.250 0.9538 0.01145 0.00374 -0.2172 0.5559 0.0283
0.000 0.9830 0.01138 0.00372 -0.2178 0.5539 0.0571
0.250 1.0130 0.01116 0.00375 -0.2187 0.5522 0.1677
0.500 1.0441 0.01073 0.00391 -0.2202 0.5504 0.4325
0.750 1.0717 0.01082 0.00405 -0.2203 0.5486 0.4923
1.000 1.0991 0.01095 0.00419 -0.2204 0.5470 0.5226
1.250 1.1268 0.01105 0.00431 -0.2206 0.5456 0.5370
1.500 1.1545 0.01114 0.00440 -0.2207 0.5443 0.5458
1.750 1.1820 0.01123 0.00451 -0.2209 0.5429 0.5535
2.000 1.2095 0.01134 0.00460 -0.2210 0.5414 0.5589
2.250 1.2368 0.01144 0.00471 -0.2211 0.5399 0.5626
2.500 1.2640 0.01155 0.00482 -0.2212 0.5384 0.5668
2.750 1.2910 0.01167 0.00494 -0.2213 0.5368 0.5711
3.000 1.3178 0.01179 0.00506 -0.2214 0.5353 0.5752
3.250 1.3446 0.01193 0.00519 -0.2215 0.5337 0.5791
3.500 1.3713 0.01207 0.00534 -0.2215 0.5323 0.5834
3.750 1.3980 0.01223 0.00550 -0.2216 0.5310 0.5886
4.000 1.4248 0.01239 0.00567 -0.2217 0.5297 0.5939
4.250 1.4512 0.01251 0.00585 -0.2217 0.5287 0.5986
4.500 1.4774 0.01264 0.00604 -0.2217 0.5274 0.6038
4.750 1.5034 0.01277 0.00622 -0.2217 0.5259 0.6096
5.000 1.5291 0.01291 0.00641 -0.2216 0.5243 0.6152
5.250 1.5547 0.01305 0.00662 -0.2215 0.5227 0.6215
5.500 1.5801 0.01321 0.00683 -0.2214 0.5212 0.6289
5.750 1.6049 0.01336 0.00703 -0.2212 0.5192 0.6372
6.000 1.6282 0.01353 0.00721 -0.2206 0.5156 0.6466
6.250 1.6505 0.01368 0.00744 -0.2199 0.5118 0.6556
6.750 1.6923 0.01398 0.00788 -0.2180 0.5029 0.6756
7.000 1.7115 0.01418 0.00813 -0.2168 0.4990 0.6879
7.250 1.7304 0.01436 0.00841 -0.2155 0.4956 0.7032
7.500 1.7474 0.01456 0.00872 -0.2138 0.4908 0.7228
7.750 1.7621 0.01482 0.00906 -0.2118 0.4856 0.7531
8.000 1.7740 0.01488 0.00939 -0.2092 0.4815 1.0000
8.250 1.7896 0.01524 0.00982 -0.2075 0.4756 1.0000
8.500 1.7977 0.01585 0.01041 -0.2046 0.4666 1.0000
8.750 1.8070 0.01648 0.01109 -0.2021 0.4535 1.0000
9.000 1.8093 0.01749 0.01206 -0.1987 0.4325 1.0000
9.250 1.7970 0.01940 0.01383 -0.1936 0.4065 1.0000
9.500 1.7808 0.02191 0.01620 -0.1885 0.3709 1.0000
9.750 1.7551 0.02541 0.01952 -0.1830 0.3402 1.0000
10.000 1.7326 0.02904 0.02303 -0.1783 0.3095 1.0000
10.250 1.7090 0.03312 0.02699 -0.1740 0.2821 1.0000
10.500 1.6852 0.03760 0.03136 -0.1703 0.2525 1.0000
10.750 1.6603 0.04253 0.03616 -0.1670 0.2220 1.0000
11.000 1.6391 0.04741 0.04093 -0.1643 0.1941 1.0000
11.250 1.6180 0.05251 0.04589 -0.1620 0.1638 1.0000
11.500 1.5992 0.05756 0.05081 -0.1600 0.1335 1.0000
11.750 1.5795 0.06290 0.05597 -0.1583 0.1009 1.0000
12.000 1.5522 0.06938 0.06218 -0.1565 0.0559 1.0000
12.250 1.5330 0.07508 0.06769 -0.1553 0.0203 1.0000
12.500 1.5326 0.07849 0.07109 -0.1547 0.0129 1.0000
12.750 1.5377 0.08118 0.07382 -0.1542 0.0116 1.0000
13.000 1.5440 0.08374 0.07643 -0.1539 0.0108 1.0000
13.250 1.5498 0.08638 0.07914 -0.1536 0.0103 1.0000
13.500 1.5561 0.08896 0.08178 -0.1533 0.0099 1.0000
13.750 1.5622 0.09155 0.08443 -0.1530 0.0096 1.0000
14.000 1.5671 0.09437 0.08732 -0.1528 0.0094 1.0000
14.250 1.5722 0.09716 0.09016 -0.1527 0.0091 1.0000
14.500 1.5771 0.09998 0.09306 -0.1525 0.0089 1.0000
14.750 1.5823 0.10279 0.09593 -0.1525 0.0088 1.0000
15.000 1.5876 0.10555 0.09877 -0.1524 0.0087 1.0000
15.250 1.5928 0.10831 0.10160 -0.1524 0.0085 1.0000
15.500 1.5969 0.11129 0.10465 -0.1525 0.0084 1.0000
15.750 1.6014 0.11420 0.10764 -0.1526 0.0083 1.0000
16.000 1.6058 0.11710 0.11061 -0.1527 0.0082 1.0000
16.250 1.6092 0.12020 0.11378 -0.1530 0.0081 1.0000
16.500 1.6127 0.12325 0.11691 -0.1533 0.0080 1.0000
16.750 1.6164 0.12625 0.11998 -0.1536 0.0079 1.0000
17.000 1.6187 0.12949 0.12330 -0.1540 0.0078 1.0000
17.250 1.6216 0.13263 0.12651 -0.1545 0.0077 1.0000
17.500 1.6243 0.13578 0.12973 -0.1551 0.0076 1.0000
17.750 1.6263 0.13907 0.13310 -0.1557 0.0076 1.0000
18.000 1.6290 0.14223 0.13633 -0.1564 0.0075 1.0000
18.250 1.6308 0.14554 0.13971 -0.1572 0.0074 1.0000
18.500 1.6327 0.14880 0.14305 -0.1581 0.0074 1.0000
18.750 1.6349 0.15200 0.14631 -0.1590 0.0073 1.0000
19.000 1.6366 0.15527 0.14965 -0.1600 0.0073 1.0000
19.250 1.6386 0.15844 0.15288 -0.1610 0.0072 1.0000
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