MH 83 13.29% (mh83-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: MH 83 13.29% (mh83-il) Reynolds number: 1,000,000 Max Cl/Cd: 123.91 at α=8.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-mh83-il-1000000-n5.txt Download as CSV file: xf-mh83-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: MH 83 13.29%
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
------ -------- --------- --------- -------- -------- --------
-9.750 -0.6117 0.03272 0.02931 -0.0583 0.6221 0.0078
-9.500 -0.5982 0.02859 0.02482 -0.0615 0.6125 0.0079
-9.250 -0.5784 0.02617 0.02212 -0.0628 0.6016 0.0079
-9.000 -0.5563 0.02427 0.01997 -0.0637 0.5911 0.0079
-8.750 -0.5325 0.02276 0.01823 -0.0642 0.5800 0.0080
-8.500 -0.5101 0.02053 0.01568 -0.0649 0.5701 0.0081
-8.250 -0.4852 0.01911 0.01402 -0.0652 0.5597 0.0082
-8.000 -0.4591 0.01805 0.01280 -0.0653 0.5492 0.0083
-7.750 -0.4323 0.01723 0.01182 -0.0654 0.5393 0.0084
-7.500 -0.4051 0.01654 0.01099 -0.0654 0.5287 0.0084
-7.250 -0.3776 0.01591 0.01024 -0.0654 0.5191 0.0085
-6.750 -0.3218 0.01483 0.00892 -0.0653 0.4997 0.0087
-6.500 -0.2936 0.01435 0.00833 -0.0653 0.4899 0.0088
-6.250 -0.2653 0.01388 0.00776 -0.0652 0.4810 0.0089
-6.000 -0.2369 0.01345 0.00722 -0.0652 0.4729 0.0091
-5.750 -0.2083 0.01305 0.00673 -0.0651 0.4641 0.0092
-5.500 -0.1797 0.01271 0.00629 -0.0651 0.4552 0.0094
-5.250 -0.1509 0.01239 0.00589 -0.0650 0.4462 0.0096
-5.000 -0.1221 0.01210 0.00550 -0.0650 0.4386 0.0099
-4.750 -0.0931 0.01180 0.00513 -0.0649 0.4313 0.0101
-4.250 -0.0351 0.01129 0.00447 -0.0648 0.4168 0.0104
-4.000 -0.0060 0.01102 0.00411 -0.0648 0.4083 0.0106
-3.750 0.0231 0.01070 0.00374 -0.0648 0.4012 0.0109
-3.500 0.0523 0.01051 0.00349 -0.0648 0.3937 0.0113
-3.250 0.0815 0.01035 0.00328 -0.0648 0.3877 0.0116
-3.000 0.1108 0.01020 0.00309 -0.0648 0.3814 0.0120
-2.750 0.1400 0.01008 0.00291 -0.0648 0.3749 0.0123
-2.500 0.1694 0.00995 0.00274 -0.0647 0.3694 0.0128
-2.250 0.1986 0.00986 0.00260 -0.0647 0.3628 0.0131
-2.000 0.2279 0.00976 0.00245 -0.0647 0.3563 0.0137
-1.750 0.2572 0.00966 0.00233 -0.0647 0.3508 0.0146
-1.500 0.2865 0.00960 0.00223 -0.0647 0.3452 0.0158
-1.250 0.3158 0.00955 0.00214 -0.0647 0.3401 0.0174
-1.000 0.3451 0.00948 0.00207 -0.0647 0.3358 0.0202
-0.750 0.3744 0.00938 0.00199 -0.0647 0.3308 0.0322
-0.250 0.4327 0.00920 0.00193 -0.0648 0.3211 0.0840
0.000 0.4619 0.00910 0.00192 -0.0649 0.3165 0.1156
0.250 0.4910 0.00902 0.00192 -0.0650 0.3121 0.1581
0.500 0.5201 0.00895 0.00195 -0.0651 0.3082 0.2018
0.750 0.5492 0.00888 0.00198 -0.0652 0.3052 0.2439
1.000 0.5783 0.00881 0.00202 -0.0653 0.3016 0.2910
1.250 0.6073 0.00879 0.00207 -0.0654 0.2975 0.3306
1.500 0.6362 0.00881 0.00213 -0.0654 0.2931 0.3684
1.750 0.6652 0.00876 0.00219 -0.0655 0.2905 0.4151
2.000 0.6941 0.00871 0.00226 -0.0656 0.2876 0.4707
2.250 0.7229 0.00867 0.00235 -0.0657 0.2846 0.5323
2.500 0.7512 0.00855 0.00246 -0.0657 0.2815 0.6339
2.750 0.7785 0.00838 0.00259 -0.0655 0.2781 0.7575
3.000 0.8050 0.00798 0.00266 -0.0648 0.2759 1.0000
3.250 0.8339 0.00809 0.00273 -0.0649 0.2733 1.0000
3.500 0.8627 0.00821 0.00282 -0.0649 0.2706 1.0000
3.750 0.8914 0.00834 0.00292 -0.0649 0.2679 1.0000
4.000 0.9200 0.00849 0.00303 -0.0650 0.2652 1.0000
4.250 0.9485 0.00865 0.00315 -0.0650 0.2623 1.0000
4.500 0.9772 0.00876 0.00325 -0.0651 0.2605 1.0000
4.750 1.0058 0.00889 0.00336 -0.0651 0.2582 1.0000
5.000 1.0342 0.00903 0.00348 -0.0652 0.2560 1.0000
5.250 1.0625 0.00918 0.00361 -0.0652 0.2537 1.0000
5.500 1.0907 0.00935 0.00376 -0.0653 0.2511 1.0000
5.750 1.1187 0.00953 0.00392 -0.0653 0.2481 1.0000
6.000 1.1469 0.00968 0.00406 -0.0654 0.2464 1.0000
6.250 1.1750 0.00982 0.00421 -0.0654 0.2447 1.0000
6.500 1.2030 0.00997 0.00437 -0.0654 0.2429 1.0000
6.750 1.2309 0.01014 0.00453 -0.0655 0.2407 1.0000
7.000 1.2586 0.01032 0.00471 -0.0655 0.2381 1.0000
7.250 1.2860 0.01053 0.00490 -0.0655 0.2354 1.0000
7.500 1.3133 0.01075 0.00512 -0.0655 0.2329 1.0000
7.750 1.3408 0.01091 0.00530 -0.0656 0.2317 1.0000
8.000 1.3683 0.01108 0.00549 -0.0656 0.2300 1.0000
8.250 1.3955 0.01127 0.00569 -0.0656 0.2277 1.0000
8.500 1.4225 0.01148 0.00590 -0.0656 0.2252 1.0000
8.750 1.4492 0.01170 0.00614 -0.0655 0.2230 1.0000
9.000 1.4755 0.01196 0.00640 -0.0655 0.2204 1.0000
9.250 1.5019 0.01220 0.00665 -0.0654 0.2181 1.0000
9.500 1.5285 0.01240 0.00688 -0.0654 0.2163 1.0000
9.750 1.5548 0.01262 0.00713 -0.0653 0.2141 1.0000
10.000 1.5807 0.01287 0.00740 -0.0653 0.2114 1.0000
10.250 1.6060 0.01316 0.00770 -0.0651 0.2085 1.0000
10.500 1.6308 0.01350 0.00804 -0.0649 0.2054 1.0000
10.750 1.6562 0.01374 0.00832 -0.0648 0.2033 1.0000
11.000 1.6813 0.01401 0.00863 -0.0647 0.2008 1.0000
11.250 1.7056 0.01432 0.00896 -0.0644 0.1975 1.0000
11.500 1.7289 0.01470 0.00935 -0.0641 0.1941 1.0000
11.750 1.7520 0.01508 0.00974 -0.0638 0.1907 1.0000
12.000 1.7753 0.01541 0.01012 -0.0635 0.1871 1.0000
12.250 1.7969 0.01585 0.01057 -0.0630 0.1824 1.0000
12.500 1.8171 0.01636 0.01108 -0.0623 0.1780 1.0000
12.750 1.8376 0.01680 0.01155 -0.0617 0.1735 1.0000
13.000 1.8547 0.01742 0.01217 -0.0608 0.1679 1.0000
13.250 1.8713 0.01801 0.01278 -0.0598 0.1636 1.0000
13.500 1.8845 0.01862 0.01343 -0.0582 0.1592 1.0000
13.750 1.8876 0.01955 0.01438 -0.0556 0.1547 1.0000
14.000 1.8937 0.02053 0.01541 -0.0537 0.1509 1.0000
14.250 1.8943 0.02205 0.01693 -0.0519 0.1439 1.0000
14.500 1.8959 0.02372 0.01863 -0.0506 0.1383 1.0000
14.750 1.8917 0.02604 0.02095 -0.0495 0.1307 1.0000
15.000 1.8907 0.02830 0.02325 -0.0488 0.1251 1.0000
15.250 1.8823 0.03140 0.02637 -0.0483 0.1186 1.0000
15.500 1.8777 0.03432 0.02935 -0.0481 0.1137 1.0000
15.750 1.8646 0.03826 0.03333 -0.0482 0.1081 1.0000
16.000 1.8521 0.04230 0.03743 -0.0486 0.1030 1.0000
16.250 1.8397 0.04648 0.04168 -0.0491 0.0995 1.0000
16.500 1.8205 0.05161 0.04689 -0.0501 0.0956 1.0000
16.750 1.7989 0.05730 0.05265 -0.0514 0.0907 1.0000
17.000 1.7795 0.06300 0.05843 -0.0530 0.0877 1.0000
17.250 1.7608 0.06879 0.06432 -0.0548 0.0854 1.0000
17.500 1.7418 0.07484 0.07046 -0.0568 0.0821 1.0000
17.750 1.7212 0.08122 0.07693 -0.0590 0.0794 1.0000
18.250 1.6800 0.09461 0.09050 -0.0641 0.0741 1.0000
18.500 1.6607 0.10133 0.09730 -0.0669 0.0712 1.0000
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