Rhode St. Genese 30 (rhodesg30-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: Rhode St. Genese 30 (rhodesg30-il) Reynolds number: 1,000,000 Max Cl/Cd: 105.36 at α=3.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-rhodesg30-il-1000000.txt Download as CSV file: xf-rhodesg30-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: Rhode St. Genese 30
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-14.500 -0.3692 0.12396 0.12235 -0.0220 1.0000 0.0126
-14.250 -0.3764 0.11771 0.11610 -0.0242 1.0000 0.0126
-10.750 -0.6869 0.02640 0.02288 -0.0658 0.9934 0.0090
-10.500 -0.6641 0.02348 0.01975 -0.0667 0.9889 0.0085
-10.250 -0.6359 0.02157 0.01764 -0.0679 0.9856 0.0085
-10.000 -0.6053 0.02006 0.01596 -0.0693 0.9829 0.0087
-9.750 -0.5780 0.01883 0.01459 -0.0697 0.9768 0.0088
-9.500 -0.5461 0.01769 0.01333 -0.0710 0.9728 0.0090
-9.250 -0.5147 0.01672 0.01225 -0.0720 0.9685 0.0091
-9.000 -0.4839 0.01612 0.01153 -0.0727 0.9614 0.0094
-8.750 -0.4524 0.01523 0.01054 -0.0737 0.9548 0.0095
-8.500 -0.4234 0.01474 0.00995 -0.0739 0.9456 0.0096
-8.250 -0.3972 0.01386 0.00899 -0.0737 0.9363 0.0097
-8.000 -0.3736 0.01280 0.00785 -0.0730 0.9269 0.0099
-7.750 -0.3508 0.01190 0.00686 -0.0721 0.9177 0.0102
-7.500 -0.3259 0.01133 0.00620 -0.0714 0.9091 0.0106
-7.250 -0.3008 0.01088 0.00565 -0.0707 0.9001 0.0109
-7.000 -0.2754 0.01046 0.00516 -0.0700 0.8920 0.0113
-6.750 -0.2494 0.01016 0.00479 -0.0694 0.8839 0.0117
-6.500 -0.2230 0.00991 0.00448 -0.0689 0.8764 0.0122
-6.250 -0.1966 0.00970 0.00421 -0.0684 0.8681 0.0125
-6.000 -0.1704 0.00945 0.00387 -0.0678 0.8595 0.0130
-5.750 -0.1447 0.00912 0.00343 -0.0672 0.8508 0.0137
-5.500 -0.1191 0.00875 0.00295 -0.0665 0.8406 0.0148
-5.250 -0.0932 0.00850 0.00260 -0.0659 0.8295 0.0158
-5.000 -0.0673 0.00826 0.00230 -0.0653 0.8171 0.0192
-4.750 -0.0406 0.00822 0.00237 -0.0649 0.8039 0.0359
-4.500 -0.0117 0.00857 0.00275 -0.0648 0.7904 0.0393
-4.250 0.0187 0.00931 0.00350 -0.0650 0.7761 0.0404
-4.000 0.0441 0.00904 0.00318 -0.0645 0.7608 0.0424
-3.750 0.0715 0.00921 0.00333 -0.0642 0.7444 0.0436
-3.500 0.0983 0.00928 0.00336 -0.0639 0.7268 0.0447
-3.250 0.1249 0.00934 0.00336 -0.0635 0.7084 0.0459
-3.000 0.1516 0.00950 0.00344 -0.0631 0.6890 0.0473
-2.750 0.1777 0.00948 0.00334 -0.0626 0.6691 0.0479
-2.500 0.2052 0.01002 0.00378 -0.0624 0.6465 0.0489
-2.250 0.2305 0.00975 0.00343 -0.0618 0.6241 0.0488
-2.000 0.2548 0.00922 0.00282 -0.0610 0.5997 0.0492
-1.750 0.2778 0.00880 0.00227 -0.0600 0.5655 0.0504
-1.500 0.3013 0.00881 0.00209 -0.0592 0.5103 0.0514
-1.250 0.3237 0.00905 0.00205 -0.0581 0.4393 0.0521
-1.000 0.3484 0.00916 0.00201 -0.0575 0.4044 0.0529
-0.750 0.3740 0.00920 0.00197 -0.0571 0.3842 0.0535
-0.500 0.4000 0.00923 0.00194 -0.0567 0.3703 0.0541
-0.250 0.4265 0.00923 0.00190 -0.0563 0.3606 0.0546
0.000 0.4529 0.00924 0.00188 -0.0560 0.3523 0.0550
0.250 0.4795 0.00924 0.00187 -0.0558 0.3457 0.0556
0.500 0.5060 0.00927 0.00188 -0.0555 0.3390 0.0561
0.750 0.5327 0.00928 0.00188 -0.0552 0.3322 0.0567
1.000 0.5591 0.00934 0.00191 -0.0549 0.3263 0.0575
1.250 0.5861 0.00935 0.00194 -0.0547 0.3222 0.0585
1.500 0.6127 0.00938 0.00196 -0.0545 0.3162 0.0601
1.750 0.6390 0.00944 0.00200 -0.0542 0.3110 0.0640
2.000 0.6660 0.00945 0.00205 -0.0540 0.3076 0.0696
2.250 0.6918 0.00931 0.00214 -0.0537 0.3026 0.1804
2.500 0.7585 0.00764 0.00247 -0.0631 0.2931 1.0000
2.750 0.7832 0.00774 0.00255 -0.0625 0.2873 1.0000
3.000 0.8073 0.00789 0.00266 -0.0618 0.2804 1.0000
3.250 0.8323 0.00798 0.00275 -0.0613 0.2731 1.0000
3.500 0.8566 0.00813 0.00286 -0.0606 0.2622 1.0000
3.750 0.8798 0.00836 0.00298 -0.0598 0.2383 1.0000
4.000 0.8920 0.00949 0.00357 -0.0572 0.1343 1.0000
4.250 0.9099 0.01021 0.00403 -0.0556 0.0874 1.0000
4.500 0.9279 0.01096 0.00453 -0.0540 0.0452 1.0000
4.750 0.9511 0.01124 0.00483 -0.0532 0.0417 1.0000
5.000 0.9744 0.01151 0.00513 -0.0524 0.0402 1.0000
5.250 0.9974 0.01181 0.00545 -0.0516 0.0384 1.0000
5.500 1.0198 0.01217 0.00582 -0.0507 0.0365 1.0000
5.750 1.0414 0.01260 0.00628 -0.0497 0.0341 1.0000
6.000 1.0621 0.01309 0.00685 -0.0486 0.0324 1.0000
6.250 1.0853 0.01335 0.00713 -0.0479 0.0318 1.0000
6.500 1.1079 0.01365 0.00746 -0.0472 0.0309 1.0000
6.750 1.1301 0.01398 0.00782 -0.0464 0.0297 1.0000
7.000 1.1517 0.01435 0.00821 -0.0455 0.0285 1.0000
7.250 1.1725 0.01476 0.00864 -0.0445 0.0272 1.0000
7.500 1.1877 0.01558 0.00952 -0.0427 0.0250 1.0000
7.750 1.2088 0.01593 0.00991 -0.0418 0.0243 1.0000
8.000 1.2316 0.01614 0.01013 -0.0412 0.0233 1.0000
8.250 1.2527 0.01645 0.01047 -0.0403 0.0221 1.0000
8.500 1.2739 0.01674 0.01075 -0.0395 0.0208 1.0000
8.750 1.2887 0.01743 0.01145 -0.0377 0.0190 1.0000
9.000 1.3080 0.01778 0.01185 -0.0366 0.0181 1.0000
9.250 1.3276 0.01805 0.01214 -0.0355 0.0169 1.0000
9.500 1.3445 0.01840 0.01247 -0.0340 0.0157 1.0000
9.750 1.3533 0.01913 0.01322 -0.0312 0.0143 1.0000
10.000 1.3665 0.01967 0.01382 -0.0292 0.0137 1.0000
10.250 1.3800 0.02023 0.01442 -0.0274 0.0129 1.0000
10.500 1.3928 0.02083 0.01507 -0.0256 0.0122 1.0000
10.750 1.4028 0.02162 0.01588 -0.0235 0.0115 1.0000
11.000 1.4030 0.02304 0.01739 -0.0205 0.0106 1.0000
11.250 1.4156 0.02378 0.01818 -0.0191 0.0103 1.0000
11.500 1.4237 0.02484 0.01932 -0.0174 0.0100 1.0000
11.750 1.4315 0.02598 0.02053 -0.0158 0.0095 1.0000
12.000 1.4390 0.02720 0.02181 -0.0144 0.0091 1.0000
12.250 1.4442 0.02867 0.02336 -0.0131 0.0089 1.0000
12.500 1.4452 0.03058 0.02534 -0.0117 0.0083 1.0000
12.750 1.4394 0.03324 0.02812 -0.0103 0.0080 1.0000
13.000 1.4351 0.03599 0.03098 -0.0095 0.0079 1.0000
13.250 1.4342 0.03858 0.03368 -0.0092 0.0077 1.0000
13.500 1.4334 0.04131 0.03652 -0.0091 0.0076 1.0000
13.750 1.4326 0.04417 0.03949 -0.0093 0.0075 1.0000
14.000 1.4290 0.04748 0.04290 -0.0097 0.0074 1.0000
14.250 1.4260 0.05087 0.04640 -0.0103 0.0072 1.0000
14.500 1.4215 0.05458 0.05022 -0.0112 0.0071 1.0000
14.750 1.4153 0.05866 0.05440 -0.0123 0.0069 1.0000
15.000 1.4087 0.06295 0.05881 -0.0137 0.0068 1.0000
15.250 1.3994 0.06776 0.06372 -0.0154 0.0067 1.0000
15.500 1.3886 0.07288 0.06896 -0.0172 0.0066 1.0000
15.750 1.3810 0.07764 0.07381 -0.0190 0.0065 1.0000
16.000 1.3667 0.08342 0.07972 -0.0211 0.0066 1.0000
16.250 1.3578 0.08848 0.08488 -0.0232 0.0065 1.0000
16.500 1.3490 0.09362 0.09009 -0.0253 0.0064 1.0000
16.750 1.3359 0.09948 0.09606 -0.0277 0.0063 1.0000
17.000 1.3258 0.10495 0.10161 -0.0301 0.0062 1.0000
17.250 1.3135 0.11088 0.10765 -0.0328 0.0062 1.0000
17.500 1.3042 0.11642 0.11327 -0.0353 0.0061 1.0000
17.750 1.2902 0.12288 0.11983 -0.0384 0.0060 1.0000
18.000 1.2810 0.12860 0.12564 -0.0413 0.0060 1.0000
18.250 1.2694 0.13490 0.13204 -0.0445 0.0059 1.0000
18.500 1.2555 0.14180 0.13905 -0.0481 0.0058 1.0000
18.750 1.2410 0.14893 0.14629 -0.0520 0.0057 1.0000
19.000 1.2326 0.15504 0.15250 -0.0555 0.0057 1.0000
19.250 1.2152 0.16329 0.16089 -0.0602 0.0057 1.0000
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Polar data table (+)
Polar graphs
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