NACA 65(2)-415 (naca652415-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 65(2)-415 (naca652415-il) Reynolds number: 1,000,000 Max Cl/Cd: 105.92 at α=3.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca652415-il-1000000-n5.txt Download as CSV file: xf-naca652415-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NACA 65(2)-415
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
------ -------- --------- --------- -------- -------- --------
-18.500 -1.0231 0.07641 0.07356 -0.0675 1.0000 0.0088
-18.250 -1.0473 0.06866 0.06565 -0.0720 1.0000 0.0089
-18.000 -1.0645 0.06248 0.05934 -0.0755 1.0000 0.0089
-17.750 -1.0764 0.05749 0.05423 -0.0781 1.0000 0.0090
-17.500 -1.0852 0.05320 0.04982 -0.0800 1.0000 0.0090
-17.250 -1.0906 0.04957 0.04609 -0.0815 1.0000 0.0092
-17.000 -1.0915 0.04667 0.04311 -0.0825 1.0000 0.0092
-16.750 -1.0902 0.04414 0.04051 -0.0832 1.0000 0.0094
-16.500 -1.0901 0.04162 0.03790 -0.0837 1.0000 0.0095
-16.250 -1.0861 0.03959 0.03581 -0.0839 1.0000 0.0097
-16.000 -1.0835 0.03747 0.03361 -0.0840 1.0000 0.0098
-15.750 -1.0768 0.03583 0.03189 -0.0839 1.0000 0.0100
-15.500 -1.0728 0.03398 0.02995 -0.0837 1.0000 0.0100
-15.250 -1.0647 0.03256 0.02847 -0.0834 1.0000 0.0103
-15.000 -1.0563 0.03121 0.02705 -0.0830 1.0000 0.0105
-14.750 -1.0501 0.02972 0.02548 -0.0823 1.0000 0.0107
-14.500 -1.0401 0.02861 0.02430 -0.0816 1.0000 0.0109
-14.250 -1.0319 0.02741 0.02303 -0.0807 1.0000 0.0110
-14.000 -1.0250 0.02627 0.02181 -0.0792 0.9916 0.0111
-13.750 -0.9979 0.02482 0.02028 -0.0823 0.9780 0.0115
-13.500 -0.9632 0.02361 0.01899 -0.0863 0.9684 0.0117
-13.250 -0.9266 0.02256 0.01788 -0.0903 0.9584 0.0120
-13.000 -0.8914 0.02173 0.01696 -0.0938 0.9450 0.0123
-12.750 -0.8663 0.02101 0.01614 -0.0950 0.9262 0.0126
-12.500 -0.8496 0.02040 0.01541 -0.0944 0.9083 0.0129
-12.250 -0.8361 0.01976 0.01465 -0.0931 0.8933 0.0132
-12.000 -0.8223 0.01919 0.01398 -0.0917 0.8807 0.0134
-11.750 -0.8092 0.01858 0.01327 -0.0902 0.8691 0.0136
-11.500 -0.7942 0.01810 0.01270 -0.0888 0.8591 0.0138
-11.250 -0.7794 0.01767 0.01217 -0.0873 0.8492 0.0140
-11.000 -0.7687 0.01704 0.01146 -0.0852 0.8391 0.0143
-10.750 -0.7573 0.01657 0.01092 -0.0830 0.8304 0.0147
-10.500 -0.7406 0.01612 0.01041 -0.0817 0.8226 0.0149
-10.250 -0.7217 0.01573 0.00996 -0.0807 0.8158 0.0152
-10.000 -0.7013 0.01538 0.00956 -0.0799 0.8087 0.0155
-9.500 -0.6591 0.01470 0.00876 -0.0784 0.7952 0.0162
-9.250 -0.6377 0.01433 0.00833 -0.0777 0.7888 0.0165
-9.000 -0.6151 0.01402 0.00796 -0.0772 0.7833 0.0169
-8.750 -0.5923 0.01369 0.00757 -0.0767 0.7772 0.0172
-8.500 -0.5696 0.01336 0.00717 -0.0761 0.7711 0.0174
-8.250 -0.5470 0.01296 0.00672 -0.0756 0.7655 0.0177
-8.000 -0.5241 0.01257 0.00630 -0.0751 0.7594 0.0183
-7.750 -0.5000 0.01229 0.00598 -0.0748 0.7540 0.0188
-7.500 -0.4752 0.01202 0.00568 -0.0746 0.7492 0.0193
-7.250 -0.4502 0.01175 0.00537 -0.0744 0.7439 0.0197
-7.000 -0.4252 0.01150 0.00507 -0.0741 0.7385 0.0201
-6.750 -0.3995 0.01126 0.00479 -0.0740 0.7338 0.0206
-6.500 -0.3736 0.01104 0.00454 -0.0740 0.7288 0.0210
-6.250 -0.3475 0.01085 0.00430 -0.0739 0.7240 0.0214
-6.000 -0.3218 0.01057 0.00398 -0.0738 0.7200 0.0222
-5.750 -0.2954 0.01033 0.00374 -0.0738 0.7157 0.0231
-5.500 -0.2687 0.01014 0.00352 -0.0738 0.7110 0.0239
-5.250 -0.2419 0.00997 0.00332 -0.0738 0.7066 0.0248
-5.000 -0.2147 0.00981 0.00314 -0.0740 0.7026 0.0258
-4.750 -0.1873 0.00964 0.00296 -0.0741 0.6986 0.0268
-4.500 -0.1601 0.00947 0.00278 -0.0742 0.6946 0.0291
-4.250 -0.1327 0.00933 0.00262 -0.0743 0.6907 0.0314
-4.000 -0.1050 0.00918 0.00248 -0.0745 0.6872 0.0347
-3.750 -0.0772 0.00903 0.00234 -0.0747 0.6832 0.0393
-3.500 -0.0496 0.00886 0.00220 -0.0749 0.6791 0.0506
-3.250 -0.0224 0.00864 0.00205 -0.0751 0.6755 0.0749
-3.000 0.0048 0.00835 0.00190 -0.0753 0.6723 0.1164
-2.750 0.0319 0.00795 0.00174 -0.0756 0.6690 0.1842
-2.500 0.0586 0.00743 0.00155 -0.0760 0.6654 0.2818
-2.250 0.0851 0.00682 0.00133 -0.0765 0.6616 0.4000
-1.750 0.1408 0.00618 0.00124 -0.0772 0.6552 0.5737
-1.500 0.1698 0.00615 0.00126 -0.0776 0.6520 0.6000
-1.250 0.1988 0.00614 0.00127 -0.0779 0.6488 0.6134
-1.000 0.2278 0.00616 0.00126 -0.0782 0.6455 0.6178
-0.500 0.2858 0.00618 0.00126 -0.0789 0.6393 0.6243
-0.250 0.3150 0.00619 0.00127 -0.0793 0.6363 0.6276
0.000 0.3441 0.00621 0.00128 -0.0797 0.6332 0.6308
0.500 0.4017 0.00627 0.00132 -0.0803 0.6269 0.6370
0.750 0.4308 0.00628 0.00135 -0.0807 0.6242 0.6402
1.000 0.4599 0.00630 0.00138 -0.0810 0.6213 0.6436
1.250 0.4889 0.00633 0.00142 -0.0814 0.6181 0.6472
1.500 0.5177 0.00637 0.00146 -0.0817 0.6148 0.6503
1.750 0.5462 0.00641 0.00151 -0.0820 0.6117 0.6537
2.000 0.5750 0.00643 0.00156 -0.0823 0.6077 0.6571
2.250 0.6036 0.00647 0.00161 -0.0825 0.6016 0.6609
2.500 0.6315 0.00655 0.00167 -0.0827 0.5947 0.6646
2.750 0.6599 0.00658 0.00173 -0.0829 0.5862 0.6681
3.000 0.6872 0.00666 0.00180 -0.0829 0.5722 0.6718
3.250 0.7141 0.00677 0.00187 -0.0829 0.5545 0.6756
3.500 0.7393 0.00698 0.00198 -0.0825 0.5250 0.6795
3.750 0.7613 0.00739 0.00216 -0.0817 0.4729 0.6834
4.000 0.7767 0.00822 0.00258 -0.0797 0.3800 0.6876
4.250 0.7918 0.00909 0.00307 -0.0778 0.2955 0.6921
4.500 0.8084 0.00983 0.00350 -0.0761 0.2280 0.6964
4.750 0.8261 0.01047 0.00389 -0.0746 0.1751 0.7002
5.000 0.8437 0.01106 0.00429 -0.0731 0.1290 0.7046
5.250 0.8608 0.01165 0.00470 -0.0715 0.0884 0.7095
5.500 0.8795 0.01213 0.00506 -0.0701 0.0629 0.7144
5.750 0.8983 0.01256 0.00542 -0.0688 0.0449 0.7192
6.000 0.9179 0.01293 0.00576 -0.0675 0.0348 0.7244
6.250 0.9372 0.01324 0.00606 -0.0662 0.0302 0.7295
6.500 0.9546 0.01354 0.00637 -0.0645 0.0268 0.7344
6.750 0.9729 0.01384 0.00670 -0.0630 0.0249 0.7399
7.000 0.9905 0.01418 0.00706 -0.0615 0.0230 0.7459
7.250 1.0075 0.01457 0.00747 -0.0598 0.0211 0.7518
7.500 1.0254 0.01491 0.00786 -0.0584 0.0201 0.7586
7.750 1.0425 0.01532 0.00829 -0.0569 0.0188 0.7652
8.000 1.0585 0.01577 0.00878 -0.0553 0.0175 0.7718
8.250 1.0750 0.01622 0.00927 -0.0538 0.0167 0.7790
8.500 1.0916 0.01668 0.00977 -0.0524 0.0158 0.7858
8.750 1.1075 0.01719 0.01032 -0.0509 0.0152 0.7939
9.000 1.1230 0.01773 0.01091 -0.0495 0.0145 0.8017
9.250 1.1371 0.01837 0.01159 -0.0479 0.0139 0.8111
9.500 1.1518 0.01898 0.01226 -0.0464 0.0135 0.8198
9.750 1.1671 0.01959 0.01294 -0.0451 0.0132 0.8292
10.000 1.1814 0.02026 0.01367 -0.0436 0.0129 0.8386
10.250 1.1954 0.02097 0.01445 -0.0422 0.0126 0.8491
10.500 1.2089 0.02170 0.01525 -0.0408 0.0122 0.8615
10.750 1.2212 0.02249 0.01613 -0.0393 0.0120 0.8759
11.000 1.2334 0.02327 0.01699 -0.0377 0.0117 0.8932
11.250 1.2435 0.02412 0.01793 -0.0359 0.0115 0.9156
11.500 1.2539 0.02498 0.01892 -0.0342 0.0112 0.9534
11.750 1.2667 0.02613 0.02013 -0.0335 0.0109 1.0000
12.000 1.2775 0.02732 0.02136 -0.0324 0.0108 1.0000
12.250 1.2900 0.02838 0.02248 -0.0314 0.0107 1.0000
12.500 1.3014 0.02957 0.02371 -0.0305 0.0106 1.0000
12.750 1.3131 0.03075 0.02495 -0.0296 0.0104 1.0000
13.000 1.3236 0.03203 0.02629 -0.0287 0.0103 1.0000
13.250 1.3341 0.03335 0.02767 -0.0279 0.0102 1.0000
13.500 1.3444 0.03472 0.02909 -0.0271 0.0100 1.0000
13.750 1.3548 0.03610 0.03053 -0.0264 0.0099 1.0000
14.000 1.3635 0.03767 0.03215 -0.0257 0.0097 1.0000
14.250 1.3727 0.03923 0.03377 -0.0250 0.0096 1.0000
14.500 1.3809 0.04092 0.03553 -0.0244 0.0095 1.0000
14.750 1.3891 0.04265 0.03733 -0.0239 0.0094 1.0000
15.000 1.3965 0.04449 0.03923 -0.0235 0.0093 1.0000
15.250 1.4035 0.04641 0.04122 -0.0231 0.0092 1.0000
15.500 1.4105 0.04839 0.04325 -0.0228 0.0091 1.0000
15.750 1.4162 0.05056 0.04549 -0.0225 0.0090 1.0000
16.000 1.4211 0.05284 0.04785 -0.0224 0.0089 1.0000
16.250 1.4250 0.05529 0.05037 -0.0223 0.0088 1.0000
16.500 1.4278 0.05794 0.05310 -0.0223 0.0087 1.0000
16.750 1.4293 0.06083 0.05607 -0.0225 0.0086 1.0000
17.000 1.4288 0.06403 0.05937 -0.0228 0.0085 1.0000
17.250 1.4274 0.06742 0.06285 -0.0232 0.0084 1.0000
17.500 1.4247 0.07108 0.06662 -0.0238 0.0083 1.0000
17.750 1.4251 0.07445 0.07008 -0.0246 0.0083 1.0000
18.000 1.4245 0.07801 0.07375 -0.0255 0.0083 1.0000
18.250 1.4228 0.08183 0.07768 -0.0266 0.0082 1.0000
18.500 1.4224 0.08553 0.08148 -0.0278 0.0082 1.0000
18.750 1.4187 0.08985 0.08591 -0.0293 0.0082 1.0000
19.000 1.4150 0.09427 0.09043 -0.0310 0.0081 1.0000
19.250 1.4113 0.09877 0.09506 -0.0328 0.0081 1.0000
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