FX 74-130 WP1 (fx74130wp1-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: FX 74-130 WP1 (fx74130wp1-il) Reynolds number: 1,000,000 Max Cl/Cd: 145.62 at α=3.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx74130wp1-il-1000000-n5.txt Download as CSV file: xf-fx74130wp1-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: FX 74-130 WP1
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-10.500 -0.1369 0.08418 0.08135 -0.1178 0.7941 0.0057
-10.250 -0.1353 0.08042 0.07760 -0.1196 0.7931 0.0056
-10.000 -0.1337 0.07680 0.07398 -0.1214 0.7919 0.0054
-9.750 -0.1357 0.07247 0.06966 -0.1237 0.7905 0.0052
-9.500 -0.1431 0.06705 0.06426 -0.1267 0.7888 0.0051
-9.250 -0.1562 0.06062 0.05788 -0.1316 0.7874 0.0049
-9.000 -0.1777 0.05437 0.05162 -0.1358 0.7857 0.0048
-8.500 -0.3383 0.02323 0.01914 -0.1238 0.7804 0.0045
-8.250 -0.3241 0.02114 0.01678 -0.1226 0.7793 0.0046
-8.000 -0.3045 0.01993 0.01539 -0.1219 0.7782 0.0047
-7.750 -0.2850 0.01852 0.01374 -0.1212 0.7771 0.0049
-7.500 -0.2638 0.01729 0.01230 -0.1207 0.7760 0.0052
-7.250 -0.2417 0.01609 0.01090 -0.1201 0.7750 0.0053
-7.000 -0.2180 0.01523 0.00988 -0.1199 0.7741 0.0056
-6.750 -0.1942 0.01433 0.00884 -0.1195 0.7733 0.0057
-6.500 -0.1697 0.01357 0.00796 -0.1193 0.7724 0.0059
-6.250 -0.1447 0.01294 0.00723 -0.1191 0.7714 0.0060
-6.000 -0.1195 0.01236 0.00655 -0.1190 0.7703 0.0061
-5.750 -0.0942 0.01183 0.00595 -0.1188 0.7691 0.0062
-5.500 -0.0682 0.01143 0.00549 -0.1188 0.7679 0.0063
-5.250 -0.0419 0.01109 0.00511 -0.1188 0.7668 0.0064
-5.000 -0.0172 0.01046 0.00440 -0.1186 0.7658 0.0069
-4.750 0.0092 0.01012 0.00403 -0.1186 0.7647 0.0072
-4.500 0.0359 0.00981 0.00370 -0.1187 0.7637 0.0075
-4.250 0.0628 0.00954 0.00339 -0.1188 0.7626 0.0079
-4.000 0.0900 0.00930 0.00311 -0.1189 0.7615 0.0085
-3.750 0.1175 0.00911 0.00287 -0.1191 0.7603 0.0091
-3.500 0.1449 0.00891 0.00266 -0.1193 0.7592 0.0097
-3.250 0.1723 0.00869 0.00244 -0.1195 0.7580 0.0113
-3.000 0.2001 0.00854 0.00229 -0.1198 0.7567 0.0127
-2.750 0.2279 0.00840 0.00214 -0.1200 0.7554 0.0151
-2.500 0.2558 0.00824 0.00203 -0.1203 0.7541 0.0223
-2.250 0.2837 0.00807 0.00192 -0.1206 0.7528 0.0386
-2.000 0.3114 0.00784 0.00182 -0.1210 0.7514 0.0776
-1.750 0.3391 0.00756 0.00172 -0.1214 0.7500 0.1408
-1.500 0.3666 0.00716 0.00163 -0.1219 0.7486 0.2525
-1.250 0.3944 0.00659 0.00154 -0.1227 0.7473 0.4161
-1.000 0.4225 0.00563 0.00156 -0.1238 0.7460 0.7292
-0.750 0.4508 0.00572 0.00171 -0.1239 0.7446 0.7705
-0.500 0.4794 0.00581 0.00180 -0.1242 0.7430 0.7843
-0.250 0.5083 0.00588 0.00185 -0.1246 0.7412 0.7927
0.000 0.5363 0.00594 0.00193 -0.1247 0.7393 0.7983
0.250 0.5650 0.00601 0.00198 -0.1250 0.7376 0.8037
0.500 0.5937 0.00605 0.00201 -0.1254 0.7360 0.8076
0.750 0.6220 0.00608 0.00203 -0.1257 0.7343 0.8098
1.000 0.6507 0.00610 0.00205 -0.1261 0.7325 0.8110
1.250 0.6791 0.00611 0.00208 -0.1264 0.7298 0.8120
1.500 0.7075 0.00611 0.00209 -0.1268 0.7262 0.8131
1.750 0.7358 0.00611 0.00209 -0.1271 0.7223 0.8141
2.000 0.7641 0.00612 0.00208 -0.1274 0.7185 0.8149
2.250 0.7923 0.00613 0.00212 -0.1277 0.7127 0.8156
2.500 0.8199 0.00614 0.00211 -0.1279 0.7063 0.8164
2.750 0.8477 0.00616 0.00214 -0.1281 0.6984 0.8171
3.000 0.8748 0.00620 0.00215 -0.1282 0.6892 0.8177
3.250 0.9011 0.00626 0.00220 -0.1281 0.6775 0.8183
3.500 0.9267 0.00637 0.00226 -0.1279 0.6629 0.8188
3.750 0.9509 0.00653 0.00236 -0.1274 0.6420 0.8195
4.000 0.9727 0.00679 0.00250 -0.1264 0.6122 0.8202
4.250 0.9827 0.00750 0.00287 -0.1231 0.5367 0.8210
4.500 0.9849 0.00852 0.00346 -0.1184 0.4487 0.8219
4.750 0.9880 0.00944 0.00401 -0.1140 0.3724 0.8228
5.000 0.9908 0.01020 0.00450 -0.1095 0.3134 0.8238
5.250 0.9947 0.01087 0.00496 -0.1053 0.2678 0.8247
5.500 0.9987 0.01164 0.00552 -0.1012 0.2224 0.8257
5.750 1.0056 0.01237 0.00608 -0.0979 0.1844 0.8269
6.000 1.0141 0.01309 0.00667 -0.0949 0.1523 0.8279
6.250 1.0246 0.01380 0.00726 -0.0925 0.1242 0.8288
6.500 1.0356 0.01453 0.00787 -0.0902 0.0985 0.8296
6.750 1.0477 0.01526 0.00850 -0.0881 0.0759 0.8304
7.000 1.0610 0.01596 0.00912 -0.0863 0.0576 0.8311
7.250 1.0758 0.01661 0.00972 -0.0847 0.0453 0.8318
7.500 1.0913 0.01723 0.01031 -0.0833 0.0363 0.8325
7.750 1.1068 0.01788 0.01093 -0.0819 0.0288 0.8331
8.000 1.1232 0.01848 0.01153 -0.0807 0.0246 0.8337
8.250 1.1394 0.01911 0.01216 -0.0795 0.0208 0.8343
8.500 1.1565 0.01969 0.01277 -0.0784 0.0193 0.8349
8.750 1.1729 0.02031 0.01341 -0.0772 0.0175 0.8357
9.000 1.1884 0.02100 0.01412 -0.0760 0.0154 0.8365
9.250 1.2049 0.02164 0.01479 -0.0749 0.0143 0.8373
9.500 1.2216 0.02227 0.01547 -0.0738 0.0135 0.8382
9.750 1.2375 0.02296 0.01620 -0.0728 0.0125 0.8390
10.000 1.2530 0.02370 0.01696 -0.0716 0.0114 0.8398
10.250 1.2673 0.02453 0.01782 -0.0704 0.0101 0.8405
10.500 1.2834 0.02523 0.01856 -0.0694 0.0095 0.8413
10.750 1.2988 0.02599 0.01937 -0.0684 0.0088 0.8421
11.000 1.3136 0.02682 0.02023 -0.0673 0.0080 0.8428
11.250 1.3272 0.02773 0.02117 -0.0662 0.0072 0.8436
11.500 1.3411 0.02865 0.02213 -0.0651 0.0067 0.8444
11.750 1.3555 0.02954 0.02308 -0.0640 0.0062 0.8452
12.000 1.3690 0.03051 0.02412 -0.0630 0.0057 0.8461
12.250 1.3818 0.03156 0.02520 -0.0619 0.0051 0.8469
12.500 1.3935 0.03273 0.02641 -0.0607 0.0045 0.8476
12.750 1.4059 0.03384 0.02758 -0.0597 0.0043 0.8484
13.000 1.4180 0.03501 0.02882 -0.0587 0.0041 0.8493
13.250 1.4296 0.03623 0.03013 -0.0577 0.0038 0.8502
13.500 1.4404 0.03754 0.03150 -0.0566 0.0036 0.8512
13.750 1.4509 0.03890 0.03293 -0.0557 0.0033 0.8522
14.000 1.4605 0.04039 0.03449 -0.0547 0.0032 0.8533
14.250 1.4687 0.04205 0.03625 -0.0536 0.0029 0.8544
14.500 1.4752 0.04391 0.03821 -0.0525 0.0027 0.8556
14.750 1.4835 0.04562 0.04001 -0.0517 0.0027 0.8568
15.000 1.4914 0.04739 0.04187 -0.0509 0.0026 0.8581
15.250 1.4991 0.04923 0.04381 -0.0502 0.0026 0.8595
15.500 1.5054 0.05127 0.04596 -0.0495 0.0025 0.8609
15.750 1.5113 0.05341 0.04819 -0.0488 0.0024 0.8623
16.000 1.5166 0.05563 0.05052 -0.0483 0.0023 0.8639
16.250 1.5204 0.05807 0.05308 -0.0478 0.0022 0.8656
16.500 1.5245 0.06055 0.05566 -0.0474 0.0022 0.8673
16.750 1.5268 0.06332 0.05855 -0.0472 0.0021 0.8692
17.000 1.5282 0.06626 0.06163 -0.0470 0.0021 0.8712
17.250 1.5285 0.06944 0.06493 -0.0470 0.0020 0.8732
17.500 1.5279 0.07280 0.06841 -0.0472 0.0020 0.8753
18.000 1.5231 0.08033 0.07621 -0.0481 0.0019 0.8801
18.250 1.5190 0.08452 0.08054 -0.0489 0.0019 0.8830
18.500 1.5137 0.08902 0.08517 -0.0500 0.0018 0.8862
18.750 1.5065 0.09393 0.09024 -0.0514 0.0018 0.8894
19.000 1.4980 0.09919 0.09565 -0.0532 0.0018 0.8932
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