NACA 63-415 AIRFOIL (n63415-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 63-415 AIRFOIL (n63415-il) Reynolds number: 1,000,000 Max Cl/Cd: 102.95 at α=4.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-n63415-il-1000000-n5.txt Download as CSV file: xf-n63415-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NACA 63-415 AIRFOIL
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
------ -------- --------- --------- -------- -------- --------
-19.750 -0.9210 0.12577 0.12323 -0.0276 1.0000 0.0095
-19.500 -0.9645 0.11353 0.11083 -0.0343 1.0000 0.0095
-19.250 -1.0022 0.10277 0.09991 -0.0402 1.0000 0.0095
-19.000 -1.0363 0.09301 0.09000 -0.0455 1.0000 0.0094
-18.750 -1.0621 0.08489 0.08173 -0.0500 1.0000 0.0095
-18.500 -1.0816 0.07809 0.07480 -0.0537 1.0000 0.0095
-18.250 -1.0979 0.07193 0.06852 -0.0571 1.0000 0.0095
-18.000 -1.1111 0.06645 0.06293 -0.0601 1.0000 0.0096
-17.750 -1.1206 0.06172 0.05809 -0.0625 1.0000 0.0096
-17.500 -1.1270 0.05751 0.05379 -0.0647 1.0000 0.0097
-17.250 -1.1326 0.05360 0.04978 -0.0666 1.0000 0.0098
-17.000 -1.1361 0.05006 0.04615 -0.0682 1.0000 0.0099
-16.750 -1.1374 0.04692 0.04291 -0.0695 1.0000 0.0100
-16.500 -1.1378 0.04405 0.03996 -0.0706 1.0000 0.0101
-16.250 -1.1370 0.04138 0.03721 -0.0715 1.0000 0.0102
-16.000 -1.1342 0.03901 0.03475 -0.0722 1.0000 0.0104
-15.750 -1.1314 0.03667 0.03234 -0.0728 1.0000 0.0105
-15.500 -1.1255 0.03474 0.03033 -0.0731 1.0000 0.0107
-15.250 -1.1207 0.03275 0.02825 -0.0734 1.0000 0.0107
-15.000 -1.1126 0.03113 0.02658 -0.0735 1.0000 0.0110
-14.750 -1.1071 0.02932 0.02470 -0.0735 1.0000 0.0111
-14.500 -1.1013 0.02763 0.02295 -0.0733 1.0000 0.0114
-14.250 -1.0929 0.02622 0.02150 -0.0729 1.0000 0.0116
-14.000 -1.0841 0.02492 0.02015 -0.0724 1.0000 0.0118
-13.750 -1.0746 0.02376 0.01894 -0.0717 1.0000 0.0120
-13.500 -1.0657 0.02265 0.01778 -0.0708 1.0000 0.0122
-13.250 -1.0568 0.02168 0.01676 -0.0696 1.0000 0.0125
-13.000 -1.0480 0.02076 0.01579 -0.0682 0.9911 0.0127
-12.750 -1.0101 0.01977 0.01474 -0.0723 0.9727 0.0130
-12.500 -0.9691 0.01883 0.01371 -0.0768 0.9544 0.0134
-12.250 -0.9408 0.01800 0.01275 -0.0787 0.9254 0.0138
-12.000 -0.9279 0.01745 0.01209 -0.0772 0.9000 0.0142
-11.750 -0.9117 0.01695 0.01149 -0.0760 0.8831 0.0146
-11.500 -0.8936 0.01650 0.01096 -0.0749 0.8694 0.0151
-11.250 -0.8744 0.01607 0.01045 -0.0740 0.8575 0.0155
-11.000 -0.8539 0.01566 0.00997 -0.0733 0.8464 0.0160
-10.750 -0.8324 0.01527 0.00950 -0.0727 0.8370 0.0164
-10.250 -0.7882 0.01445 0.00857 -0.0716 0.8188 0.0175
-10.000 -0.7649 0.01412 0.00818 -0.0712 0.8103 0.0183
-9.750 -0.7407 0.01379 0.00781 -0.0710 0.8028 0.0190
-9.500 -0.7161 0.01349 0.00745 -0.0707 0.7951 0.0198
-9.250 -0.6915 0.01315 0.00707 -0.0705 0.7882 0.0205
-9.000 -0.6663 0.01285 0.00674 -0.0703 0.7807 0.0215
-8.750 -0.6408 0.01257 0.00642 -0.0702 0.7740 0.0224
-8.500 -0.6146 0.01232 0.00612 -0.0702 0.7672 0.0234
-8.250 -0.5885 0.01207 0.00581 -0.0701 0.7601 0.0244
-8.000 -0.5623 0.01178 0.00551 -0.0701 0.7539 0.0255
-7.750 -0.5356 0.01154 0.00524 -0.0701 0.7473 0.0267
-7.500 -0.5088 0.01133 0.00497 -0.0701 0.7409 0.0277
-7.250 -0.4814 0.01112 0.00473 -0.0702 0.7344 0.0286
-7.000 -0.4545 0.01087 0.00445 -0.0702 0.7277 0.0300
-6.750 -0.4271 0.01065 0.00421 -0.0703 0.7218 0.0316
-6.500 -0.3995 0.01046 0.00399 -0.0705 0.7151 0.0331
-6.250 -0.3718 0.01030 0.00378 -0.0706 0.7087 0.0342
-6.000 -0.3439 0.01008 0.00355 -0.0707 0.7030 0.0364
-5.750 -0.3160 0.00990 0.00335 -0.0709 0.6965 0.0388
-5.500 -0.2880 0.00973 0.00316 -0.0711 0.6904 0.0421
-5.250 -0.2598 0.00954 0.00298 -0.0713 0.6845 0.0470
-5.000 -0.2316 0.00935 0.00280 -0.0715 0.6782 0.0543
-4.750 -0.2035 0.00915 0.00262 -0.0717 0.6725 0.0658
-4.500 -0.1751 0.00892 0.00244 -0.0720 0.6663 0.0815
-4.250 -0.1468 0.00870 0.00228 -0.0723 0.6603 0.1024
-4.000 -0.1184 0.00844 0.00211 -0.0727 0.6550 0.1308
-3.750 -0.0899 0.00816 0.00195 -0.0730 0.6488 0.1654
-3.500 -0.0615 0.00787 0.00178 -0.0734 0.6427 0.2093
-3.250 -0.0328 0.00755 0.00162 -0.0739 0.6376 0.2597
-2.750 0.0248 0.00697 0.00137 -0.0749 0.6261 0.3663
-2.500 0.0539 0.00675 0.00131 -0.0753 0.6207 0.4160
-2.250 0.0832 0.00663 0.00127 -0.0757 0.6147 0.4469
-2.000 0.1123 0.00657 0.00124 -0.0760 0.6093 0.4734
-1.750 0.1417 0.00653 0.00123 -0.0763 0.6044 0.4887
-1.500 0.1711 0.00651 0.00122 -0.0767 0.5986 0.5027
-1.000 0.2296 0.00649 0.00122 -0.0772 0.5879 0.5247
-0.750 0.2590 0.00650 0.00122 -0.0775 0.5827 0.5321
-0.500 0.2881 0.00653 0.00123 -0.0778 0.5772 0.5388
-0.250 0.3174 0.00653 0.00124 -0.0781 0.5721 0.5461
0.000 0.3467 0.00655 0.00126 -0.0784 0.5666 0.5531
0.250 0.3758 0.00658 0.00128 -0.0786 0.5611 0.5593
0.500 0.4050 0.00661 0.00131 -0.0789 0.5558 0.5658
0.750 0.4342 0.00664 0.00134 -0.0792 0.5497 0.5713
1.250 0.4923 0.00672 0.00142 -0.0797 0.5377 0.5829
1.500 0.5212 0.00677 0.00146 -0.0799 0.5315 0.5886
1.750 0.5501 0.00682 0.00152 -0.0801 0.5257 0.5941
2.000 0.5792 0.00686 0.00158 -0.0804 0.5197 0.5999
2.250 0.6079 0.00693 0.00164 -0.0806 0.5129 0.6055
2.500 0.6367 0.00698 0.00171 -0.0808 0.5057 0.6118
2.750 0.6648 0.00709 0.00179 -0.0809 0.4943 0.6180
3.000 0.6932 0.00719 0.00187 -0.0811 0.4817 0.6234
3.250 0.7216 0.00727 0.00197 -0.0812 0.4718 0.6293
3.500 0.7494 0.00740 0.00207 -0.0813 0.4582 0.6359
3.750 0.7766 0.00759 0.00220 -0.0813 0.4362 0.6420
4.000 0.8033 0.00782 0.00235 -0.0812 0.4128 0.6484
4.250 0.8298 0.00806 0.00251 -0.0811 0.3876 0.6546
4.500 0.8535 0.00855 0.00279 -0.0806 0.3386 0.6607
4.750 0.8760 0.00914 0.00315 -0.0799 0.2858 0.6677
5.000 0.8999 0.00960 0.00345 -0.0794 0.2498 0.6741
5.250 0.9233 0.01008 0.00379 -0.0789 0.2143 0.6804
5.500 0.9464 0.01058 0.00414 -0.0783 0.1816 0.6875
5.750 0.9689 0.01110 0.00452 -0.0777 0.1488 0.6939
6.000 0.9910 0.01163 0.00491 -0.0770 0.1185 0.7011
6.250 1.0132 0.01213 0.00530 -0.0763 0.0946 0.7079
6.500 1.0360 0.01255 0.00567 -0.0756 0.0777 0.7148
6.750 1.0579 0.01302 0.00607 -0.0749 0.0620 0.7221
7.000 1.0800 0.01346 0.00645 -0.0741 0.0498 0.7285
7.250 1.1020 0.01387 0.00684 -0.0733 0.0415 0.7359
7.750 1.1459 0.01462 0.00760 -0.0718 0.0328 0.7501
8.000 1.1675 0.01498 0.00798 -0.0710 0.0305 0.7575
8.250 1.1887 0.01533 0.00837 -0.0701 0.0287 0.7652
8.500 1.2085 0.01573 0.00879 -0.0690 0.0271 0.7738
8.750 1.2274 0.01611 0.00922 -0.0677 0.0257 0.7824
9.000 1.2441 0.01647 0.00963 -0.0660 0.0246 0.7923
9.250 1.2593 0.01689 0.01010 -0.0641 0.0234 0.8032
9.500 1.2733 0.01738 0.01064 -0.0621 0.0222 0.8147
10.000 1.3022 0.01838 0.01177 -0.0585 0.0205 0.8405
10.250 1.3156 0.01895 0.01240 -0.0568 0.0194 0.8545
10.500 1.3277 0.01959 0.01311 -0.0549 0.0185 0.8709
10.750 1.3384 0.02027 0.01388 -0.0528 0.0177 0.8936
11.000 1.3467 0.02084 0.01459 -0.0502 0.0170 0.9424
11.250 1.3607 0.02161 0.01543 -0.0491 0.0161 1.0000
11.500 1.3731 0.02253 0.01637 -0.0479 0.0152 1.0000
11.750 1.3850 0.02353 0.01739 -0.0467 0.0144 1.0000
12.000 1.3972 0.02453 0.01843 -0.0456 0.0138 1.0000
12.250 1.4086 0.02563 0.01956 -0.0445 0.0131 1.0000
12.500 1.4192 0.02682 0.02079 -0.0434 0.0125 1.0000
12.750 1.4292 0.02810 0.02211 -0.0424 0.0121 1.0000
13.000 1.4385 0.02948 0.02352 -0.0415 0.0117 1.0000
13.250 1.4482 0.03085 0.02495 -0.0406 0.0114 1.0000
13.500 1.4573 0.03233 0.02648 -0.0398 0.0111 1.0000
13.750 1.4657 0.03389 0.02809 -0.0391 0.0109 1.0000
14.000 1.4734 0.03555 0.02982 -0.0384 0.0106 1.0000
14.250 1.4806 0.03731 0.03163 -0.0378 0.0104 1.0000
14.500 1.4873 0.03916 0.03354 -0.0373 0.0102 1.0000
14.750 1.4932 0.04114 0.03556 -0.0368 0.0100 1.0000
15.000 1.4981 0.04327 0.03776 -0.0365 0.0098 1.0000
15.250 1.5022 0.04557 0.04011 -0.0362 0.0096 1.0000
15.500 1.5051 0.04808 0.04268 -0.0361 0.0094 1.0000
15.750 1.5099 0.05043 0.04511 -0.0361 0.0093 1.0000
16.000 1.5141 0.05291 0.04767 -0.0362 0.0092 1.0000
16.250 1.5172 0.05559 0.05043 -0.0364 0.0091 1.0000
16.500 1.5199 0.05840 0.05332 -0.0367 0.0091 1.0000
16.750 1.5220 0.06134 0.05633 -0.0371 0.0089 1.0000
17.000 1.5231 0.06447 0.05955 -0.0377 0.0089 1.0000
17.250 1.5241 0.06771 0.06288 -0.0384 0.0088 1.0000
17.500 1.5244 0.07112 0.06637 -0.0392 0.0087 1.0000
17.750 1.5235 0.07475 0.07009 -0.0402 0.0086 1.0000
18.000 1.5218 0.07858 0.07401 -0.0414 0.0086 1.0000
18.250 1.5196 0.08258 0.07811 -0.0427 0.0085 1.0000
18.500 1.5166 0.08679 0.08241 -0.0442 0.0084 1.0000
18.750 1.5130 0.09115 0.08687 -0.0458 0.0084 1.0000
19.000 1.5085 0.09576 0.09158 -0.0477 0.0083 1.0000
19.250 1.5033 0.10054 0.09646 -0.0497 0.0082 1.0000
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