WORTMANN FX 73-170 A (fx73170a-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: WORTMANN FX 73-170 A (fx73170a-il) Reynolds number: 500,000 Max Cl/Cd: 117.85 at α=8.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx73170a-il-500000.txt Download as CSV file: xf-fx73170a-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: FX 73-170 A
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
------ -------- --------- --------- -------- -------- --------
-12.250 0.0247 0.10555 0.10171 -0.1338 0.7527 0.0183
-12.000 0.0294 0.10191 0.09808 -0.1362 0.7506 0.0184
-11.750 0.0328 0.09781 0.09400 -0.1389 0.7486 0.0185
-11.500 0.0385 0.09426 0.09045 -0.1412 0.7465 0.0185
-11.250 0.0428 0.09052 0.08671 -0.1423 0.7445 0.0188
-11.000 0.0571 0.08928 0.08545 -0.1420 0.7425 0.0196
-10.750 0.0628 0.08566 0.08181 -0.1448 0.7406 0.0193
-10.500 0.0716 0.08284 0.07897 -0.1467 0.7387 0.0198
-10.250 0.0763 0.07977 0.07594 -0.1483 0.7368 0.0202
-10.000 0.0805 0.07654 0.07272 -0.1503 0.7346 0.0202
-9.750 0.0811 0.07255 0.06876 -0.1527 0.7324 0.0218
-9.500 0.0808 0.06826 0.06449 -0.1557 0.7303 0.0222
-8.000 -0.0291 0.04185 0.03747 -0.1570 0.7163 0.0235
-7.750 -0.0275 0.03938 0.03490 -0.1550 0.7142 0.0236
-7.500 -0.0159 0.03778 0.03332 -0.1542 0.7124 0.0241
-7.250 -0.0078 0.03617 0.03161 -0.1525 0.7106 0.0247
-7.000 0.0017 0.03462 0.02994 -0.1509 0.7085 0.0252
-6.750 0.0093 0.03273 0.02791 -0.1486 0.7066 0.0259
-6.500 -0.0073 0.02514 0.01918 -0.1403 0.7045 0.0186
-6.250 0.0080 0.02326 0.01702 -0.1385 0.7024 0.0186
-6.000 0.0266 0.02099 0.01460 -0.1374 0.7005 0.0181
-5.750 0.0475 0.01958 0.01294 -0.1363 0.6989 0.0182
-5.500 0.0706 0.01841 0.01154 -0.1356 0.6973 0.0183
-5.250 0.0946 0.01712 0.01005 -0.1351 0.6957 0.0188
-5.000 0.1192 0.01607 0.00890 -0.1348 0.6941 0.0193
-4.750 0.1414 0.01539 0.00821 -0.1339 0.6925 0.0197
-4.500 0.1639 0.01489 0.00770 -0.1331 0.6906 0.0205
-4.250 0.1867 0.01446 0.00725 -0.1323 0.6886 0.0216
-4.000 0.2098 0.01405 0.00678 -0.1316 0.6867 0.0228
-3.750 0.2311 0.01350 0.00621 -0.1306 0.6850 0.0243
-3.500 0.2552 0.01323 0.00593 -0.1301 0.6835 0.0272
-3.250 0.2786 0.01287 0.00551 -0.1294 0.6820 0.0300
-3.000 0.3028 0.01260 0.00522 -0.1290 0.6805 0.0341
-2.750 0.3269 0.01239 0.00498 -0.1285 0.6790 0.0427
-2.500 0.3477 0.01208 0.00479 -0.1274 0.6775 0.0662
-2.250 0.3639 0.01147 0.00466 -0.1256 0.6757 0.1891
-2.000 0.3731 0.01055 0.00453 -0.1227 0.6739 0.4220
-1.750 0.3789 0.00978 0.00453 -0.1184 0.6719 0.6451
-1.500 0.3977 0.00975 0.00473 -0.1164 0.6703 0.7390
-1.250 0.4215 0.00988 0.00485 -0.1154 0.6688 0.7735
-1.000 0.4471 0.01000 0.00493 -0.1150 0.6675 0.7910
-0.750 0.4730 0.01015 0.00503 -0.1145 0.6662 0.8062
-0.500 0.4988 0.01038 0.00524 -0.1140 0.6648 0.8230
-0.250 0.5204 0.01062 0.00552 -0.1124 0.6634 0.8412
0.000 0.5409 0.01074 0.00565 -0.1109 0.6617 0.8526
0.250 0.5637 0.01083 0.00576 -0.1099 0.6600 0.8612
0.500 0.5866 0.01088 0.00580 -0.1091 0.6581 0.8681
0.750 0.6123 0.01091 0.00582 -0.1088 0.6566 0.8724
1.000 0.6379 0.01096 0.00583 -0.1087 0.6552 0.8765
1.250 0.6637 0.01101 0.00584 -0.1085 0.6538 0.8804
1.500 0.6914 0.01103 0.00583 -0.1088 0.6525 0.8833
1.750 0.7205 0.01108 0.00585 -0.1094 0.6513 0.8863
2.000 0.7498 0.01121 0.00593 -0.1101 0.6498 0.8894
2.250 0.7704 0.01130 0.00605 -0.1090 0.6483 0.8934
2.500 0.7904 0.01139 0.00617 -0.1077 0.6465 0.8972
2.750 0.8138 0.01146 0.00628 -0.1072 0.6449 0.9005
3.000 0.8376 0.01155 0.00639 -0.1068 0.6432 0.9041
3.250 0.8619 0.01162 0.00647 -0.1065 0.6416 0.9080
3.500 0.8870 0.01167 0.00652 -0.1063 0.6400 0.9116
3.750 0.9164 0.01171 0.00657 -0.1070 0.6386 0.9145
4.000 0.9463 0.01178 0.00664 -0.1079 0.6374 0.9176
4.250 0.9770 0.01187 0.00673 -0.1090 0.6361 0.9207
4.500 1.0055 0.01205 0.00690 -0.1096 0.6345 0.9242
4.750 1.0256 0.01219 0.00714 -0.1086 0.6327 0.9286
5.000 1.0501 0.01233 0.00736 -0.1085 0.6306 0.9329
5.250 1.0758 0.01245 0.00754 -0.1087 0.6285 0.9373
5.500 1.1037 0.01254 0.00768 -0.1093 0.6265 0.9416
5.750 1.1396 0.01253 0.00771 -0.1115 0.6245 0.9450
6.000 1.1765 0.01254 0.00773 -0.1139 0.6227 0.9486
6.250 1.2145 0.01259 0.00778 -0.1166 0.6208 0.9520
6.500 1.2455 0.01276 0.00806 -0.1181 0.6179 0.9573
6.750 1.2797 0.01290 0.00830 -0.1203 0.6147 0.9626
7.000 1.3180 0.01284 0.00831 -0.1232 0.6110 0.9676
7.250 1.3602 0.01268 0.00815 -0.1266 0.6076 0.9718
7.500 1.3985 0.01273 0.00826 -0.1295 0.6037 0.9784
7.750 1.4262 0.01284 0.00848 -0.1303 0.5985 1.0000
8.000 1.4530 0.01260 0.00822 -0.1305 0.5925 1.0000
8.250 1.4633 0.01269 0.00839 -0.1276 0.5845 1.0000
8.500 1.4825 0.01258 0.00823 -0.1262 0.5761 1.0000
8.750 1.4876 0.01292 0.00869 -0.1227 0.5690 1.0000
9.000 1.5064 0.01308 0.00887 -0.1216 0.5627 1.0000
9.250 1.5167 0.01356 0.00946 -0.1193 0.5556 1.0000
9.500 1.5307 0.01396 0.00987 -0.1177 0.5468 1.0000
9.750 1.5367 0.01476 0.01075 -0.1151 0.5353 1.0000
10.000 1.5432 0.01570 0.01173 -0.1128 0.5222 1.0000
10.250 1.5474 0.01686 0.01291 -0.1104 0.5063 1.0000
10.500 1.5451 0.01849 0.01449 -0.1073 0.4834 1.0000
10.750 1.5351 0.02070 0.01659 -0.1036 0.4552 1.0000
11.000 1.5082 0.02408 0.01974 -0.0981 0.4165 1.0000
11.250 1.4984 0.02654 0.02213 -0.0948 0.3937 1.0000
11.500 1.4784 0.02989 0.02532 -0.0907 0.3629 1.0000
11.750 1.4586 0.03340 0.02867 -0.0869 0.3308 1.0000
12.000 1.4406 0.03697 0.03207 -0.0836 0.2995 1.0000
12.250 1.4321 0.03986 0.03486 -0.0812 0.2745 1.0000
12.500 1.4110 0.04394 0.03869 -0.0780 0.2361 1.0000
12.750 1.4080 0.04652 0.04119 -0.0763 0.2145 1.0000
13.000 1.3960 0.04996 0.04442 -0.0740 0.1820 1.0000
13.250 1.3892 0.05299 0.04729 -0.0722 0.1543 1.0000
13.500 1.3858 0.05576 0.04994 -0.0708 0.1314 1.0000
13.750 1.3812 0.05868 0.05272 -0.0693 0.1077 1.0000
14.000 1.3770 0.06162 0.05552 -0.0680 0.0855 1.0000
14.250 1.3759 0.06433 0.05813 -0.0669 0.0684 1.0000
14.500 1.3767 0.06687 0.06063 -0.0659 0.0569 1.0000
14.750 1.3787 0.06932 0.06306 -0.0651 0.0484 1.0000
15.000 1.3795 0.07197 0.06569 -0.0643 0.0416 1.0000
15.250 1.3847 0.07419 0.06795 -0.0638 0.0382 1.0000
15.500 1.3846 0.07699 0.07075 -0.0631 0.0341 1.0000
15.750 1.3910 0.07913 0.07298 -0.0627 0.0320 1.0000
16.000 1.3954 0.08146 0.07534 -0.0624 0.0293 1.0000
16.250 1.3936 0.08457 0.07848 -0.0618 0.0268 1.0000
16.500 1.4006 0.08667 0.08068 -0.0616 0.0251 1.0000
16.750 1.4031 0.08932 0.08337 -0.0614 0.0229 1.0000
17.000 1.4013 0.09253 0.08662 -0.0611 0.0208 1.0000
17.250 1.4079 0.09474 0.08891 -0.0610 0.0185 1.0000
17.500 1.4036 0.09830 0.09250 -0.0608 0.0167 1.0000
17.750 1.4035 0.10139 0.09569 -0.0608 0.0154 1.0000
18.000 1.4094 0.10372 0.09807 -0.0609 0.0140 1.0000
18.250 1.4031 0.10768 0.10208 -0.0610 0.0128 1.0000
18.500 1.4010 0.11115 0.10566 -0.0612 0.0121 1.0000
18.750 1.4048 0.11385 0.10843 -0.0616 0.0111 1.0000
19.000 1.4051 0.11702 0.11168 -0.0620 0.0105 1.0000
19.250 1.4010 0.12082 0.11555 -0.0626 0.0101 1.0000
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