WORTMANN FX 73-170 (fx73170-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
|---|---|
|
Airfoil: WORTMANN FX 73-170 (fx73170-il) Reynolds number: 200,000 Max Cl/Cd: 45.58 at α=9.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx73170-il-200000-n5.txt Download as CSV file: xf-fx73170-il-200000-n5.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 = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.250 -0.0970 0.11361 0.10853 -0.1230 0.7918 0.0217
-13.000 -0.0858 0.11170 0.10660 -0.1239 0.7903 0.0223
-12.750 -0.0975 0.10250 0.09739 -0.1276 0.7893 0.0168
-12.500 -0.0998 0.09711 0.09202 -0.1300 0.7879 0.0168
-12.250 -0.0945 0.09400 0.08888 -0.1317 0.7864 0.0166
-12.000 -0.0936 0.08991 0.08481 -0.1337 0.7849 0.0165
-11.750 -0.0952 0.08541 0.08036 -0.1358 0.7831 0.0163
-11.500 -0.0932 0.08190 0.07686 -0.1377 0.7813 0.0158
-11.250 -0.1198 0.07018 0.06520 -0.1440 0.7797 0.0158
-11.000 -0.1431 0.06109 0.05603 -0.1504 0.7780 0.0150
-10.750 -0.1766 0.05375 0.04853 -0.1545 0.7759 0.0150
-10.500 -0.2029 0.04874 0.04332 -0.1558 0.7738 0.0149
-10.250 -0.2196 0.04529 0.03969 -0.1557 0.7720 0.0149
-10.000 -0.2393 0.04179 0.03594 -0.1546 0.7701 0.0148
-9.750 -0.2535 0.03937 0.03337 -0.1522 0.7674 0.0147
-9.500 -0.2674 0.03723 0.03101 -0.1490 0.7648 0.0150
-9.250 -0.2694 0.03512 0.02864 -0.1468 0.7624 0.0150
-9.000 -0.2671 0.03296 0.02616 -0.1449 0.7605 0.0153
-8.750 -0.2589 0.03095 0.02384 -0.1433 0.7588 0.0154
-8.500 -0.2459 0.02926 0.02185 -0.1421 0.7573 0.0157
-8.250 -0.2297 0.02767 0.01995 -0.1411 0.7560 0.0161
-8.000 -0.2112 0.02639 0.01833 -0.1402 0.7547 0.0169
-7.750 -0.1937 0.02561 0.01756 -0.1394 0.7527 0.0177
-7.500 -0.1750 0.02490 0.01679 -0.1385 0.7506 0.0185
-7.250 -0.1547 0.02404 0.01583 -0.1377 0.7486 0.0191
-7.000 -0.1339 0.02316 0.01484 -0.1368 0.7468 0.0196
-6.750 -0.1129 0.02238 0.01397 -0.1360 0.7452 0.0203
-6.500 -0.0918 0.02169 0.01316 -0.1352 0.7437 0.0211
-6.250 -0.0717 0.02097 0.01242 -0.1344 0.7423 0.0218
-6.000 -0.0505 0.02042 0.01185 -0.1338 0.7410 0.0231
-5.750 -0.0276 0.02000 0.01136 -0.1335 0.7398 0.0254
-5.500 -0.0066 0.01946 0.01078 -0.1329 0.7384 0.0276
-5.250 0.0118 0.01910 0.01043 -0.1318 0.7360 0.0293
-5.000 0.0322 0.01876 0.01007 -0.1310 0.7339 0.0318
-4.750 0.0535 0.01839 0.00969 -0.1304 0.7320 0.0359
-4.500 0.0759 0.01805 0.00933 -0.1299 0.7304 0.0432
-4.250 0.0990 0.01768 0.00898 -0.1296 0.7288 0.0545
-4.000 0.1222 0.01724 0.00864 -0.1294 0.7274 0.0838
-3.750 0.1441 0.01653 0.00829 -0.1293 0.7260 0.1681
-3.500 0.1635 0.01542 0.00785 -0.1292 0.7247 0.3419
-3.250 0.1822 0.01512 0.00846 -0.1274 0.7236 0.5556
-3.000 0.2048 0.01555 0.00887 -0.1264 0.7215 0.6016
-2.750 0.2272 0.01599 0.00926 -0.1254 0.7192 0.6214
-2.500 0.2505 0.01653 0.00978 -0.1243 0.7172 0.6409
-2.250 0.2741 0.01712 0.01035 -0.1230 0.7154 0.6589
-2.000 0.2991 0.01742 0.01061 -0.1223 0.7137 0.6681
-1.750 0.3256 0.01754 0.01065 -0.1221 0.7122 0.6739
-1.500 0.3534 0.01753 0.01051 -0.1225 0.7109 0.6792
-1.250 0.3808 0.01757 0.01049 -0.1225 0.7098 0.6813
-1.000 0.4087 0.01760 0.01046 -0.1227 0.7089 0.6837
-0.750 0.4357 0.01766 0.01046 -0.1228 0.7078 0.6862
-0.500 0.4498 0.01804 0.01088 -0.1208 0.7041 0.6889
-0.250 0.4712 0.01821 0.01100 -0.1200 0.7014 0.6914
0.000 0.4955 0.01829 0.01103 -0.1199 0.6994 0.6938
0.250 0.5208 0.01836 0.01106 -0.1198 0.6979 0.6955
0.500 0.5471 0.01840 0.01108 -0.1198 0.6965 0.6968
0.750 0.5749 0.01841 0.01105 -0.1200 0.6953 0.6980
1.000 0.6036 0.01839 0.01100 -0.1204 0.6943 0.6993
1.250 0.6330 0.01837 0.01095 -0.1210 0.6934 0.7008
1.500 0.6358 0.01911 0.01178 -0.1171 0.6883 0.7027
1.750 0.6529 0.01941 0.01210 -0.1157 0.6853 0.7042
2.000 0.6766 0.01951 0.01219 -0.1153 0.6832 0.7056
2.250 0.7026 0.01957 0.01224 -0.1153 0.6817 0.7071
2.500 0.7300 0.01961 0.01226 -0.1156 0.6805 0.7088
3.000 0.7900 0.01953 0.01218 -0.1169 0.6786 0.7115
3.500 0.7866 0.02106 0.01386 -0.1075 0.6677 0.7141
3.750 0.8141 0.02104 0.01386 -0.1077 0.6663 0.7153
4.000 0.8438 0.02098 0.01384 -0.1082 0.6652 0.7165
4.250 0.8764 0.02085 0.01374 -0.1093 0.6642 0.7177
4.500 0.9102 0.02070 0.01362 -0.1106 0.6634 0.7194
5.000 0.8484 0.02426 0.01728 -0.0928 0.6435 0.7238
5.250 0.9026 0.02301 0.01608 -0.0965 0.6461 0.7250
5.500 0.9573 0.02198 0.01509 -0.1007 0.6478 0.7262
6.000 0.9377 0.02471 0.01795 -0.0906 0.6312 0.7291
6.250 0.9902 0.02333 0.01666 -0.0938 0.6329 0.7302
6.750 0.9894 0.02579 0.01926 -0.0873 0.6165 0.7337
7.000 1.0492 0.02375 0.01731 -0.0910 0.6189 0.7354
7.500 1.0265 0.02777 0.02145 -0.0827 0.5942 0.7398
7.750 1.0624 0.02690 0.02066 -0.0836 0.5914 0.7417
8.250 1.0886 0.02803 0.02196 -0.0807 0.5706 0.7449
8.750 1.1382 0.02755 0.02160 -0.0800 0.5447 0.7487
9.000 1.1511 0.02822 0.02230 -0.0787 0.5235 0.7508
9.250 1.1875 0.02709 0.02109 -0.0792 0.4942 0.7532
9.500 1.2139 0.02663 0.02038 -0.0786 0.4528 0.7554
9.750 1.2202 0.02768 0.02120 -0.0764 0.4135 0.7577
10.000 1.2159 0.02954 0.02282 -0.0735 0.3712 0.7599
10.250 1.2128 0.03155 0.02466 -0.0709 0.3364 0.7622
10.500 1.2076 0.03385 0.02678 -0.0685 0.3004 0.7651
10.750 1.2043 0.03616 0.02892 -0.0664 0.2664 0.7677
11.000 1.2028 0.03846 0.03106 -0.0647 0.2350 0.7706
11.500 1.2028 0.04313 0.03546 -0.0618 0.1739 0.7756
11.750 1.2046 0.04547 0.03766 -0.0608 0.1462 0.7785
12.000 1.2085 0.04765 0.03977 -0.0599 0.1235 0.7817
12.250 1.2132 0.04981 0.04185 -0.0591 0.1042 0.7852
12.750 1.2260 0.05404 0.04604 -0.0580 0.0754 0.7929
13.000 1.2341 0.05609 0.04812 -0.0577 0.0676 0.7977
13.250 1.2412 0.05823 0.05029 -0.0574 0.0596 0.8029
13.500 1.2500 0.06036 0.05253 -0.0573 0.0542 0.8092
13.750 1.2578 0.06262 0.05484 -0.0572 0.0491 0.8167
14.000 1.2667 0.06493 0.05726 -0.0574 0.0453 0.8273
14.250 1.2773 0.06726 0.05975 -0.0580 0.0420 0.8433
14.500 1.2878 0.07024 0.06289 -0.0595 0.0386 0.8796
14.750 1.2915 0.07218 0.06494 -0.0585 0.0367 1.0000
15.000 1.2968 0.07454 0.06741 -0.0581 0.0347 1.0000
15.250 1.3018 0.07698 0.06991 -0.0579 0.0326 1.0000
15.500 1.3032 0.07984 0.07281 -0.0576 0.0309 1.0000
15.750 1.3079 0.08234 0.07542 -0.0574 0.0293 1.0000
16.000 1.3124 0.08485 0.07805 -0.0573 0.0279 1.0000
16.250 1.3160 0.08753 0.08081 -0.0572 0.0264 1.0000
16.500 1.3180 0.09042 0.08377 -0.0572 0.0252 1.0000
16.750 1.3180 0.09359 0.08698 -0.0573 0.0239 1.0000
17.000 1.3218 0.09631 0.08984 -0.0574 0.0229 1.0000
17.250 1.3246 0.09918 0.09283 -0.0576 0.0218 1.0000
17.500 1.3274 0.10214 0.09590 -0.0581 0.0205 1.0000
17.750 1.3277 0.10538 0.09923 -0.0586 0.0197 1.0000
18.000 1.3259 0.10892 0.10281 -0.0591 0.0190 1.0000
18.250 1.3278 0.11202 0.10607 -0.0597 0.0182 1.0000
18.500 1.3289 0.11524 0.10943 -0.0603 0.0175 1.0000
18.750 1.3294 0.11866 0.11297 -0.0613 0.0166 1.0000
19.000 1.3292 0.12216 0.11658 -0.0623 0.0161 1.0000
19.250 1.3287 0.12575 0.12027 -0.0635 0.0157 1.0000
|
Polar data table (+)
Polar graphs
<< Back to WORTMANN FX 73-170 (fx73170-il)