NACA 63(2)-215 MOD B (n63215b-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 63(2)-215 MOD B (n63215b-il) Reynolds number: 1,000,000 Max Cl/Cd: 83.93 at α=10° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-n63215b-il-1000000-n5.txt Download as CSV file: xf-n63215b-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NACA 63(2)-215 MOD B
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 -1.1811 0.09145 0.08766 -0.0311 1.0000 0.0083
-19.500 -1.1948 0.08553 0.08164 -0.0342 1.0000 0.0084
-19.250 -1.2090 0.07974 0.07572 -0.0372 1.0000 0.0083
-19.000 -1.2213 0.07437 0.07024 -0.0399 1.0000 0.0084
-18.750 -1.2263 0.07023 0.06602 -0.0418 1.0000 0.0084
-18.500 -1.2315 0.06616 0.06187 -0.0436 1.0000 0.0086
-18.250 -1.2382 0.06197 0.05757 -0.0454 1.0000 0.0085
-18.000 -1.2420 0.05831 0.05383 -0.0468 1.0000 0.0086
-17.750 -1.2424 0.05518 0.05062 -0.0479 1.0000 0.0086
-17.500 -1.2452 0.05181 0.04717 -0.0490 1.0000 0.0086
-17.250 -1.2439 0.04903 0.04430 -0.0499 1.0000 0.0088
-17.000 -1.2432 0.04625 0.04145 -0.0506 1.0000 0.0088
-16.750 -1.2405 0.04378 0.03890 -0.0511 1.0000 0.0088
-16.500 -1.2371 0.04151 0.03656 -0.0514 1.0000 0.0089
-16.250 -1.2323 0.03942 0.03441 -0.0516 1.0000 0.0090
-16.000 -1.2291 0.03721 0.03215 -0.0518 1.0000 0.0092
-15.750 -1.2237 0.03527 0.03015 -0.0518 1.0000 0.0092
-15.500 -1.2173 0.03348 0.02830 -0.0516 1.0000 0.0094
-15.250 -1.2102 0.03180 0.02659 -0.0514 1.0000 0.0097
-15.000 -1.2026 0.03019 0.02493 -0.0511 1.0000 0.0098
-14.750 -1.1936 0.02876 0.02346 -0.0506 1.0000 0.0100
-14.500 -1.1842 0.02740 0.02206 -0.0501 1.0000 0.0103
-14.250 -1.1743 0.02612 0.02072 -0.0495 1.0000 0.0103
-14.000 -1.1634 0.02496 0.01953 -0.0488 1.0000 0.0103
-13.750 -1.1522 0.02386 0.01839 -0.0480 1.0000 0.0106
-13.500 -1.1405 0.02284 0.01734 -0.0472 1.0000 0.0109
-13.250 -1.1286 0.02187 0.01634 -0.0462 1.0000 0.0110
-13.000 -1.1165 0.02098 0.01541 -0.0451 1.0000 0.0112
-12.750 -1.1041 0.02016 0.01456 -0.0439 1.0000 0.0115
-12.500 -1.0921 0.01937 0.01375 -0.0425 1.0000 0.0119
-12.250 -1.0800 0.01867 0.01304 -0.0410 1.0000 0.0124
-12.000 -1.0615 0.01800 0.01235 -0.0405 0.9767 0.0128
-11.750 -1.0210 0.01732 0.01160 -0.0441 0.9372 0.0135
-11.500 -1.0089 0.01691 0.01106 -0.0419 0.9042 0.0139
-11.250 -0.9954 0.01654 0.01059 -0.0398 0.8845 0.0144
-11.000 -0.9782 0.01614 0.01015 -0.0382 0.8696 0.0151
-10.750 -0.9592 0.01579 0.00975 -0.0370 0.8569 0.0159
-10.500 -0.9387 0.01545 0.00936 -0.0359 0.8458 0.0167
-10.250 -0.9174 0.01512 0.00896 -0.0349 0.8362 0.0172
-10.000 -0.8955 0.01478 0.00859 -0.0341 0.8273 0.0178
-9.750 -0.8729 0.01445 0.00823 -0.0333 0.8198 0.0188
-9.500 -0.8498 0.01412 0.00788 -0.0326 0.8122 0.0193
-9.250 -0.8259 0.01384 0.00755 -0.0320 0.8055 0.0200
-9.000 -0.8014 0.01355 0.00723 -0.0315 0.7982 0.0206
-8.750 -0.7764 0.01332 0.00695 -0.0311 0.7911 0.0212
-8.500 -0.7518 0.01299 0.00661 -0.0306 0.7839 0.0220
-8.250 -0.7268 0.01271 0.00630 -0.0301 0.7769 0.0228
-8.000 -0.7011 0.01244 0.00602 -0.0298 0.7709 0.0236
-7.750 -0.6751 0.01220 0.00575 -0.0295 0.7646 0.0243
-7.250 -0.6223 0.01174 0.00524 -0.0289 0.7532 0.0260
-7.000 -0.5959 0.01148 0.00498 -0.0287 0.7471 0.0274
-6.750 -0.5691 0.01127 0.00474 -0.0284 0.7414 0.0285
-6.500 -0.5419 0.01106 0.00452 -0.0283 0.7353 0.0297
-6.250 -0.5146 0.01087 0.00431 -0.0281 0.7288 0.0308
-6.000 -0.4874 0.01065 0.00409 -0.0280 0.7229 0.0327
-5.750 -0.4597 0.01045 0.00388 -0.0279 0.7172 0.0348
-5.500 -0.4322 0.01028 0.00369 -0.0277 0.7100 0.0372
-5.250 -0.4045 0.01008 0.00349 -0.0276 0.7002 0.0411
-5.000 -0.3773 0.00986 0.00328 -0.0275 0.6891 0.0495
-4.750 -0.3499 0.00962 0.00307 -0.0274 0.6779 0.0637
-4.500 -0.3224 0.00936 0.00288 -0.0274 0.6681 0.0823
-4.250 -0.2948 0.00910 0.00269 -0.0273 0.6580 0.1032
-4.000 -0.2667 0.00887 0.00253 -0.0273 0.6509 0.1237
-3.750 -0.2389 0.00861 0.00235 -0.0274 0.6432 0.1529
-3.500 -0.2111 0.00830 0.00216 -0.0274 0.6341 0.1896
-3.250 -0.1835 0.00795 0.00198 -0.0275 0.6255 0.2385
-3.000 -0.1558 0.00755 0.00179 -0.0276 0.6154 0.2991
-2.750 -0.1279 0.00720 0.00163 -0.0278 0.6021 0.3613
-2.500 -0.0995 0.00704 0.00154 -0.0279 0.5844 0.3968
-2.250 -0.0710 0.00692 0.00148 -0.0280 0.5676 0.4331
-2.000 -0.0421 0.00683 0.00145 -0.0281 0.5535 0.4629
-1.750 -0.0133 0.00684 0.00143 -0.0282 0.5330 0.4813
-1.500 0.0150 0.00692 0.00143 -0.0282 0.4966 0.4987
-1.250 0.0402 0.00745 0.00155 -0.0278 0.3704 0.5134
-1.000 0.0682 0.00764 0.00162 -0.0279 0.3405 0.5244
-0.750 0.0969 0.00774 0.00167 -0.0279 0.3212 0.5326
-0.500 0.1257 0.00786 0.00171 -0.0280 0.3029 0.5403
-0.250 0.1545 0.00796 0.00175 -0.0281 0.2841 0.5466
0.000 0.1831 0.00809 0.00180 -0.0281 0.2637 0.5528
0.250 0.2118 0.00822 0.00185 -0.0282 0.2457 0.5581
0.500 0.2405 0.00832 0.00190 -0.0283 0.2330 0.5635
0.750 0.2693 0.00842 0.00195 -0.0283 0.2224 0.5698
1.250 0.3269 0.00861 0.00208 -0.0285 0.2062 0.5809
1.500 0.3558 0.00869 0.00215 -0.0286 0.2001 0.5863
1.750 0.3845 0.00880 0.00222 -0.0287 0.1930 0.5912
2.000 0.4131 0.00889 0.00230 -0.0287 0.1868 0.5965
2.250 0.4418 0.00899 0.00239 -0.0288 0.1800 0.6024
2.750 0.4988 0.00922 0.00258 -0.0289 0.1679 0.6153
3.000 0.5271 0.00935 0.00269 -0.0289 0.1619 0.6222
3.250 0.5553 0.00948 0.00280 -0.0289 0.1560 0.6279
3.500 0.5836 0.00960 0.00292 -0.0289 0.1511 0.6343
3.750 0.6117 0.00975 0.00305 -0.0289 0.1461 0.6404
4.000 0.6397 0.00989 0.00318 -0.0289 0.1418 0.6469
4.250 0.6679 0.01001 0.00331 -0.0289 0.1391 0.6543
4.500 0.6958 0.01015 0.00346 -0.0289 0.1353 0.6607
4.750 0.7233 0.01032 0.00362 -0.0288 0.1302 0.6672
5.000 0.7509 0.01048 0.00377 -0.0288 0.1265 0.6730
5.250 0.7787 0.01062 0.00393 -0.0287 0.1237 0.6787
5.500 0.8061 0.01078 0.00410 -0.0287 0.1205 0.6851
5.750 0.8332 0.01098 0.00428 -0.0286 0.1167 0.6909
6.000 0.8602 0.01117 0.00447 -0.0284 0.1130 0.6972
6.250 0.8874 0.01133 0.00465 -0.0283 0.1110 0.7043
6.500 0.9144 0.01150 0.00485 -0.0282 0.1083 0.7111
6.750 0.9409 0.01171 0.00506 -0.0280 0.1049 0.7186
7.000 0.9670 0.01194 0.00528 -0.0278 0.1009 0.7257
7.250 0.9934 0.01214 0.00551 -0.0276 0.0980 0.7332
7.500 1.0193 0.01238 0.00574 -0.0273 0.0941 0.7399
7.750 1.0444 0.01266 0.00600 -0.0269 0.0891 0.7463
8.000 1.0699 0.01291 0.00626 -0.0266 0.0864 0.7531
8.250 1.0951 0.01316 0.00652 -0.0263 0.0836 0.7593
8.500 1.1198 0.01343 0.00680 -0.0259 0.0812 0.7663
9.000 1.1685 0.01398 0.00740 -0.0250 0.0776 0.7814
9.250 1.1924 0.01428 0.00771 -0.0244 0.0757 0.7894
9.500 1.2163 0.01453 0.00802 -0.0239 0.0746 0.7974
9.750 1.2401 0.01479 0.00832 -0.0234 0.0736 0.8054
10.000 1.2632 0.01505 0.00864 -0.0227 0.0724 0.8142
10.250 1.2854 0.01535 0.00897 -0.0220 0.0706 0.8250
10.500 1.3066 0.01568 0.00934 -0.0211 0.0685 0.8375
10.750 1.3267 0.01603 0.00973 -0.0200 0.0666 0.8505
11.000 1.3456 0.01639 0.01014 -0.0187 0.0645 0.8638
11.250 1.3622 0.01669 0.01051 -0.0170 0.0633 0.8803
11.500 1.3759 0.01700 0.01090 -0.0148 0.0618 0.9033
11.750 1.3851 0.01725 0.01129 -0.0117 0.0605 0.9704
12.000 1.4018 0.01771 0.01177 -0.0104 0.0590 1.0000
12.250 1.4172 0.01825 0.01232 -0.0090 0.0574 1.0000
12.500 1.4321 0.01884 0.01291 -0.0076 0.0556 1.0000
12.750 1.4468 0.01946 0.01354 -0.0063 0.0537 1.0000
13.000 1.4620 0.02007 0.01419 -0.0052 0.0530 1.0000
13.250 1.4771 0.02071 0.01486 -0.0040 0.0525 1.0000
13.500 1.4914 0.02141 0.01560 -0.0029 0.0516 1.0000
13.750 1.5033 0.02230 0.01648 -0.0017 0.0493 1.0000
14.000 1.5159 0.02317 0.01737 -0.0006 0.0483 1.0000
14.250 1.5276 0.02411 0.01835 0.0004 0.0470 1.0000
14.500 1.5391 0.02511 0.01937 0.0014 0.0453 1.0000
14.750 1.5510 0.02609 0.02040 0.0023 0.0444 1.0000
15.000 1.5612 0.02723 0.02157 0.0032 0.0425 1.0000
15.250 1.5734 0.02826 0.02267 0.0039 0.0430 1.0000
15.500 1.5735 0.03027 0.02463 0.0050 0.0368 1.0000
15.750 1.5834 0.03155 0.02596 0.0056 0.0367 1.0000
16.000 1.5865 0.03343 0.02787 0.0063 0.0332 1.0000
16.250 1.5827 0.03600 0.03044 0.0069 0.0284 1.0000
16.500 1.5850 0.03812 0.03261 0.0073 0.0268 1.0000
16.750 1.5621 0.04281 0.03732 0.0074 0.0190 1.0000
17.000 1.5799 0.04359 0.03818 0.0073 0.0226 1.0000
17.250 1.5742 0.04688 0.04154 0.0070 0.0208 1.0000
17.500 1.5295 0.05504 0.04980 0.0049 0.0121 1.0000
17.750 1.5271 0.05854 0.05339 0.0037 0.0124 1.0000
18.000 1.5112 0.06403 0.05901 0.0015 0.0111 1.0000
18.250 1.4877 0.07110 0.06623 -0.0019 0.0098 1.0000
18.500 1.4464 0.08181 0.07716 -0.0077 0.0080 1.0000
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