Rhode St. Genese 36 (rhodesg36-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
|---|---|
|
Airfoil: Rhode St. Genese 36 (rhodesg36-il) Reynolds number: 500,000 Max Cl/Cd: 70.08 at α=4.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-rhodesg36-il-500000-n5.txt Download as CSV file: xf-rhodesg36-il-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-15.500 -0.5391 0.03790 0.03416 -0.1428 0.9423 0.0315
-15.250 -0.5745 0.03369 0.02972 -0.1430 0.9336 0.0315
-15.000 -0.5891 0.03169 0.02758 -0.1406 0.9258 0.0316
-14.750 -0.5958 0.03023 0.02601 -0.1376 0.9176 0.0317
-14.500 -0.6003 0.02903 0.02470 -0.1341 0.9092 0.0318
-14.000 -0.5863 0.02682 0.02228 -0.1298 0.8874 0.0321
-13.750 -0.5764 0.02580 0.02114 -0.1275 0.8752 0.0323
-13.500 -0.5663 0.02477 0.01996 -0.1251 0.8630 0.0325
-13.250 -0.5546 0.02379 0.01881 -0.1227 0.8513 0.0328
-12.750 -0.5246 0.02198 0.01662 -0.1189 0.8299 0.0333
-12.500 -0.5073 0.02116 0.01559 -0.1173 0.8198 0.0336
-12.250 -0.4883 0.02039 0.01463 -0.1160 0.8098 0.0340
-12.000 -0.4683 0.01969 0.01373 -0.1147 0.8007 0.0343
-11.750 -0.4468 0.01903 0.01291 -0.1136 0.7916 0.0345
-11.250 -0.4015 0.01800 0.01172 -0.1117 0.7758 0.0351
-11.000 -0.3777 0.01762 0.01126 -0.1109 0.7668 0.0354
-10.750 -0.3532 0.01726 0.01085 -0.1101 0.7585 0.0357
-10.500 -0.3284 0.01694 0.01047 -0.1094 0.7496 0.0361
-10.250 -0.3034 0.01661 0.01006 -0.1087 0.7417 0.0366
-10.000 -0.2785 0.01625 0.00962 -0.1080 0.7319 0.0371
-9.750 -0.2536 0.01588 0.00915 -0.1072 0.7218 0.0376
-9.500 -0.2288 0.01550 0.00866 -0.1065 0.7109 0.0381
-9.250 -0.2036 0.01514 0.00818 -0.1058 0.7002 0.0386
-9.000 -0.1789 0.01480 0.00774 -0.1050 0.6892 0.0390
-8.750 -0.1536 0.01451 0.00741 -0.1044 0.6782 0.0395
-8.500 -0.1281 0.01430 0.00713 -0.1037 0.6681 0.0399
-8.250 -0.1023 0.01409 0.00687 -0.1031 0.6592 0.0405
-8.000 -0.0767 0.01390 0.00660 -0.1024 0.6511 0.0411
-7.750 -0.0506 0.01368 0.00633 -0.1019 0.6430 0.0418
-7.500 -0.0251 0.01349 0.00605 -0.1012 0.6342 0.0425
-7.250 0.0009 0.01332 0.00579 -0.1006 0.6254 0.0433
-7.000 0.0262 0.01313 0.00556 -0.1000 0.6161 0.0440
-6.750 0.0522 0.01299 0.00539 -0.0994 0.6085 0.0448
-6.500 0.0784 0.01285 0.00522 -0.0989 0.6000 0.0456
-6.250 0.1038 0.01274 0.00504 -0.0982 0.5915 0.0464
-6.000 0.1300 0.01259 0.00485 -0.0977 0.5815 0.0474
-5.750 0.1552 0.01250 0.00467 -0.0970 0.5706 0.0483
-5.500 0.1802 0.01235 0.00450 -0.0963 0.5558 0.0492
-5.250 0.2041 0.01232 0.00439 -0.0953 0.5320 0.0502
-5.000 0.2230 0.01252 0.00433 -0.0936 0.4730 0.0513
-4.750 0.2401 0.01283 0.00436 -0.0916 0.4221 0.0524
-4.500 0.2620 0.01294 0.00433 -0.0903 0.4012 0.0535
-4.250 0.2844 0.01295 0.00427 -0.0892 0.3873 0.0546
-4.000 0.3080 0.01294 0.00423 -0.0883 0.3777 0.0558
-3.750 0.3313 0.01296 0.00420 -0.0874 0.3687 0.0571
-3.500 0.3549 0.01298 0.00417 -0.0865 0.3618 0.0587
-3.250 0.3787 0.01297 0.00413 -0.0856 0.3556 0.0603
-3.000 0.4016 0.01296 0.00411 -0.0846 0.3496 0.0618
-2.750 0.4244 0.01299 0.00411 -0.0836 0.3444 0.0635
-2.500 0.4483 0.01299 0.00410 -0.0827 0.3406 0.0654
-2.250 0.4714 0.01299 0.00408 -0.0817 0.3364 0.0675
-2.000 0.4938 0.01301 0.00409 -0.0807 0.3322 0.0699
-1.750 0.5154 0.01308 0.00411 -0.0794 0.3280 0.0723
-1.500 0.5360 0.01310 0.00412 -0.0780 0.3245 0.0757
-1.250 0.5571 0.01309 0.00413 -0.0767 0.3221 0.0802
-1.000 0.5773 0.01304 0.00416 -0.0752 0.3197 0.0945
-0.750 0.5977 0.01305 0.00429 -0.0739 0.3171 0.1393
-0.500 0.6185 0.01315 0.00439 -0.0726 0.3144 0.1503
-0.250 0.6390 0.01326 0.00450 -0.0713 0.3120 0.1575
0.000 0.6597 0.01340 0.00463 -0.0700 0.3095 0.1635
0.250 0.6801 0.01357 0.00479 -0.0687 0.3070 0.1688
0.500 0.7018 0.01368 0.00492 -0.0677 0.3054 0.1759
1.000 0.7458 0.01387 0.00521 -0.0657 0.3022 0.1985
1.250 0.7659 0.01382 0.00541 -0.0646 0.3004 0.2882
1.750 0.8820 0.01294 0.00629 -0.0782 0.2949 1.0000
2.000 0.8996 0.01315 0.00646 -0.0765 0.2932 1.0000
2.250 0.9172 0.01338 0.00666 -0.0748 0.2914 1.0000
2.500 0.9348 0.01364 0.00688 -0.0731 0.2897 1.0000
2.750 0.9528 0.01391 0.00712 -0.0716 0.2880 1.0000
3.000 0.9731 0.01411 0.00731 -0.0705 0.2871 1.0000
3.250 0.9933 0.01433 0.00753 -0.0694 0.2861 1.0000
3.500 1.0134 0.01455 0.00776 -0.0683 0.2849 1.0000
3.750 1.0336 0.01480 0.00800 -0.0672 0.2838 1.0000
4.000 1.0538 0.01505 0.00825 -0.0662 0.2824 1.0000
4.250 1.0737 0.01532 0.00852 -0.0652 0.2809 1.0000
4.500 1.0933 0.01560 0.00880 -0.0642 0.2791 1.0000
4.750 1.1127 0.01590 0.00909 -0.0632 0.2775 1.0000
5.000 1.1314 0.01624 0.00940 -0.0621 0.2750 1.0000
5.250 1.1484 0.01666 0.00978 -0.0608 0.2716 1.0000
5.500 1.1682 0.01697 0.01010 -0.0600 0.2695 1.0000
5.750 1.1888 0.01726 0.01042 -0.0593 0.2677 1.0000
6.000 1.2086 0.01759 0.01077 -0.0585 0.2658 1.0000
6.250 1.2281 0.01795 0.01114 -0.0577 0.2642 1.0000
6.500 1.2474 0.01833 0.01154 -0.0570 0.2628 1.0000
6.750 1.2662 0.01873 0.01196 -0.0562 0.2612 1.0000
7.000 1.2847 0.01917 0.01240 -0.0554 0.2597 1.0000
7.250 1.3029 0.01963 0.01286 -0.0546 0.2582 1.0000
7.500 1.3201 0.02014 0.01338 -0.0538 0.2564 1.0000
7.750 1.3369 0.02070 0.01394 -0.0529 0.2546 1.0000
8.000 1.3561 0.02114 0.01442 -0.0524 0.2532 1.0000
8.250 1.3751 0.02159 0.01493 -0.0518 0.2518 1.0000
8.500 1.3937 0.02207 0.01545 -0.0513 0.2496 1.0000
8.750 1.4114 0.02261 0.01603 -0.0507 0.2474 1.0000
9.000 1.4283 0.02320 0.01664 -0.0501 0.2449 1.0000
9.250 1.4446 0.02384 0.01731 -0.0494 0.2428 1.0000
9.500 1.4599 0.02456 0.01804 -0.0487 0.2407 1.0000
9.750 1.4751 0.02529 0.01879 -0.0481 0.2386 1.0000
10.000 1.4929 0.02589 0.01945 -0.0477 0.2369 1.0000
10.250 1.5098 0.02654 0.02016 -0.0472 0.2349 1.0000
10.500 1.5262 0.02723 0.02091 -0.0468 0.2328 1.0000
10.750 1.5412 0.02803 0.02175 -0.0463 0.2300 1.0000
11.000 1.5541 0.02899 0.02273 -0.0457 0.2266 1.0000
11.250 1.5666 0.02999 0.02375 -0.0450 0.2236 1.0000
11.500 1.5817 0.03083 0.02465 -0.0447 0.2199 1.0000
11.750 1.5955 0.03177 0.02564 -0.0442 0.2162 1.0000
12.000 1.6045 0.03311 0.02700 -0.0436 0.2109 1.0000
12.250 1.6159 0.03428 0.02821 -0.0431 0.2049 1.0000
12.750 1.6274 0.03764 0.03157 -0.0418 0.1870 1.0000
13.000 1.6267 0.03995 0.03386 -0.0409 0.1744 1.0000
13.250 1.6099 0.04385 0.03765 -0.0395 0.1516 1.0000
13.500 1.5845 0.04875 0.04246 -0.0380 0.1307 1.0000
13.750 1.5701 0.05278 0.04651 -0.0373 0.1208 1.0000
14.000 1.5558 0.05695 0.05071 -0.0368 0.1133 1.0000
14.250 1.5467 0.06068 0.05451 -0.0366 0.1085 1.0000
14.500 1.5348 0.06487 0.05876 -0.0366 0.1041 1.0000
14.750 1.5207 0.06945 0.06343 -0.0367 0.1004 1.0000
15.000 1.5071 0.07413 0.06821 -0.0371 0.0960 1.0000
15.250 1.4843 0.08018 0.07435 -0.0378 0.0914 1.0000
15.500 1.4684 0.08545 0.07974 -0.0386 0.0874 1.0000
15.750 1.4407 0.09247 0.08685 -0.0398 0.0802 1.0000
16.000 1.4099 0.10005 0.09450 -0.0413 0.0724 1.0000
|
Polar data table (+)
Polar graphs
<< Back to Rhode St. Genese 36 (rhodesg36-il)