Rhode St. Genese 36 (rhodesg36-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
|---|---|
|
Airfoil: Rhode St. Genese 36 (rhodesg36-il) Reynolds number: 1,000,000 Max Cl/Cd: 91.49 at α=3.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-rhodesg36-il-1000000-n5.txt Download as CSV file: xf-rhodesg36-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: Rhode St. Genese 36
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
------ -------- --------- --------- -------- -------- --------
-18.250 -0.8331 0.03608 0.03256 -0.1449 0.9422 0.0268
-18.000 -0.8619 0.03128 0.02759 -0.1472 0.9382 0.0268
-17.750 -0.8769 0.02880 0.02497 -0.1463 0.9348 0.0268
-17.500 -0.8816 0.02717 0.02324 -0.1446 0.9310 0.0269
-17.250 -0.8848 0.02591 0.02188 -0.1419 0.9268 0.0269
-17.000 -0.8859 0.02484 0.02071 -0.1388 0.9230 0.0270
-16.750 -0.8821 0.02391 0.01969 -0.1360 0.9183 0.0270
-16.500 -0.8801 0.02306 0.01876 -0.1326 0.9138 0.0272
-16.250 -0.8706 0.02217 0.01781 -0.1303 0.9095 0.0274
-16.000 -0.8562 0.02139 0.01698 -0.1287 0.9031 0.0276
-15.750 -0.8404 0.02068 0.01621 -0.1270 0.8963 0.0277
-15.500 -0.8235 0.02005 0.01552 -0.1253 0.8856 0.0279
-15.250 -0.8080 0.01943 0.01481 -0.1231 0.8684 0.0280
-15.000 -0.7919 0.01890 0.01413 -0.1210 0.8471 0.0282
-14.750 -0.7728 0.01843 0.01353 -0.1194 0.8318 0.0284
-14.500 -0.7522 0.01798 0.01297 -0.1180 0.8208 0.0285
-14.250 -0.7302 0.01754 0.01244 -0.1169 0.8133 0.0287
-14.000 -0.7078 0.01712 0.01194 -0.1159 0.8062 0.0289
-13.750 -0.6848 0.01671 0.01145 -0.1149 0.8005 0.0291
-13.500 -0.6612 0.01629 0.01098 -0.1140 0.7949 0.0293
-13.250 -0.6375 0.01591 0.01052 -0.1131 0.7875 0.0295
-13.000 -0.6134 0.01555 0.01007 -0.1122 0.7802 0.0297
-12.750 -0.5889 0.01518 0.00964 -0.1114 0.7728 0.0300
-12.500 -0.5643 0.01485 0.00922 -0.1106 0.7656 0.0302
-12.250 -0.5390 0.01451 0.00882 -0.1099 0.7585 0.0304
-12.000 -0.5137 0.01421 0.00844 -0.1091 0.7488 0.0306
-11.750 -0.4883 0.01390 0.00806 -0.1084 0.7403 0.0307
-11.500 -0.4634 0.01355 0.00764 -0.1077 0.7294 0.0311
-11.250 -0.4377 0.01326 0.00730 -0.1070 0.7190 0.0314
-11.000 -0.4120 0.01302 0.00700 -0.1063 0.7061 0.0317
-10.750 -0.3860 0.01282 0.00672 -0.1057 0.6905 0.0320
-10.500 -0.3600 0.01264 0.00646 -0.1051 0.6742 0.0324
-10.250 -0.3338 0.01246 0.00621 -0.1044 0.6614 0.0327
-10.000 -0.3076 0.01229 0.00596 -0.1038 0.6511 0.0331
-9.750 -0.2808 0.01211 0.00573 -0.1033 0.6435 0.0336
-9.500 -0.2542 0.01195 0.00551 -0.1028 0.6353 0.0340
-9.250 -0.2275 0.01180 0.00530 -0.1023 0.6280 0.0344
-9.000 -0.2007 0.01162 0.00507 -0.1018 0.6206 0.0347
-8.750 -0.1745 0.01144 0.00485 -0.1012 0.6131 0.0353
-8.500 -0.1474 0.01128 0.00467 -0.1008 0.6071 0.0358
-8.250 -0.1203 0.01115 0.00451 -0.1003 0.6004 0.0363
-8.000 -0.0935 0.01103 0.00435 -0.0999 0.5938 0.0368
-7.750 -0.0662 0.01091 0.00420 -0.0995 0.5880 0.0374
-7.500 -0.0390 0.01079 0.00404 -0.0991 0.5800 0.0380
-7.250 -0.0123 0.01071 0.00390 -0.0986 0.5711 0.0385
-7.000 0.0148 0.01059 0.00375 -0.0982 0.5617 0.0391
-6.750 0.0411 0.01051 0.00363 -0.0976 0.5492 0.0399
-6.500 0.0671 0.01049 0.00354 -0.0971 0.5281 0.0407
-6.250 0.0853 0.01094 0.00359 -0.0952 0.4346 0.0414
-6.000 0.1086 0.01110 0.00359 -0.0942 0.4020 0.0423
-5.750 0.1335 0.01115 0.00354 -0.0935 0.3848 0.0430
-5.500 0.1593 0.01113 0.00347 -0.0929 0.3737 0.0437
-5.250 0.1846 0.01112 0.00342 -0.0922 0.3637 0.0446
-5.000 0.2107 0.01110 0.00338 -0.0917 0.3564 0.0456
-4.750 0.2363 0.01110 0.00334 -0.0911 0.3487 0.0466
-4.500 0.2622 0.01110 0.00330 -0.0905 0.3429 0.0475
-4.250 0.2883 0.01109 0.00327 -0.0900 0.3380 0.0484
-4.000 0.3137 0.01106 0.00323 -0.0894 0.3330 0.0497
-3.750 0.3390 0.01107 0.00322 -0.0888 0.3280 0.0509
-3.500 0.3646 0.01107 0.00320 -0.0882 0.3240 0.0520
-3.250 0.3904 0.01107 0.00318 -0.0877 0.3209 0.0532
-3.000 0.4156 0.01106 0.00317 -0.0871 0.3173 0.0544
-2.750 0.4405 0.01107 0.00316 -0.0864 0.3136 0.0560
-2.500 0.4652 0.01110 0.00317 -0.0857 0.3102 0.0575
-2.000 0.5146 0.01113 0.00319 -0.0844 0.3051 0.0605
-1.750 0.5393 0.01113 0.00321 -0.0837 0.3034 0.0627
-1.500 0.5637 0.01114 0.00323 -0.0830 0.3014 0.0648
-1.250 0.5877 0.01117 0.00325 -0.0822 0.2994 0.0668
-1.000 0.6110 0.01119 0.00328 -0.0813 0.2973 0.0700
-0.750 0.6329 0.01122 0.00331 -0.0801 0.2952 0.0736
-0.500 0.6532 0.01125 0.00334 -0.0786 0.2930 0.0801
-0.250 0.6724 0.01120 0.00343 -0.0770 0.2908 0.1288
0.000 0.6928 0.01129 0.00353 -0.0756 0.2884 0.1389
0.250 0.7150 0.01135 0.00362 -0.0746 0.2874 0.1465
0.500 0.7376 0.01144 0.00372 -0.0737 0.2863 0.1507
0.750 0.7600 0.01152 0.00382 -0.0727 0.2848 0.1554
1.000 0.7824 0.01162 0.00394 -0.0718 0.2832 0.1596
1.250 0.8047 0.01173 0.00406 -0.0708 0.2817 0.1633
1.500 0.8267 0.01185 0.00419 -0.0699 0.2802 0.1681
1.750 0.8484 0.01197 0.00433 -0.0689 0.2786 0.1740
2.000 0.8701 0.01211 0.00448 -0.0679 0.2771 0.1808
2.250 0.9600 0.01078 0.00514 -0.0820 0.2741 0.9835
2.500 0.9890 0.01105 0.00538 -0.0827 0.2719 1.0000
2.750 1.0076 0.01122 0.00553 -0.0811 0.2703 1.0000
3.000 1.0279 0.01137 0.00568 -0.0799 0.2693 1.0000
3.250 1.0484 0.01152 0.00583 -0.0788 0.2675 1.0000
3.500 1.0685 0.01170 0.00600 -0.0776 0.2659 1.0000
3.750 1.0887 0.01190 0.00618 -0.0765 0.2637 1.0000
4.000 1.1086 0.01212 0.00637 -0.0754 0.2610 1.0000
4.250 1.1282 0.01236 0.00659 -0.0742 0.2586 1.0000
4.500 1.1472 0.01263 0.00684 -0.0730 0.2561 1.0000
4.750 1.1667 0.01289 0.00710 -0.0719 0.2543 1.0000
5.000 1.1879 0.01310 0.00732 -0.0711 0.2534 1.0000
5.250 1.2090 0.01333 0.00756 -0.0704 0.2524 1.0000
5.500 1.2295 0.01358 0.00782 -0.0695 0.2513 1.0000
5.750 1.2500 0.01384 0.00809 -0.0687 0.2497 1.0000
6.000 1.2704 0.01412 0.00837 -0.0680 0.2480 1.0000
6.250 1.2904 0.01442 0.00867 -0.0672 0.2457 1.0000
6.500 1.3097 0.01476 0.00901 -0.0663 0.2440 1.0000
6.750 1.3290 0.01511 0.00936 -0.0655 0.2420 1.0000
7.000 1.3477 0.01550 0.00975 -0.0646 0.2398 1.0000
7.250 1.3668 0.01588 0.01014 -0.0639 0.2385 1.0000
7.500 1.3871 0.01622 0.01050 -0.0633 0.2372 1.0000
7.750 1.4071 0.01658 0.01088 -0.0627 0.2348 1.0000
8.000 1.4260 0.01700 0.01131 -0.0621 0.2315 1.0000
8.250 1.4443 0.01746 0.01177 -0.0614 0.2289 1.0000
8.500 1.4615 0.01799 0.01230 -0.0606 0.2257 1.0000
8.750 1.4793 0.01850 0.01283 -0.0599 0.2233 1.0000
9.000 1.4980 0.01898 0.01333 -0.0594 0.2203 1.0000
9.250 1.5153 0.01954 0.01390 -0.0588 0.2165 1.0000
9.500 1.5303 0.02026 0.01460 -0.0579 0.2110 1.0000
9.750 1.5464 0.02092 0.01527 -0.0573 0.2065 1.0000
10.000 1.5602 0.02174 0.01606 -0.0564 0.1985 1.0000
10.250 1.5721 0.02270 0.01699 -0.0554 0.1895 1.0000
10.750 1.5593 0.02719 0.02114 -0.0503 0.1354 1.0000
11.000 1.5535 0.02958 0.02344 -0.0481 0.1172 1.0000
11.250 1.5579 0.03127 0.02512 -0.0470 0.1097 1.0000
11.500 1.5619 0.03305 0.02690 -0.0459 0.1036 1.0000
11.750 1.5699 0.03456 0.02843 -0.0453 0.1001 1.0000
12.000 1.5715 0.03664 0.03051 -0.0443 0.0926 1.0000
12.250 1.5652 0.03949 0.03332 -0.0430 0.0772 1.0000
12.500 1.5483 0.04351 0.03727 -0.0416 0.0607 1.0000
12.750 1.5480 0.04606 0.03986 -0.0411 0.0577 1.0000
13.000 1.5490 0.04852 0.04237 -0.0407 0.0558 1.0000
13.250 1.5472 0.05135 0.04525 -0.0404 0.0540 1.0000
13.500 1.5462 0.05416 0.04812 -0.0402 0.0528 1.0000
13.750 1.5441 0.05711 0.05115 -0.0400 0.0516 1.0000
14.000 1.5414 0.06020 0.05431 -0.0400 0.0506 1.0000
14.250 1.5357 0.06370 0.05788 -0.0400 0.0499 1.0000
14.500 1.5288 0.06746 0.06173 -0.0401 0.0493 1.0000
14.750 1.5181 0.07174 0.06611 -0.0404 0.0486 1.0000
15.000 1.5050 0.07648 0.07095 -0.0409 0.0480 1.0000
15.250 1.4919 0.08134 0.07591 -0.0415 0.0476 1.0000
15.500 1.4762 0.08661 0.08129 -0.0423 0.0472 1.0000
15.750 1.4586 0.09219 0.08699 -0.0432 0.0469 1.0000
|
Polar data table (+)
Polar graphs
<< Back to Rhode St. Genese 36 (rhodesg36-il)