WORTMANN FX 73-170 (fx73170-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: WORTMANN FX 73-170 (fx73170-il) Reynolds number: 500,000 Max Cl/Cd: 110.3 at α=7.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx73170-il-500000.txt Download as CSV file: xf-fx73170-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 73-170
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
------ -------- --------- --------- -------- -------- --------
-12.500 -0.0759 0.10061 0.09691 -0.1318 0.7821 0.0233
-12.250 -0.0834 0.09271 0.08902 -0.1367 0.7809 0.0238
-12.000 -0.0787 0.08860 0.08492 -0.1394 0.7798 0.0238
-11.750 -0.0733 0.08554 0.08188 -0.1409 0.7785 0.0240
-11.500 -0.0644 0.08352 0.07987 -0.1419 0.7771 0.0244
-11.250 -0.0623 0.07918 0.07555 -0.1448 0.7758 0.0246
-11.000 -0.0580 0.07566 0.07205 -0.1472 0.7743 0.0251
-10.750 -0.0076 0.05060 0.04714 -0.1509 0.7678 0.0283
-10.500 -0.0316 0.04305 0.03953 -0.1556 0.7667 0.0280
-10.250 -0.0590 0.03715 0.03353 -0.1588 0.7654 0.0279
-10.000 -0.0815 0.03303 0.02933 -0.1599 0.7639 0.0278
-9.750 -0.1055 0.02977 0.02597 -0.1596 0.7623 0.0280
-9.500 -0.1348 0.02757 0.02361 -0.1577 0.7603 0.0285
-9.250 -0.1639 0.02757 0.02342 -0.1526 0.7578 0.0290
-9.000 -0.2359 0.03044 0.02524 -0.1544 0.7591 0.0180
-8.750 -0.2326 0.02772 0.02224 -0.1521 0.7574 0.0174
-8.500 -0.2236 0.02522 0.01942 -0.1501 0.7557 0.0170
-8.250 -0.2078 0.02367 0.01762 -0.1488 0.7540 0.0174
-8.000 -0.1891 0.02197 0.01568 -0.1479 0.7526 0.0172
-7.750 -0.1681 0.02080 0.01432 -0.1472 0.7512 0.0177
-7.500 -0.1457 0.01986 0.01322 -0.1466 0.7498 0.0180
-7.250 -0.1239 0.01941 0.01262 -0.1458 0.7484 0.0187
-7.000 -0.1036 0.01819 0.01136 -0.1449 0.7471 0.0195
-6.750 -0.0834 0.01745 0.01063 -0.1440 0.7456 0.0201
-6.500 -0.0626 0.01691 0.01008 -0.1431 0.7440 0.0207
-6.250 -0.0415 0.01641 0.00956 -0.1422 0.7423 0.0215
-6.000 -0.0199 0.01596 0.00907 -0.1415 0.7407 0.0227
-5.750 0.0026 0.01555 0.00860 -0.1408 0.7391 0.0235
-5.500 0.0217 0.01484 0.00789 -0.1398 0.7378 0.0253
-5.250 0.0457 0.01453 0.00756 -0.1396 0.7365 0.0276
-5.000 0.0690 0.01414 0.00711 -0.1392 0.7353 0.0303
-4.750 0.0929 0.01385 0.00680 -0.1389 0.7340 0.0338
-4.500 0.1157 0.01355 0.00649 -0.1383 0.7327 0.0387
-4.250 0.1379 0.01321 0.00621 -0.1377 0.7312 0.0504
-4.000 0.1580 0.01264 0.00590 -0.1368 0.7294 0.1060
-3.750 0.1750 0.01174 0.00558 -0.1358 0.7276 0.2511
-3.500 0.1881 0.01061 0.00519 -0.1341 0.7259 0.4588
-3.250 0.2096 0.01051 0.00547 -0.1330 0.7245 0.5863
-3.000 0.2372 0.01072 0.00564 -0.1329 0.7232 0.6103
-2.750 0.2653 0.01095 0.00583 -0.1329 0.7220 0.6258
-2.500 0.2938 0.01125 0.00609 -0.1329 0.7209 0.6393
-2.250 0.3225 0.01149 0.00624 -0.1331 0.7197 0.6494
-2.000 0.3519 0.01193 0.00670 -0.1331 0.7184 0.6601
-1.750 0.3773 0.01224 0.00704 -0.1325 0.7170 0.6692
-1.500 0.4028 0.01250 0.00734 -0.1320 0.7154 0.6758
-1.250 0.4283 0.01266 0.00745 -0.1317 0.7137 0.6813
-1.000 0.4541 0.01270 0.00751 -0.1314 0.7121 0.6840
-0.750 0.4809 0.01276 0.00756 -0.1314 0.7105 0.6864
-0.500 0.5082 0.01278 0.00757 -0.1315 0.7090 0.6888
-0.250 0.5358 0.01279 0.00754 -0.1317 0.7076 0.6911
0.000 0.5638 0.01281 0.00751 -0.1320 0.7064 0.6933
0.250 0.5924 0.01281 0.00747 -0.1324 0.7053 0.6952
0.500 0.6215 0.01286 0.00745 -0.1330 0.7042 0.6968
0.750 0.6501 0.01290 0.00747 -0.1335 0.7029 0.6979
1.000 0.6721 0.01293 0.00755 -0.1326 0.7010 0.6991
1.250 0.6954 0.01301 0.00766 -0.1320 0.6991 0.7003
1.500 0.7199 0.01307 0.00775 -0.1317 0.6972 0.7014
1.750 0.7457 0.01310 0.00778 -0.1316 0.6954 0.7025
2.000 0.7726 0.01310 0.00780 -0.1317 0.6938 0.7037
2.250 0.8002 0.01311 0.00780 -0.1319 0.6924 0.7050
2.500 0.8285 0.01311 0.00779 -0.1323 0.6911 0.7064
2.750 0.8580 0.01310 0.00777 -0.1329 0.6898 0.7076
3.000 0.8879 0.01315 0.00781 -0.1336 0.6886 0.7087
3.250 0.9111 0.01328 0.00798 -0.1331 0.6867 0.7099
3.500 0.9305 0.01340 0.00816 -0.1317 0.6840 0.7111
3.750 0.9539 0.01346 0.00825 -0.1312 0.6815 0.7122
4.000 0.9799 0.01343 0.00825 -0.1311 0.6794 0.7134
4.250 1.0082 0.01332 0.00816 -0.1314 0.6774 0.7146
4.500 1.0396 0.01316 0.00802 -0.1323 0.6755 0.7156
4.750 1.0743 0.01303 0.00787 -0.1338 0.6735 0.7166
5.000 1.0892 0.01310 0.00805 -0.1315 0.6696 0.7178
5.250 1.1110 0.01302 0.00803 -0.1305 0.6658 0.7190
5.500 1.1411 0.01271 0.00774 -0.1310 0.6621 0.7202
5.750 1.1766 0.01245 0.00744 -0.1326 0.6589 0.7215
6.000 1.1893 0.01247 0.00757 -0.1298 0.6539 0.7229
6.250 1.2124 0.01221 0.00735 -0.1289 0.6481 0.7245
6.500 1.2366 0.01194 0.00707 -0.1281 0.6416 0.7260
6.750 1.2489 0.01180 0.00697 -0.1250 0.6333 0.7275
7.000 1.2632 0.01168 0.00687 -0.1223 0.6249 0.7287
7.250 1.2731 0.01162 0.00688 -0.1188 0.6177 0.7301
7.500 1.2825 0.01165 0.00697 -0.1153 0.6096 0.7315
7.750 1.2949 0.01174 0.00709 -0.1124 0.6012 0.7331
8.000 1.3015 0.01197 0.00739 -0.1085 0.5907 0.7348
8.250 1.3098 0.01224 0.00770 -0.1051 0.5791 0.7365
8.500 1.3145 0.01267 0.00812 -0.1013 0.5630 0.7383
8.750 1.3148 0.01336 0.00876 -0.0971 0.5415 0.7402
9.000 1.3135 0.01437 0.00970 -0.0931 0.5157 0.7422
9.250 1.3007 0.01614 0.01129 -0.0880 0.4782 0.7442
9.500 1.2897 0.01830 0.01327 -0.0840 0.4390 0.7462
9.750 1.2769 0.02077 0.01555 -0.0801 0.3997 0.7481
10.000 1.2630 0.02344 0.01800 -0.0765 0.3582 0.7499
10.250 1.2565 0.02577 0.02018 -0.0737 0.3226 0.7519
10.500 1.2522 0.02809 0.02234 -0.0714 0.2876 0.7539
10.750 1.2460 0.03061 0.02464 -0.0691 0.2494 0.7559
11.000 1.2441 0.03288 0.02673 -0.0672 0.2135 0.7579
11.250 1.2432 0.03515 0.02881 -0.0655 0.1792 0.7598
11.500 1.2465 0.03734 0.03085 -0.0645 0.1485 0.7619
11.750 1.2495 0.03953 0.03289 -0.0634 0.1192 0.7642
12.000 1.2533 0.04166 0.03488 -0.0624 0.0946 0.7666
12.250 1.2592 0.04363 0.03678 -0.0616 0.0767 0.7693
12.500 1.2661 0.04553 0.03864 -0.0608 0.0640 0.7721
12.750 1.2735 0.04743 0.04051 -0.0601 0.0557 0.7750
13.000 1.2836 0.04935 0.04244 -0.0600 0.0491 0.7782
13.250 1.2945 0.05116 0.04432 -0.0599 0.0448 0.7820
13.500 1.3046 0.05307 0.04629 -0.0597 0.0416 0.7860
13.750 1.3103 0.05531 0.04854 -0.0592 0.0377 0.7903
14.000 1.3245 0.05711 0.05047 -0.0597 0.0355 0.7952
14.250 1.3358 0.05912 0.05255 -0.0600 0.0332 0.8012
14.500 1.3385 0.06191 0.05540 -0.0597 0.0308 0.8074
14.750 1.3534 0.06383 0.05745 -0.0605 0.0290 0.8165
15.000 1.3675 0.06599 0.05975 -0.0615 0.0273 0.8297
15.250 1.3800 0.06903 0.06291 -0.0634 0.0253 0.8521
15.500 1.4063 0.07290 0.06706 -0.0689 0.0234 0.9256
15.750 1.4145 0.07523 0.06945 -0.0684 0.0221 1.0000
16.000 1.4201 0.07754 0.07180 -0.0681 0.0210 1.0000
16.250 1.4207 0.08043 0.07472 -0.0677 0.0198 1.0000
16.500 1.4190 0.08360 0.07796 -0.0672 0.0189 1.0000
16.750 1.4246 0.08599 0.08045 -0.0671 0.0182 1.0000
17.000 1.4285 0.08861 0.08315 -0.0670 0.0174 1.0000
17.250 1.4321 0.09129 0.08590 -0.0669 0.0165 1.0000
17.500 1.4330 0.09428 0.08893 -0.0670 0.0158 1.0000
17.750 1.4273 0.09805 0.09276 -0.0668 0.0153 1.0000
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