WORTMANN FX 75-193 (fx75193-il) Xfoil prediction polar at RE=100,000 Ncrit=9
| Details | Polar file |
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Airfoil: WORTMANN FX 75-193 (fx75193-il) Reynolds number: 100,000 Max Cl/Cd: 23.4 at α=12.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx75193-il-100000.txt Download as CSV file: xf-fx75193-il-100000.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 75-193
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.100 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-11.000 -0.3214 0.12186 0.11739 -0.0934 0.9458 0.1329
-10.750 -0.2947 0.12058 0.11608 -0.0882 0.9446 0.1343
-10.500 -0.2923 0.11950 0.11502 -0.0847 0.9430 0.1365
-10.250 -0.3005 0.11775 0.11331 -0.0826 0.9411 0.1398
-10.000 -0.4091 0.11310 0.10888 -0.0851 0.9420 0.1452
-9.750 -0.3520 0.11246 0.10819 -0.0799 0.9399 0.1475
-9.500 -0.5148 0.12959 0.12578 -0.0316 1.0000 0.1299
-9.250 -0.5542 0.12346 0.11976 -0.0348 1.0000 0.1340
-9.000 -0.5393 0.12234 0.11863 -0.0316 1.0000 0.1363
-8.750 -0.5459 0.11954 0.11586 -0.0308 1.0000 0.1397
-8.500 -0.6489 0.10992 0.10633 -0.0378 1.0000 0.1448
-8.250 -0.5984 0.10972 0.10617 -0.0328 1.0000 0.1484
-8.000 -0.6041 0.10705 0.10352 -0.0315 1.0000 0.1514
-7.750 -0.6472 0.10162 0.09813 -0.0322 1.0000 0.1546
-7.500 -0.7018 0.09739 0.09391 -0.0303 1.0000 0.1553
-7.250 -0.7670 0.09256 0.08892 -0.0298 1.0000 0.1572
-7.000 -0.8307 0.06680 0.06098 -0.0334 0.9987 0.0703
-6.750 -0.8053 0.06795 0.06264 -0.0355 0.9945 0.0868
-6.500 -0.7896 0.05473 0.04748 -0.0351 0.9919 0.0521
-6.250 -0.7694 0.05199 0.04444 -0.0352 0.9874 0.0510
-6.000 -0.7418 0.04938 0.04131 -0.0363 0.9822 0.0497
-5.750 -0.7104 0.04796 0.03943 -0.0376 0.9788 0.0494
-5.500 -0.6884 0.04611 0.03733 -0.0371 0.9711 0.0497
-5.250 -0.6571 0.04520 0.03618 -0.0381 0.9661 0.0510
-5.000 -0.6270 0.04499 0.03567 -0.0387 0.9632 0.0526
-4.750 -0.6084 0.04357 0.03435 -0.0376 0.9537 0.0550
-4.500 -0.5776 0.04358 0.03434 -0.0387 0.9493 0.0603
-4.250 -0.5596 0.04286 0.03365 -0.0377 0.9413 0.0668
-4.000 -0.5328 0.04235 0.03325 -0.0379 0.9345 0.0778
-3.750 -0.5036 0.04223 0.03344 -0.0391 0.9311 0.1045
-3.500 -0.4918 0.04108 0.03248 -0.0375 0.9210 0.1294
-3.250 -0.4633 0.04084 0.03269 -0.0389 0.9153 0.1795
-2.750 -0.4434 0.04335 0.03777 -0.0293 0.8983 0.6612
-2.500 -0.4159 0.04710 0.04131 -0.0266 0.8939 0.6936
-2.250 -0.4191 0.04700 0.04119 -0.0198 0.8819 0.7049
-2.000 -0.3950 0.04902 0.04306 -0.0174 0.8763 0.7229
-1.750 -0.3920 0.04929 0.04325 -0.0127 0.8685 0.7348
-1.500 -0.3789 0.05012 0.04397 -0.0087 0.8605 0.7520
-1.250 -0.3612 0.05203 0.04580 -0.0045 0.8566 0.7764
-1.000 -0.3716 0.05134 0.04511 0.0029 0.8469 0.7919
-0.750 -0.3628 0.05203 0.04574 0.0086 0.8403 0.8183
-0.500 -0.3434 0.05378 0.04740 0.0130 0.8371 0.8444
-0.250 -0.3601 0.05194 0.04554 0.0198 0.8273 0.8559
0.000 -0.3386 0.05237 0.04584 0.0208 0.8217 0.8692
0.250 -0.2986 0.05406 0.04736 0.0179 0.8187 0.8738
0.500 -0.3114 0.05221 0.04548 0.0227 0.8085 0.8779
0.750 -0.2819 0.05286 0.04597 0.0209 0.8035 0.8820
1.000 -0.2406 0.05477 0.04773 0.0175 0.8008 0.8854
1.250 -0.2543 0.05284 0.04579 0.0222 0.7906 0.8880
1.500 -0.2214 0.05367 0.04650 0.0200 0.7860 0.8897
2.000 -0.1939 0.05408 0.04677 0.0206 0.7746 0.8940
2.250 -0.1595 0.05500 0.04759 0.0182 0.7690 0.8964
2.500 -0.1201 0.05691 0.04938 0.0148 0.7663 0.8978
2.750 -0.1300 0.05591 0.04839 0.0179 0.7589 0.8995
3.000 -0.0941 0.05689 0.04928 0.0153 0.7528 0.9007
3.250 -0.0662 0.05824 0.05057 0.0136 0.7498 0.9022
3.500 -0.0637 0.05780 0.05014 0.0153 0.7410 0.9040
3.750 -0.0152 0.05949 0.05174 0.0115 0.7356 0.9061
4.000 -0.0223 0.05915 0.05142 0.0141 0.7282 0.9085
4.250 0.0260 0.06051 0.05271 0.0103 0.7212 0.9100
4.500 0.0670 0.05816 0.05026 0.0096 0.6840 0.9113
4.750 0.1162 0.05844 0.05049 0.0064 0.6770 0.9131
5.000 0.1221 0.05896 0.05101 0.0073 0.6665 0.9151
5.250 0.1677 0.05928 0.05130 0.0044 0.6612 0.9168
5.500 0.1694 0.06025 0.05231 0.0055 0.6526 0.9183
5.750 0.2052 0.06064 0.05270 0.0035 0.6466 0.9197
6.000 0.2213 0.06139 0.05346 0.0034 0.6375 0.9213
6.250 0.2503 0.06192 0.05401 0.0020 0.6311 0.9233
6.500 0.3008 0.06205 0.05416 -0.0010 0.6275 0.9255
6.750 0.2952 0.06338 0.05553 0.0004 0.6157 0.9272
7.000 0.3415 0.06348 0.05566 -0.0023 0.6114 0.9288
7.250 0.3430 0.06495 0.05717 -0.0016 0.6002 0.9301
7.500 0.3818 0.06524 0.05750 -0.0038 0.5951 0.9315
7.750 0.4310 0.06522 0.05755 -0.0067 0.5924 0.9332
8.000 0.4180 0.06747 0.05987 -0.0052 0.5795 0.9349
8.250 0.4639 0.06734 0.05981 -0.0076 0.5758 0.9374
8.500 0.4620 0.06938 0.06192 -0.0070 0.5638 0.9394
8.750 0.5040 0.06928 0.06192 -0.0091 0.5589 0.9417
9.000 0.5554 0.06857 0.06129 -0.0117 0.5560 0.9438
9.250 0.5502 0.07092 0.06373 -0.0111 0.5418 0.9453
9.750 0.5903 0.07338 0.06641 -0.0132 0.5251 0.9498
10.000 0.6385 0.07262 0.06579 -0.0155 0.5215 0.9535
10.250 0.6343 0.07577 0.06904 -0.0157 0.5082 0.9565
10.500 0.6796 0.07518 0.06862 -0.0179 0.5039 0.9610
10.750 0.7338 0.07349 0.06710 -0.0201 0.5009 0.9682
11.250 0.7283 0.07884 0.07264 -0.0197 0.4731 1.0000
11.500 0.7717 0.07761 0.07158 -0.0209 0.4679 1.0000
11.750 0.8173 0.07559 0.06973 -0.0218 0.4617 1.0000
12.000 0.9399 0.06317 0.05763 -0.0233 0.4642 1.0000
12.250 0.9499 0.06391 0.05850 -0.0227 0.4487 1.0000
12.500 1.0485 0.05295 0.04777 -0.0231 0.4378 1.0000
12.750 1.1113 0.04750 0.04232 -0.0236 0.4078 1.0000
13.000 1.1091 0.04975 0.04463 -0.0224 0.3800 1.0000
13.250 1.1154 0.05111 0.04584 -0.0214 0.3393 1.0000
13.500 1.1109 0.05369 0.04813 -0.0201 0.2857 1.0000
13.750 1.0940 0.05775 0.05173 -0.0187 0.2200 1.0000
14.000 1.0703 0.06292 0.05638 -0.0176 0.1614 1.0000
14.250 1.0488 0.06822 0.06123 -0.0170 0.1211 1.0000
14.500 1.0340 0.07300 0.06570 -0.0167 0.0964 1.0000
14.750 1.0290 0.07676 0.06927 -0.0166 0.0820 1.0000
15.000 1.0329 0.07944 0.07184 -0.0164 0.0709 1.0000
15.250 1.0462 0.08094 0.07320 -0.0162 0.0632 1.0000
15.500 1.0669 0.08167 0.07385 -0.0159 0.0575 1.0000
15.750 1.0911 0.08218 0.07429 -0.0159 0.0530 1.0000
16.000 1.1232 0.08198 0.07395 -0.0158 0.0497 1.0000
16.250 1.1544 0.08235 0.07445 -0.0158 0.0475 1.0000
16.500 1.1968 0.08206 0.07410 -0.0161 0.0458 1.0000
16.750 1.2329 0.08306 0.07524 -0.0166 0.0448 1.0000
17.000 1.2519 0.08546 0.07794 -0.0169 0.0444 1.0000
17.250 1.2635 0.08850 0.08128 -0.0173 0.0441 1.0000
17.500 1.2699 0.09194 0.08501 -0.0177 0.0441 1.0000
17.750 1.2718 0.09574 0.08910 -0.0182 0.0442 1.0000
18.000 1.2695 0.09989 0.09353 -0.0188 0.0443 1.0000
18.250 1.2640 0.10432 0.09822 -0.0197 0.0445 1.0000
18.500 1.2564 0.10896 0.10312 -0.0209 0.0447 1.0000
18.750 1.2507 0.11358 0.10795 -0.0222 0.0450 1.0000
19.000 1.2486 0.11806 0.11261 -0.0236 0.0453 1.0000
19.250 1.1751 0.12937 0.12453 -0.0287 0.0464 1.0000
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